AMS A330 I10 A01

A330 AIRCRAFT MAINTENANCE SCHEDULE

VIETNAM AIRLINES TECHNICAL DEPARTMENT 200 NGUYEN SON - LONG BIEN - HA NOI

ISSUE 10 DATE: 25 JAN 2014; AMENDMENT 01 DATE:

06 SEP 2014

APPROVED BY: CIVIL AVIATION ADMINISTRATION OF VIETNAM

BO GIAO

THONG VAN TAl

CT)C HANG KHONG vrsr

NAM

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C()NG HoA xA H()I CmJ NGHiA vrsr NAM flQe Hip - Tlf do - Hanh phue

HaN9i, ngaY26 thang 09 ndm 2014

QUYETDINH V~ vi~e: Phe ehuAn tai li~u Chuong trinh bao dufrng A330 phat hanh 10 sira ctAi 01 ciia TAng Cong ty Hang khong Vi~t Nam

CT)C TRUONG CT)C HANG KHONG

vrer

NAM

- Can cir Luat Hang khong dan dung Viet Nam ngay 29106/2006; - Can cir Quyet dinh 94/QD- TTg ngay 16/07/2009 cua Thu nrong Chinh phu quy dinh chirc nang nhiem vu, quyen han va co d.u t6 chirc cua Cue Hang khong Viet Nam; - Can cir quy djnh cua BQ quy ch~ an toan hang khong dan dung linh virc tau bay va khai thac tau bay ban hanh theo thong nr sf> Ol/2011/TT-BGTVT ngay 27/0112011 cua BQ Giao thong Van tai; - Xet d~ nghi cua Tong Cong ty Hang khong Vi~t Nam tai cong van s5 1320/TCTHK-ATCL&AN, ngay 18/09/2014; - Xet d~ nghi cua Truong phong Tieu chuan an toan bay, QUYETDINH Di~u 1- Phe chuan Tai lieu "Chuong trinh bao dufrng may bay A330" phat hanh 10, sua d6i 01 CAMS A330 PH 10 Sf) 01) cua T6ng Cong ty

Hang khong Viet Nam.

Dieu 2- Truong phong Tieu chuan an toan bay, T6ng Cong ty HKVN va thu twang cac co quan don vi co lien quan chiu trach nhiem thi hanh quyet dinh nay.

Dieu 3- Quyet dinh nay c6 hieu lire

N(Ji nh~n:

- T6ng Cong ty HKVN; - Cue tnrong d~ bao cao - Luu VT, TCA TB.

k6 tir ngay kYq;;.., '--

Aircraft type: A330 AMS Amendment No: 01 Issue: 10 Date: 06/09/2014 In accordance with MPD revision 20 Issue 00 Date 01/09/2013

Vietnam Airlines ~'~

MAINTENANCE Submitted

NO.: VNA-TE-F21 Issue No.: 03 Deie: Jul. 2009

SCHEDULE APPROVAL SUBMISSION (CERTIFICATION)

Department:

by: ~

FORM

Checked

Department:

by:

zz>:

1/uQ;

NGUYEN CHIEN THANG Compliance Statement:

TECHNICAL

DEPT.

Date:

SAFETY-QUALITY AND SECURITY DEPARTMENT

16/09/2014

This Maintenance Schedule complies with the manufacturer's minimum maintenance and inspection requirements Authority for the airframe, engine (on wing), systems, and components except wherein previously or hereby approved

Date:

and that requirements of the Airworthiness by the Airworthiness Authority.

, Signed

Name

.... ~

Organisation:

Vietnam

..I?(/C)(f6

Position

Schedule Amendment

is

~_Xl/Ad

Airlines Company

..

p.~..p./~

....

Limited

The above Maintenance Schedule/ Maintenance approved with the following exception(s):

Siqnature Name:

Dale

=:': .. ~~

.

1K.A.!Y 'PlA..tyjj f.t.OtVG. 1.&".SIP, wf/ ..1~~~VTt~

.

For: (Airworthiness

. Authority)

. .

A330 AIRCRAFT MAINTENANCE SCHEDULE RECORD OF AMENDMENTS ALL AMENDMENTS TO THIS SCHEDULE WILL BE ACCOMPLISHED BY EITHER THE ORIGINATING DOCUMENT FOR THE "MASTER SCHEDULE" AND "MASTER COPY" FOR SCHEDULE "COPY HOLDERS". ENTER THE NUMBER IN NUMERICAL ORDER TOGETHER WITH THE DATE INSERTED AND THE SIGNATURE OF THE PERSON AMENDING THIS SCHEDULE.

ISSUE NO.

ISSUE DATE

AMDT NO.

AMDT DATE

01

JAN. 2007

00

JAN. 2007

02

MAR. 2007

00

MAR. 2007

03

JUN.2008

00

JUN.2008

04

FEB.2009

00

FEB.2009

05

AUG. 2009

00

AUG. 2009

05

AUG. 2009

01

OCT. 2009

06

FEB. 2010

00

FEB. 2010

06

FEB. 2010

01

APR.2010

07

SEPT.2010

00

SEPT.2010

08

JAN.2011

00

JAN.2011

08 08 08 08 08

JAN. 2011 JAN. 2011 JAN. 2011 JAN. 2011 JAN. 2011

01 02 03 04 05

APR.2011 JUN.2011 AUG.2011 NOV.2011 FEB.2012

09 09 09

APR.2012 APR.2012 APR.2012

00 01 02

APR.2012 AUG.2012 JAN.2013

10 10

DEC/2013 DEC/2013

00 01

DEC/2013 SEP/2014

Issue 10 Amendment 01

INSERTED DATE

SIGNATURE

Date:06/09/2014

A330 Maintenance Schedule

SECTION 0 SUMMARY OF CHANGES


REASON FOR ISSUE 10 AMENDMENT 01 1. INSTRUCTIONS This Amendment of Issue replaces A330 AMS Issue 10 Amendment 00 dated 01/12/2013 2. REASON FOR ISSUE 10 AMENDMENT 01 Revise AMS to add MSN 946VN-A383 in VNA A330-fleet

Date: 06/09/2014 ISSUE: 10 AMENDMENT: 01

Page 1


SUMMARY OF CHANGES 1.SECTION 0 Reason of issue: New 2. SECTION 1 Revise General Introduction 3. SECTION 2 Revise Line maintenance check list 4. SECTION 3 Update ENG LLP list; Revise TCI list 5. SECTION 4 See SUMARY OF CHANGE AMS I10 A01 for detail.

Date: 06/09/2014 ISSUE: 10 AMENDMENT: 01

Page 1

SUMMARY OF CHANGES AMS A330 I10 A01

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

REV CODE R R R R R R R R R R R R R R R R R R R R R R R R R

200001-08-1 200001-09-1 200007-02-2 212800-02-2 213100-05-2 233300-02-1 237300-10-1 242400-05-2 255100-01-1 255100-02-1 255100-08-1 255100-10-1 255100-19-1 261800-12-1 261800-13-1 262300-01-1 262300-04-2 271400-01-2 272100-18-1 272100-19-1 272200-01-2 272400-08-1 273400-01-1 274000-18-1 275100-01-1

26

R

275400-04-1

27 28 29 30 31 32 33 34 35 36 37 38 39 40

R R R R R R R R R R R R R R

275400-10-1 275400-11-2 278000-03-1 279000-09-2 279000-14-2 279000-15-1 279000-16-1 279000-20-1 282700-02-4 290000-01-1 291000-03-1 291000-04-1 291000-17-1 291000-19-1

41

R

291000-19-2

42 43 44 45

R R R R

292000-06-1 316001-01-1 316001-03-1 316001-04-1

ITEM

AMS A330 I10 A01

AMS TASK NUMBER

DESCRIPTION OF CHANGE INTERVAL CHANGE FROM 2C TO 36 MO INTERVAL CHANGE FROM 2C TO 36 MO IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED INTERVAL CHANGE FROM 1C TO 18 MO IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED INTERVAL CHANGE FROM 1000 FH TO 12000 FH IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED INTERVAL CHANGE FROM 1C TO 18 MO AMM update APPCABILITY CHANGE FROM ALL TO 275, 294, 299, 366, 943, 962, 1019, 1256, 1266 IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED AMM UPDATE IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED INTERVAL CHANGE FROM 1C TO 18 MO INTERVAL CHANGE FROM 1C TO 18 MO INTERVAL CHANGE FROM 1C TO 18 MO APPLICABILITY CHANGE FROM ALL TO 946 INTERVAL CHANGE FROM 1A TO 900 FH APPLICABILITY CHANGE FROM ALL TO 275, 294, 299, 366, 943, 962, 1019, 1256, 1266 INTERVAL CHANGE FROM 1A TO 900 FH IN IN IN IN

APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY

MSN MSN MSN MSN

946 946 946 946

ADDED ADDED ADDED ADDED Page 1 of 10

SUMMARY OF CHANGES AMS A330 I10 A01 ITEM 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94

REV CODE D R R R R R D R R R R R R R R R N R R R R R R R R R R R R R D D R R R R R R R R R R R R R D R D R

AMS A330 I10 A01

AMS TASK NUMBER 321000-05-1 321100-02-1 321112-01-1 322100-04-1 323100-12-1 325100-02-1 341300-02-1 341300-05-1 342200-01-1 342200-02-1 342200-03-1 344100-01-1 344100-02-1 344800-01-1 345200-01-1 361251-01-4 381000-02-1 381000-03-1 521000-07-1 522200-09-1 524103-01-3S020 525111-07-1 525111-08-1 531106-01-5S020 531124-01-6S020 531125-01-5S020 531129-02-3S020 531130-01-3 531131-01-3 531131-02-3 531142-01-2 531142-01-2S100 531143-01-3S020 531144-01-3S020 531149-01-2S020 531152-01-1 531154-01-3S020 531158-01-2S020 531165-01-1 531172-02-1 531175-01-4S020 531186-01-1 531188-01-5 531189-01-3S020 531198-01-3S020 532101-01-2 532107-02-1 532117-01-3 532117-02-5

DESCRIPTION OF CHANGE TASK DELETED AMM UPDATE IN APPLICABILITY MSN 946 ADDED AMM UPDATE IN APPCABILITY 299 REMOVED AMM UPDATE TASK DELETED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED APPLICABILITY CHANGE TO ALL IN APPLICABILITY MSN 946 ADDED NEW TASK IN APPLICABILITY MSN 946 ADDED INTERVAL CHANGE FROM 1C TO 18 MO INTERVAL CHANGE FROM 1C TO 18 MO IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED TASK DELETED TASK DELETED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED TASK DELETED IN APPLICABILITY MSN 946 ADDED TASK DELETED IN APPLICABILITY MSN 946 ADDED Page 2 of 10


REV CODE R R R R R R R R D R D D R R R R R R R N R R R R R R R R R R R R R R D R R D R R R R R R R D D R R

AMS A330 I10 A01

AMS TASK NUMBER 532124-02-1 532125-01-1 532129-01-3 532134-02-1 532138-01-1 532153-01-3 532156-01-4 532157-01-3 532166-01-3 533006-01-2 533009-01-2 533009-01-2S100 533013-01-5 533016-01-4S020 533019-01-2S020 533021-01-3 533035-01-2 533036-01-2 533101-01-9S020 533104-02-6 533106-01-5S020 533107-01-7S020 533109-01-2S020 533113-01-6 533114-01-5S020 533115-01-7 533126-01-6 533127-03-3 533154-01-6S020 533156-01-3 533164-01-4S020 533170-02-1 533181-01-7 533187-01-4 533193-02-1 533194-01-2 533195-02-2 533197-01-1 534102-01-5 534104-01-6 534105-01-6 534107-01-4 534108-01-2 534110-01-2 534120-01-4 534124-02-2 534126-01-2 534131-01-4 534140-01-1

DESCRIPTION OF CHANGE IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED IN APPLICABILITY TASK DELETED TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY NEW TASK IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED IN APPLICABILITY IN APPLICABILITY TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED TASK DELETED IN APPLICABILITY IN APPLICABILITY

MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN 946 ADDED

MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN 946 ADDED MSN 946 ADDED MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946


MSN 946 ADDED MSN 946 ADDED Page 3 of 10


144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164

REV CODE R R R R D R R R R R R R R R R R R R R R R

534143-01-4 534144-01-4 534156-01-1 534159-02-1 534177-01-3 535110-01-1 535118-01-1 535124-01-1 535127-01-3 535129-01-1 535130-01-1 535131-01-1 545101-02-2 545104-02-20 545106-01-2 545108-04-12 545118-02-2 545119-01-2 545122-01-2 545126-02-2 545126-02-2S100

IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED TASK DELETED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED THRESHOLD CHANGED FROM: "20 YE", TO: "24 YE" IN APPLICABILITY: 275, 962, 1019, 1256, 1266 REMOVED

165 166 167

R R R

545128-01-2 545129-01-3 545129-01-3S100

IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED THRESHOLD CHANGE FROM 26900 FC OR 87900 FH TO 21200 FC OR 143500 FH INTERVAL CHANGE FROM "8500 FC OR 27700 FH" TO "6700 FC OR 45300 FH"

168 169 170 171 172 173 174 175 176

D D R R R D D R R

545139-02-7 545140-01-8 545140-02-14 545142-02-7 545146-03-5S020 545146-03-7S020 545146-03-7 545146-04-5S020 545150-02-2

TASK DELETED TASK DELETED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED TASK DELETED TASK DELETED IN APPLICABILITY MSN 946 ADDED THRESHOLD CHANGE FROM 26700 FC OR 81900 FH TO 24100 FC OR 153600 FH INTERVAL CHANGE FROM "6000 FC OR 18300 FH" TO "5400 FC OR 34200 FH"

177 178 179 180 181

R R R R R

545150-02-7S020 545158-01-2 545160-01-1 545164-01-1 545168-02-13

R R

545168-02-13S100 545174-02-5S100 545174-04-2

IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED THRESHOLD CHANGE FROM 50000 FH TO 60000 FH. IN EFF 943, 946, 962, 1019, 1256, 1266 ADDED IN APPCABILITY 943, 962, 1019, 1256, 1266 REMOVED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED

ITEM

182 R 183 184

AMS A330 I10 A01

AMS TASK NUMBER

DESCRIPTION OF CHANGE

Page 4 of 10


185 186 187 188 189 190 191 192 193 194 195

REV CODE R R R R R R R D R R R

551001-01-1 551004-01-1 551008-01-9 551009-01-7 551011-01-1 551016-01-4S020 551019-01-4 551028-01-4 551028-02-4 551029-02-4 551600-01-1

IN APPLICABILITY MSN IN APPLICABILITY MSN IN APPLICABILITY MSN IN APPLICABILITY MSN IN APPLICABILITY MSN IN APPLICABILITY MSN IN APPLICABILITY MSN TASK DELETED IN APPLICABILITY MSN IN APPLICABILITY MSN INTERVAL CHANGE FROM

196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232

D R R R R R R D R R R R R R R R R R R R R R R R R R R R R R R D D R R R R

552007-02-2 553020-01-1 553024-01-2 553026-01-2 554021-01-2 554023-01-2 571102-01-6S020 571103-02-4 571107-01-5S020 571108-01-9S020 571116-01-5S020 571118-01-9S020 571121-01-5S020 571122-01-8S020 571123-01-5 571125-01-7S020 571126-01-6 571129-01-6S020 571130-01-6 571133-01-5S020 571137-01-6S020 571144-01-6S020 571145-01-5S020 571146-02-7S020 571152-01-5S020 571153-01-2S100 571159-01-7S020 571164-01-2 572004-02-7S020 572007-01-7 572009-01-8S020 572009-02-4 572009-02-4S100 572009-02-8S020 572010-01-1 572010-02-9S020 572012-02-6S020

TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY

ITEM

AMS A330 I10 A01

AMS TASK NUMBER

DESCRIPTION OF CHANGE 946 946 946 946 946 946 946


946 ADDED 946 ADDED "18MO 8500 FH" TO "24 MO 10000 FH"

MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN MSN MSN MSN

946 946 946 946

ADDED ADDED ADDED ADDED Page 5 of 10


REV CODE R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R D R R R R R R R

AMS A330 I10 A01

AMS TASK NUMBER 572015-02-6S020 572016-02-9S020 572017-01-7S020 572018-01-9S020 572019-01-9S020 572023-02-8S020 572027-01-9S020 572029-01-8S020 572030-01-9S020 572032-01-9S100 572033-01-9S020 572034-01-8S020 572035-01-8S020 572036-01-8S020 572037-01-7S020 572039-01-9S020 572040-01-8S020 572043-01-9S020 572045-01-4 572046-01-9S020 572047-01-8S020 572049-01-9S020 572050-01-8S020 572051-01-10 572052-03-8S020 572054-01-1S100 572062-01-1 572063-01-9S020 572064-01-1 572065-01-6S020 572066-01-1 572067-03-7 572068-01-9S020 572069-01-10S020 572071-01-8S020 572073-01-8S020 572075-01-1 572081-01-14 572082-01-1S020 572083-01-1 572084-01-5S020 572090-02-1 572092-01-8S020 572093-01-4S020 572093-02-4S020 572094-01-9S020 572106-01-8S020 572106-02-4 572107-01-8S020

DESCRIPTION OF CHANGE IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY TASK DELETED IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED Page 6 of 10


REV CODE R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R

AMS A330 I10 A01

AMS TASK NUMBER 572107-02-5 572108-02-9S020 572109-02-8S020 572110-01-9S020 572111-01-9S020 572119-02-5 572120-01-8S020 572121-01-9S020 572125-01-11S020 572125-02-9S020 572126-01-1 572126-02-8S020 572131-01-9S020 572133-01-9S020 572140-01-7S020 572141-01-7S020 572144-01-8S020 572148-01-9S020 572149-01-7S020 572151-01-1 572152-01-1 572153-01-10S020 572154-01-9 572155-01-1 572156-01-8S020 572158-01-9S020 572159-01-8S020 572161-01-1 572162-01-7S020 572163-01-1 572164-01-10S020 572165-01-10 572166-01-7S020 572171-02-1 572174-01-6S020 572180-01-9S020 572183-01-8S020 572183-02-8S020 572605-01-5S020 572606-01-8 572607-01-2S020 572608-02-2S020 572610-01-2 572610-02-8S020 572612-01-3 572612-02-9S020 572612-03-4S020 573001-01-10S020 573002-01-3S020

DESCRIPTION OF CHANGE IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN IN

APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY APPLICABILITY

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED Page 7 of 10


331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357

REV CODE R R R R R R R R R R R R R R R R R R R R R R R R R R R

358

R

574404-03-2

359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 374 375 376 377 378

R R R R R R R R R R R R R R R R R R R R

574404-03-2S100 574405-01-1 574501-01-1 574501-02-4 574504-01-1 574504-02-4 574505-01-1 574601-01-3 574601-02-1 574604-01-1 574604-02-3 574605-01-1 574701-01-1 574701-02-4 574704-01-1 574704-02-3 574704-03-1 574705-01-1 574801-01-1 574801-02-3

ITEM

AMS A330 I10 A01

AMS TASK NUMBER 573003-01-1 573003-02-8S020 573004-01-1 574101-01-1 574102-01-8S020 574103-02-4S020 574104-01-7S020 574105-01-7S020 574106-01-7S020 574107-01-2 574107-02-7S020 574109-02-5S020 574110-02-4S020 574111-01-7S020 574112-01-1 574114-03-5S020 574115-02-6S020 574116-01-7S020 574119-01-1 574301-01-3 574304-01-1 574304-03-2 574305-01-1 574307-01-1 574401-01-3 574401-02-1 574404-01-1

DESCRIPTION OF CHANGE IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY AMM update IN APPLICABILITY AMM update AMM UPDATE IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY IN APPLICABILITY

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED

MSN 946 ADDED

MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN MSN

946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946 946

ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED ADDED Page 8 of 10


379 380 381 382 383 384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 400 401 402 403 404 405 406 407 408 409 410 411 412

REV CODE R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R R

574804-03-2 574805-01-1 574901-01-1 574901-02-3 574904-01-1 574904-02-4S020 574905-01-1 575001-01-1 575002-01-1 575003-01-1 575004-01-1 575005-01-1 575006-01-1 575008-01-1 575010-01-7S020 575011-01-9S020 575012-01-7S020 575013-01-5S020 575015-02-3 575016-01-9S020 575017-01-8S020 575018-01-8S020 575022-01-4 575023-01-3S020 575025-01-8S100 575051-01-2 575054-01-1 575055-01-1 575057-01-2 575059-01-1 575063-01-3 575065-01-1 575067-01-2 575067-01-2S100

IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPCABILITY 943, 946, 962, 1019, 1256, 1266 ADDED THRESHOLD CHANGE FROM " 22500 FC OR 67500 FH" TO "18200 FC OR 109200 FH" INTERVAL CHANGE FROM "8500 FC OR 25500 FH" TO "6400 FC OR 38400 FH"

413 414

R R

575067-02-2 575067-02-2S100

IN APPCABILITY 943, 946, 962, 1019, 1256, 1266 ADDED THRESHOLD CHANGE FROM " 22500 FC OR 67500 FH" TO "18200 FC OR 109200 FH" INTERVAL CHANGE FROM "8500 FC OR 25500 FH" TO "6400 FC OR 38400 FH"

415 416 417 418 419 420 421 422

R D R R R R R R

575069-01-2 575401-02-1 575402-01-1 575403-01-1 575403-01-1S100 575404-03-2 575405-01-1 575405-02-1

IN APPLICABILITY MSN 946 ADDED TASK DELETED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED APPCABILITY CHANGE FROM 275 TO 294, 299, 366 IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED

ITEM

AMS A330 I10 A01

AMS TASK NUMBER

DESCRIPTION OF CHANGE

Page 9 of 10

SUMMARY OF CHANGES AMS A330 I10 A01 ITEM 423 424 425 426 427 428 429 430 431 432 433 434 435 436 437 438 439 440 441 442 443 444 445 446 447 448 449 450 451 452 453 454 455 456 457 458 459

REV CODE R R R R R R R R R R R R R R R R R R R R R N R R R R R R R N N D D R R R R

AMS A330 I10 A01

AMS TASK NUMBER 575407-01-1 575409-01-1 575503-01-1 575503-02-1 575505-01-1 575505-02-1 575507-01-1 575507-02-1 575509-01-1 575509-02-1 576103-01-1 576104-01-1 576105-01-1 576108-01-1 576113-01-1 576114-01-1 576114-02-1 576115-01-1 576117-01-1 576118-01-1 577003-01-1 577003-01-3 723300-P1-1 783200-P3-1 ZL-322-01-3 ZL-323-02-3 ZL-325-02-3 ZL-326-02-4 ZL-326-03-4 256500-01-1VNA 282500-01-VNA 533021-02-2 255100-20-1 242100-15-1 361251-01-3 361251-01-4 731000-P1-1

DESCRIPTION OF CHANGE IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPCABILITY 943, 962, 1019, 1256, 1266 REMOVED NEW TASK APPCABILITY CHANGE FROM TO ALL. (NOTE IN DESCRIPTION) INTERVAL CHANGE FROM 1C TO 18 MO IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED IN APPLICABILITY MSN 946 ADDED NEW TASK NEW TASK TASK DELETED TASK DELETED REMOVE TASK FROM TCI CROSS REFERENCE TABLE REMOVE TASK FROM TCI CROSS REFERENCE TABLE REMOVE TASK FROM TCI CROSS REFERENCE TABLE REMOVE TASK FROM TCI CROSS REFERENCE TABLE

Page 10 of 10


SECTION 1 INTRODUCTION

A330 Maintenance Schedule GENERAL INTRODUCTION The Aircraft Maintenance Schedule (AMS) document is issued by VIETNAM AIRLINES to define the maintenance program applicable to A330 aircraft shown on aircraft list (below). The AMS has been established to give a coordinated view of all tasks periodically performed on airframe systems, structure or power plant in purpose of detecting or preventing any fault which could affect the airworthiness of the aircraft. It contains maintenance tasks from the A330 Maintenance Planning Document (MPD) Revision 20 date 01/Sep/2013 customized in accordance with VIETNAM AIRLINES: -

National Requirements General Maintenance Policy Vendors Recommendations Aircraft Definition (Basic version, model and modification status).

It is also kept updated by additions/ amendments/ or intervals arising from (if any) : - In service experience - Reliability Program Document The following issues of the A330 major source documents are covered in this AMS Revision : -

Maintenance Review Board Report (MRBR) Revision 14 dated JUN 13 ALS part 1 Safe Life Airworthiness Limitation Items Rev 07 date SEP 23/13 ALS Part 2 Damage Tolerant Airworthiness Limitation Items (DT ALI) Issue 19 dated 23 MAR 2012 ALS Part 3 Certification Maintenance Requirements (CMR) Rev 04 dated AUGUST 2013 ALS Part 4 Ageing Systems Maintenance (ASM) Rev 04 dated AUGUST 2013 ALS Part 5 Fuel Airworthiness Limitations (FAL) Rev 00 dated 16 NOV 2011 ETOPS CMP Document Issue 25 dated 28 MAY 2013 PW Engine Manual Chapter 5

The AMS is kept updated by additions or amendments from sources mentioned here in above and detailed in the following section Attention is drawn to the fact that although the Maintenance Planning Document will reflect all repetitive scheduled ISSUE 10 AMENDMENT 01

INTRODUCTION

Page : 1/21

A330 Maintenance Schedule maintenance tasks promulgated by MRBR, ALS Parts, AOT, ISB, SIL, AD/CN, ..., it is the operators’ responsibility to adjust their programs on receipt of the source document and not to wait until the amended A330 MPD revision has been published This Maintenance Schedule is applicable to the following aircraft: AIRCRAFT LIST REGISTRATI ON

MS N

MODEL

VERSIO N

ENGINE

APU

WV

WV GROUP

VN-A371

0275

A330-223

PAX

PW4168A

GTCP331

021

32A

VN-A372

0294

A330-223

PAX

PW4168A

GTCP331

021

32A

VN-A374

0299

A330-223

PAX

PW4168A

GTCP331

021

32A

VN-A375

0366

A330-223

PAX

PW4168A

GTCP331

021

32A

VN-A376

0943

A330-223

PAX

PW4168A

GTCP331

052

VN-A377

0962

A330-223

PAX

PW4168A

GTCP331

052

32E 32E

VN-A378

1019

A330-223

PAX

PW4168A PW4170

GTCP331

052

32E

VN-A379

1256

A330-223

PAX

PW4170

052

32E

VN-A381

1266

A330-223

PAX

PW4170

GTCP331 GTCP331

052

32E

VN-A383

0946

A330-223

PAX

PW4168A

GTCP331

052

32E

ISSUE 10 AMENDMENT 01

INTRODUCTION

REMARKS

Page : 2/21


CONTENT The A330 Aircraft Maintenance Schedule (AMS) defines all Requirements for scheduled maintenance. Unscheduled maintenance such as lightning strike, hard landing inspection etc… is performed i.a.w. Chapter 05 AMM. The A330 Aircraft Maintenance Schedule (AMS) is divided into Sections 0 to 4. Section 0 SUMMARY OF CHANGES Section 1 GENERAL INTRODUCTION Section 2 LINE MAINTENANCE CHECK Section 3 SCHEDULED COMPONENTS MAINTENANCE Section 4 SCHEDULED AIRCRAFT MAINTENANCE


INTRODUCTION

Page : 3/21

A330 Maintenance Schedule MAINTENANCE CHECKS INTERVAL 1. LINE MAINTENANCE CHECKS PF TR TE WY ETOP PDSC

Pre-Flight Check: Transit Check Terminal Check (Daily Check ) Weekly Check

To be performed before each flight, but not earlier than 2 hours before the flight. To be performed during each A/C transit if it doesn’t exceed 36 calendar hours. To be performed in principle every day and in any case interval must not exceed 36 hours elapsed time. To be performed every 7 calendar days or before the next flight if the aircraft has not flown for more than 7 days.

ETOPS PreDeparture Service Check

To be performed within 2-4 hours of ETOPS departure

2. A CHECK: To be accomplished every 800 flying hours. A-Check and multiples : To be accomplished every 800 FH and multiples 3. C CHECK: 1C-Check

:

To be performed every 24 Months

2C-Check

:

To be performed every 42 Months

4C-Check

:

To be performed every 6 Years


INTRODUCTION

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A330 Maintenance Schedule 8C-Check : To be performed every 12 Years 4. Structure Section: For the Structure section, the basic initial thresholds and intervals for environmental deterioration related items are as follows: Thresholds: 6 Years and 12 Years Intervals: 6 Years and 12 Years NOTE: Some calendar thresholds and intervals remain at 5 Years or 10 Years, pending further evolution. Thresholds and intervals for fatigue damage related items are given in Flight Cycles (and Flight Hours for range sensitive items).


INTRODUCTION

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A330 Maintenance Schedule TASK INTERVAL FRAME: Operational units (usage parameters) - "FH" (Flight hours) : Elapsed time between wheel lift off and touchdown. - "CY", “FC” (Flight Cycle) : A complete take off and landing sequence. - "AH" (APU Hours) : APU operating hours. PU task intervals quoted in terms of APU HRS may be converted to another usage parameter in accordance with conversion factor. APU hours multiply flight hours by 0.35; APU cycles multiply APU hours by 1.00 - Battery Operating Hour: To calculate the Battery Operating Hour the following apply: 1 FH = 1.25 Battery Operating Hour Calendar units - HR" (Hour) : One Calendar hour elapsed. - "DY" (Day) : 24 Calendar hours elapsed. - "MO" (Month) : One Calendar month. - YE" (Year) : One Calendar year. Other codes - "NR" (National Requirement): Task known as being subject to national regulatory requirement. - “VR" (Vendor Recommendation): Interval value dependent on task vendor recommendation. - "NT" (Note): Refer to the note at the task description.


INTRODUCTION

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A330 Maintenance Schedule GENERAL RULES The following rules, apply to the A330 maintenance program: A. The operator's manuals shall contain the details and responsibilities for accomplishing the maintenance identified by this document. B.

The overall reliability of the A330 will be monitored by each operator's system for continuous analysis and surveillance as required by the operator's Regulatory Authority.

C.

Task intervals of tasks with source “MRBR” may be changed in accordance with operator's Regulatory Authority. However, tasks with Failure Effect Category 5 and 8 must not be deleted from the operator's maintenance program. In this respect, attention is drawn to the task origin (refer to MPD “SOURCE” column).

D.

Each operator should be aware of the various inspection techniques such as X-Ray, ultrasonic, eddy current, radio isotope, which are available and described in the Non Destructive Testing Manual (NTM). The use of such techniques can be developed to provide a valuable adjunct to the prescribed visual inspections. For any substitution of such inspection technique, it must be ensured that the same damage size will be detectable by the proposed technique with, at least, the same level of confidence.

E.

Items that are life limited will be removed from service according to the life limits stated in the appropriate section of the engine or aircraft manufacturer's manuals. These sections are referenced in the aircraft "Type Certificate Data Sheet".

F.

Certification Maintenance Requirement tasks generated by systems safety assessment shall not be deleted from operators maintenance program. CMR** : CMR* :

Task interval may be escalated by an operator, in accordance with an approved related program. Task interval shall not be escalated by an operator.

G.

Tasks may be considered to conform to the requirements of the scheduled maintenance program if accomplished as part of a Regulatory Authorities approved/accepted equivalent check/test by flight crew.

H.

It is the responsibility of each operator to adjust his own maintenance program in accordance with his National Requirements and to comply with existing rules with respect to reporting to his Regulatory Authority and to the


INTRODUCTION

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A330 Maintenance Schedule manufacturer events having effects on the continued airworthiness of the aircraft. I.

Task interval parameters expressed in this MPD may be converted to an individual operator’s desired unit (flight hours, cycles or calendar time) provided this conversion does not result in the operator exceeding the initial requirements of the MPD.

J.

The maintenance clock does not stop while the aircraft is in maintenance condition. Although the aircraft does not collect any FH or FC when being on ground, attention has to be given to tasks, where the interval is expressed in calendar time (hours, days, month, year). All tasks that become due at the time of the maintenance visit have to be performed prior to return to service. However, there is no need to repeat inspections during the check event. E.g. during a 4 weeks downtime, tasks with interval 8 DY only need to be performed at the end of the check (return to service).

K.

The thresholds and intervals quoted in calendar time in this document include aircraft time in and out of service. In other words, operators will not, in general, be allowed to take credit for time out of service or storage periods to extend calendar inspection thresholds/intervals. Exceptions to this can be considered by Airbus Maintenance Engineering but will depend on variables such as time duration, aircraft age, environment and where aircraft was in maintenance cycle. Specific advice can be given by Airbus Maintenance Engineering on a case-by-case basis if relevant aircraft details are provided.

L.

The reapplication of all protective materials (e.g. Temporary Protection Systems (TPS), paints etc.) Shall be carried out following their removal to perform the inspection/maintenance task.

M.

The CMP (ETOPS) document, reference AI/EA5000, is the authoritative document for mandatory ETOPS Maintenance Standards. Where maintenance task intervals in the CMP are more restrictive than required in the MRBR, these overrule those in the MRBR. Where the MRBR task interval is more frequent than required by the CMP, the MRBR value remains valid until the operator justifies escalation (the CMP interval acts as an upper limit to the escalation). Maintenance tasks, which become obsolete due to an authorized configuration change are not applicable. Any fairings, panels, doors or other items which are removed/opened to gain access for maintenance tasks must also be inspected for general condition with a minimum level of GVI before reassembly/refitting. Operators shall report any findings to the manufacturer via the inspection reporting system on AirbusWorld/Maintenance and Engineering/Prepare Maintenance/Optimize maintenance management/Optimize maintenance program/Report my check records.

N. O.


INTRODUCTION

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MAINTENANCE CLOCK STARTING POINT Unless otherwise specified by AIRBUS in the documentation of an aircraft at time of first delivery, the starting point for calculation of the due dates or times of all aircraft maintenance tasks is identified in the following paragraphs. A. General rule The date of first Transfer of Title (ToT) may be used as the starting point for the following: • Systems / Power Plant tasks with intervals expressed in airframe FH, FC or Calendar Time (except as identified in paragraph “2. Specific guidance”) • Structure tasks with an interval quoted in Calendar Time • Zonal tasks NOTE: This may not be valid if the first ToT occurs more than 90 days after first flight. In this situation specific guidance may be given to the operator at time of delivery. If details are not available to subsequent operators then any task that has not yet been accomplished shall be conservatively planned with reference to first flight date. First flight shall be used for all structure tasks with an interval quoted in FH, FC or LDGS. Tasks with intervals quoted in terms of component FH or component FC (e.g. APU Hours, Engine Cycles, ACT FH) shall be counted from First Flight of the component. The time to start the clock for tasks with applicability determined by post-delivery modification embodiment is the date of embodiment. B. Specific guidance - For ALS Part 1 (SL-ALI) items : Limitations quoted in Calendar Time, FC, LDGS or FH count from first flight after installation - For ALS Part 2 (DT-ALI) tasks: o The threshold is the time at which the maintenance task is first due.  Threshold limitations quoted in FC or FH count from first flight.  Threshold limitations quoted in Calendar Time may be counted from the Transfer of Title to the first operator o For repeat maintenance tasks, the interval usage parameter (Calendar Time, FC or FH) is counted from the time the task was previously performed. ISSUE 10 AMENDMENT 01

INTRODUCTION

Page : 9/21


-

-

-

-

-

-

o In cases where the first maintenance is accomplished very early, the next inspection can be performed at the threshold if the period (Calendar Time, FC or FH) between initial task accomplishment and the threshold is greater than the interval o When alternative inspection methods are provided, the next interval applicable is the one associated with the inspection method used at the previous inspection. o "Touch and Go" cycles can be neglected if they are less than 5% of the total number of Flight Cycles up to threshold inspection or between two consecutive inspections. Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold inspection or between two consecutive inspections. For ALS Part 3 (CMR) tasks: o Limitations quoted in FH or Calendar Time may be counted from the Transfer of Title to the first Operator. This policy is agreed with EASA in Consideration of the very low number of FH performed between first flight and delivery, and the methodology used to define the value of CMR task limitations. o Limitations quoted in FC count from first flight. For ALS Part 4 (ASM) tasks: o Limitations controlled at aircraft level and quoted in Calendar Time count from the Transfer of Title to the first operator. o Limitations controlled at aircraft level and quoted in FH, FC or LDGS count from first flight. o Limitations controlled at component/subassembly level and quoted in Calendar Time, FH, FC or LDGS count from the date at which the component/item accomplishes the first flight for which it will undertake its intended function. For ALS Part 5 (FAL) tasks: o Limitations quoted in Calendar Time may be counted from the Transfer of Title to the first operator. o Limitations quoted in FH or FC count from first flight. For an overhauled landing gear or a new landing gear installed after first Transfer of Title: the start date for Calendar Time tasks is the date of the gear’s first flight after installation. If this first flight takes place more than 90 days after installation contact Airbus Maintenance Programs Engineering front desk: [email protected] For equipment having intervals defined by the vendor (VR) or by National Requirements (NR) : the starting point is the date of manufacture or date of overhaul (for Calendar Time tasks) or the first flight for which it will undertake its intended function (for FH and FC tasks) unless otherwise stated by vendor or National Authority. For components addressed by Airworthiness Directive (AD):as stated in the AD.


INTRODUCTION

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A330 Maintenance Schedule - For components that are transferred between aircraft: If the required task on the transferred component is performed as part of the installation process, then the next performance of the task counts from the installation date. Otherwise: o For system and structural components transferred between aircraft, the threshold for Calendar Time tasks is counted from either the date at which the aircraft to which it was originally fitted had its first Transfer of Title (if applicable) or, for a new component installed after delivery, the date at which the component accomplishes its first flight. o For structural components transferred between aircraft, the threshold for FH, FC or LDGS tasks is counted from the date at which the component accomplishes its first flight. o For system components transferred between aircraft, the threshold for FH and FC tasks is counted from either the date at which the aircraft to which it was originally fitted had its first Transfer of Title (if applicable) or, for a new component installed after delivery, the date at which the component accomplishes its first flight. Summary: Source SYSTEM MRBR STRUCTURE ZONAL Part 1 Part 2 Part 3 Part 4 (aircraft ALS level) Part 4 (component level) Part 5 LDG overhaul or installation of new gear ISSUE 10 AMENDMENT 01

Calendar Time TOT TOT TOT 1st Flight TOT TOT

Flight Hours TOT 1st Flight TOT 1st Flight 1st Flight TOT

Flight Cycles or Landings TOT 1st Flight TOT 1st Flight 1st Flight 1st Flight

TOT

1st Flight

1st Flight

1st Flight TOT

1st Flight 1st Flight

1st Flight 1st Flight

1st Flight after installation

N/A

1st Flight

INTRODUCTION

Page : 11/21

A330 Maintenance Schedule after first TOT Date of Manufacture or Date of Manufacture or Overhaul* Overhaul* NR, VR See AD See AD AD * Unless otherwise stated in vendor or National Authority documentation


INTRODUCTION

Date of Manufacture or Overhaul* See AD

Page : 12/21

A330 Maintenance Schedule IMPLEMENTATION PERIOD A. GENERAL The IMPLEMENTATION PERIOD is a Grace period for the first time accomplishment of new tasks added to a Maintenance Program of an aircraft already in service in case there is no specific note of compliance date. The following paragraphs suggest Implementation Periods for the tasks originating from the various MPD source documents. The Implementation Period, often referred to as a “Grace” period, is to assist with first time accomplishment of new tasks added to a maintenance program of an aircraft already in service. B. AD/CN The compliance date is identified in the AD/CN. C. Airworthiness Limitations Items (ALI)– ALS Part 2 ALI grace periods must be handled on a case by case basis, using specific utilization data from concerned aircraft. It would be ensured that there do not exceed the limitation without prior agreement with the manufacturer, the local airworthiness authority and the certificating authority. In exceptional circumstances an ALI may be issued which is already overdue on a particular aircraft. In such cases Vietnam Airlines will contact manufacture (Airbus) to provide guidance for specific advice. D. Certification Maintenance Requirements (CMR)– ALS Part 3 In theory, a CMR cannot be added, or an existing CMR made more restrictive, to an in-service aircraft. All CMRs should be published before the subject design feature enters service, whether this is on the basic aircraft or as a result of a modification. If delays occur in CMR document approval it is possible that a CMR becomes valid after EIS. In this case, the CMR document transmittal letter will advise an appropriate grace period before first time accomplishment. E. Aging System Maintenance (ASM) – ALS Part 4 ALS Part 4 tasks are being established in order to allow operation of aircraft systems beyond their original qualification. Beyond this point, ageing effects may affect the characteristics leading to an increased potential for failure. The Part 4 of the Airworthiness Limitations Section (ALS) therefore contains the maintenance actions together with their limitation to help to qualify the systems for continued operation F. Fuel Airworthiness Limitation Items (FAL) – ALS Part 5 On aircraft that have already exceeded the task threshold, It is recommended that the FAL tasks are performed at the operator's next scheduled structural inspection at 6 YE or 12 YE. G. MRB Report and MRB Report Temporary Revision (TR) MRB Report (MRBR) tasks arise from a theoretical analysisof the aircraft prior to entry into service. Tasks are categorized according to whether they are associated with hidden or evident conditions and according to their contribution to the avoidance of safety and non safety related failure effects. These categories give an idea of 'importance' or 'criticality' (FEC 5, 8, 9, 6 and 7 decreasing order of importance) and allow a different grace period policy to be established for different groups. ISSUE 10 AMENDMENT 01

INTRODUCTION

Page : 13/21

A330 Maintenance Schedule Depending on Vietnam Airlines qualifications and overall VAECO maintenance experience, adjustments to initial maintenance program tasks and intervals shall be approved by CAAV. Vietnam Airlines suggest that a local guideline could be as follows: - For all A and A multiple tasks (including those quoted in an equivalent FH/FC/Calendar Time parameter): Perform at the next A-Check. This might not be the next A-Check (for which the planning may be completed) but it would be expected in the following one. - For all former C and 2C tasks (18 MO, 24 MO, 10000 FH, 42 MO, 20000 FH & 48 MO tasks) or equivalent threshold/interval: Perform at the next C-Check. This might not be the next C-Check (for which the planning may be completed) but it would be expected in the following one. NOTE: If task elapsed time is short and any possible corrective action is easily addressed, first performance of at least the FEC 5 and 8 tasks in the next convenient Acheck package. NOTE: L/HIRF ATA 20 tasks (listed in MRB Appendix 9) should be scheduled as a priority in the next C–Check. - For 4C and 8C tasks (including those quoted in an equivalent FH/FC/Calendar Time parameter): Perform at the next C-Check or next equivalent check. NOTE: It is recognized that in some cases access is not available at the C/2C opportunity, for example, fuel tank entry, galley or lavatory removal. In these cases, unless stated otherwise in the MRB Report transmittal letter, Airbus recommends accomplishment at the next 4C check. - For CPCP related tasks A revised CPCP requirement is normally associated with corrosion findings. In case of overruns, the concerned operator needs to consider his local operating conditions in order to assess the potential for corrosion in this area on his particular aircraft. It is recommended to perform the task as soon as possible on at least one aircraft in the fleet in order to help make this assessment. Delay in accomplishment may lead to higher repair costs but not a loss of continued airworthiness. Note that if a safety concern exists, a new CPCP task recommendation on an inservice aircraft would be promulgated by ISB (and possibly CN/AD) in addition to inclusion in the MRB Report. - For EWIS related tasks On aircraft that have already exceeded the task threshold, Airbus recommend that the EWIS tasks are performed at the operator's next convenient check opportunity unless access is assessed as insufficient to perform the task without ISSUE 10 AMENDMENT 01

INTRODUCTION

Page : 14/21

A330 Maintenance Schedule exceeding the scheduled out-of-service period. In this case, the task should be performed at the next suitable access opportunity (e.g. a structural inspection at 6 YE or 12 YE) but not exceeding the task interval counting from the MRBR. H.

I.

Inspection Service Bulletins / All Operator Telexes As for AD, these documents normally include a recommended compliance time. Where this is not stated, it is recommended that Vietnam Airlines follows the same guidance as for the MRB Report. Service Information Letters It is recommended that Vietnam Airlines follows the same guidance as for the MRB Report.


INTRODUCTION

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A330 Maintenance Schedule PERMITTED VARIATIONS TO MAINTENANCE PERIODS Vietnam Airlines may vary the periods described by this Maintenance Schedule provided such variations are within the limits defined below. Variations shall be permitted only when the periods prescribed by this Maintenance Schedule (or documents m support of this Maintenance Schedule) cannot be complied with due to circumstances which could not have reasonably been foreseen by Vietnam Airlines. The decision to vary any of the prescribed periods shall be taken only by the Chief Inspector/Quality Manager or person of equivalent status on behalf of Vietnam Airlines. item controlled by flying hours 5000 flying hours or less more than 5000 flying hours

maximum variation of the prescribed period 10% 500 flying hours

item controlled by calendar maximum variation of the prescribed time period 1 year or less 10% or 1 month whichever is the lesser More than 1 year but not 2 months exceeding 3 years more than 3 years 3 months item controlled landing/cycles 500 landing/cycles or less

by maximum variation of the prescribed period 5% or 25 landing/cycles, whichever is the lesser. more than 500 landing/cycles 5% or 250 landings/cycles, whichever is the lesser. ISSUE 10 AMENDMENT 01

INTRODUCTION

Page : 16/21

A330 Maintenance Schedule NOTES : 1) 2) 3) 4)

Tolerances may not be cumulated. Tolerances are not allowed for items related to ALIs , LLP, CMR , ASM, FAL, AD/CN, If Permitted Variations is used for ETOPS Tasks (task with note “CMP task”), this Aircraft must be downgrate to NON ETOPS till performance of the task. For the ECO task Tolerances is 20%.


INTRODUCTION

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A330 Maintenance Schedule METHOD OF NEXT DUE CALCULATION : When determine the next due of a check, use the following method:

Due

CRS date

Next Due

CRS date

- If CRS date is after Due Date, then the Next Due = Due + Interval - If CRS date is before Due Date, then the Next Due = CRS + Interval


INTRODUCTION

Page : 18/21

A330 Maintenance Schedule FORMAT LAYOUT DESCRIPTION A GENERAL

B

The schedule maintenance tasks are shown in a table of 7 columns. Each task is identified by a specific "Task Number". The total information recorded under a task number is called "Item". DEFINITION OF TERMS (1) REVISION column A letter code gives the status of the item at the date of issuance : «N» «R» «D» Blank

: New : Revised : Deleted : No change

(2) ITEM NUMBER Column. a) General rules : The Item Number is built as written in the A330 Maintenance Planning Document and ATA 100 specification and has following format :

with

XX-YYY-YY XX = ATA chapter YYY-YY = MPD sequence number

(3) ZONE Column


INTRODUCTION

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A330 Maintenance Schedule A Number of three digits identifying the area where the system, part or equipment covered by the item is located, in compliance with the A330 zoning system. The zone allocation has been made according to the following rules : a) If the task involves only one zone, the relevant zone number is indicated b) If the task involves several zones for access, action and result, the most appropriate zone number is indicated. c) If the zone number cannot be determined, the number "000" is indicated. (4) DESCRIPTION Column This column provides the following information : a) b) C)

Task description Gives a concise description of the test or inspection to be performed. Task preparation (if applicable). Specifies the preliminary steps to be performed prior the maintenance task itself. Specifies the identifiers of the access panels, lining or doors to be opened or removed for accomplishment of the task.

(5) INTERVAL and THRESHOLD Column This information gives a specific value of an operational parameter or of a letter code defining the maximum time that can separate two complete accomplishments of the task and the first accomplishment of the task. (6) REFERENCES Column This column provides references of the task in the A330 Aircraft Maintenance Manual.


INTRODUCTION

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A330 Maintenance Schedule (7) EFFECTIVITY Column The information given in this column defines the aircraft on which the task is applicable: - "ALL" indicates that the task is applicable to all aircraft in the A330 fleet. - Serial number indicates that the task is applicable to this particular aircraft in A330 fleet.\ - For Task with the “NOTE: TASK COMPONENT RELATED” the effectivity is shown as “ALL”, because the component is changeable and can replaced with another P/N. UP-DATING Revision of subject document will be done as follows : Revision amendment list shall provide the modifications brought since the last revision with a short description of the technical background of this change. Urgent items will be handled separately with a yellow form (Temporary Revision). In case of cancellation of an item within a given sub-chapter, the item number should be retained and the letter "D" is indicated in revision column. On the next revision, it would be no more present.


INTRODUCTION

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A330 Maintenance Schedule GLOSSARY 01.

GENERAL DEFINITIONS THRESHOLD

The specific value of a usage parameter (flight cycles, flight hours, etc…) at which the first inspection of some particular level or method should be conducted.

REPEAT INTERVAL

The maximum permitted period for all tasks not performed on a sampling basis that can separate total completion of a task from its next accomplishment.

MAINTENANCE TASK

An action or set of actions required to achieve a desired outcome which maintains an item (component, system/sub-system, structure) in or restores an item to serviceable condition. This term includes inspection and determination of condition.

Item identified by the manufacturer, whose failure: - Could affect safety (ground or flight), and/or MAINTENANCE SIGNIFICANT - Is undetectable during operation, and/or ITEM (MSI) - Could have significant operational economic impact, and/or- Could have significant non-operational economic impact. STRUCTURE SIGNIFICANT ITEM (SSI)

A structural detail, structural element or structural assembly which is judged significant by the manufacturers because of the reduction in aircraft residual strength or loss of structural function which are consequences of its failure.

DISCARD (DIS)

The removal from service of an item at a specified life limit

RESTORATION

That work (on/off the aircraft) necessary to return the item to a specific standard.

REPLACEMENT

The action whereby an item is removed and another new or restored item is installed in its place.

SERVICING ISSUE 10 AMENDMENT 01

Consumable replenishment by servicing GLOSSARY

Page : 1/11

A330 Maintenance Schedule 02.

SYSTEMS TASK DEFINITIONS :

CHECK

Task performed to ensure that a system or component is still serviceable (check of bottle weight, check of firing circuit continuity, etc…) or that pressures or fluid levels are correct.

VISUAL CHECK ( VC )

A visual check is an observation to determine that an item is fulfilling its intended purpose.Does not require quantitative tolerances. This is a failure finding task.

DETAILED VISUAL INSPECTION (DVI)

An intensive visual examination of a specified detail, assembly, or installation. It searches for evidence of damage or irregularity using adequate lighting and, where necessary, inspection aids such as mirrors, hand lens, etc. Surface cleaning and elaborate access procedures may be required.

FUNCTIONAL CHECK ( FUC )

A quantitative check to determine if one or more functions of a system/sub-system or component performs, within specified limits. This task may call for the use of special test equipment.

OPERATIONAL CHECK OPC )

A task to determine that an item is fulfilling its intended purpose. Do not require quantitative tolerances. This is a failure finding task.

LUBRICATION (LUB)


(

Term covering all types of lubrication (grease gun, squirt can, spray, brush or hand application) for the purpose of maintaining the inherent design operating capabilities of an item.

GLOSSARY

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STRUCTURAL AND ZONAL TASKS DEFINITIONS :

GENERAL VISUAL INSPECTION ( GVI ) DETAILED INSPECTION ( DI )

SPECIAL DETAILED INSPECTION ( SDI )


A visual inspection that will detect obvious unsatisfactory conditions/discrepancies in structure and system/powerplant installations. This type of inspection may require removal of fillets, fairings, access panels, doors, etc…, to gain access and the use of ladders, workstands, etc, may be required to gain proximity. An intensive visual examination of a specified detail, assembly, or installation . A potential failure finding task. An intensive check of a specific location requiring some special technique such as nondestructive test techniques, dye penetrant, high-powered magnification, etc… and that may require disassembly procedures.

GLOSSARY

Page : 3/11


CORROSION LEVEL DEFINITIONS :

LEVEL 1 CORROSION

Corrosion occurring between successive inspections that is local and can be reworked/blended-out within manufacturer’s allowable limits (e.g. SRM, SB, etc.). OR Corrosion occurring between successive inspections exceeds allowable limit but is local and can be attributed to an event not typical of operator usage of other aircraft in the same fleet (e.g. Mercury spill). OR Operator experience over several inspections has demonstrated only light corrosion between each schedule inspections but the latest inspection and cumulative blendout now exceed allowable limit. The terms « local corrosion » and « light corrosion » are model specific and will be determined by the manufacturer and published in appropriate maintenance documents.

LEVEL 2 CORROSION

Corrosion occurring between successive inspections that requires a single rework/blend-out which then exceeds allowable limits, requiring a repair/reinforcement, or complete or partial replacement of a PSE, or other structure listed in the Baseline Program. OR Corrosion occurring between successive inspections, that is widespread and requires a single blend-out approaching allowable rework limits.


GLOSSARY

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A330 Maintenance Schedule Corrosion found during the first or subsequent inspections, which is determined (normally by the operator) to be an urgent airworthiness concern, requiring expeditious action. LEVEL 3 CORROSION

05.

Note : When LEVEL 3 corrosion is found, consideration should be given to action required on other airplanes in the operator's fleet. Details of the corrosion finding and planned action(s) should be expeditiously reported to the appropriate regulatory authority.

COMPONENT TASKS CODE DEFINITIONS : O = OVERHAUL

Overhaul of a component according to the Component Maintenance Manual (CMM) or the detailed description of this task code in the CMM.

R = REPAIR

Repair or partial overhaul of the component according to the detailed description of this task code in the CMM.

B = BENCH

Test of a component to verify, whether the component characteristics meet the requirement specified under « Testing » in the CMM or the detailed description of this task code in the CMM.


GLOSSARY

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A330 Maintenance Schedule ABBREVIATIONS The following abbreviations are used through out the present document : A/C : Aircraft AC : Alternating Current AC : APU Change ACMS : Aircraft Condition Monitoring System AD : Airworthiness Directive EAD : EASA Airworthiness Directive FAD : FAA Airworthiness Directive ADF : Automatic Direction Finder AFT : Rear AH : APU Operating Hours AIB : Airbus AMM : Aircraft Maintenance Manual AMTOSS : Aircraft Maintenance Task Oriented Support System AOL : All Operators Letter AOT : All Operator Telex AOW : All Operator Wire APU : Auxiliary Power Unit ASM : Ageing Systems Maintenance ATA : ATA Specification ATT : Attitude BAT : Battery BCL : Battery Charge Limiter BCRC : Bulk Crew Rest Compt. ISSUE 10 AMENDMENT 01

GLOSSARY

Page : 6/11

A330 Maintenance Schedule CESM CFMI CMR CN COMPT CPCP CRR CSU CVR CY

: : : : : : : : : :

Commercial Engine Service Memorandum CFM International Certification Maintenance Requirements Consigne de Navigabilité (French Airworthiness Directive) Compartment Corrosion Prevention and Control Program Crew Rest Room Command Sensor Unit Cockpit Voice Recorder Cycle

D DC DFDR DI DS DY EC ECAM EDP ELT EMER EMP EXTIR FAA F-BCRC

: : : : : : : : : : : : : : :

Deleted Direct Current Digital Flight Data Recorder Detailed Inspection Discard Day Engine Change Electronic Centralized Aircraft Monitoring Engine Driven Pump Emergency Locator Transmitter Emergency Engine Management Plan (RR engines) Extinguisher United States Federal Aviation Administration Full Bulk Crew Rest Compartment


GLOSSARY

Page : 7/11

A330 Maintenance Schedule FC FC FCOM FCRC FH FWD GCU GLC GPCU GPWS GSE GRP x GVI HDG HIRF HR IDG INTRO IOR ISB ISIS LD LD LDF LDL

: : : : : : : : : : : : : : : : : : : : : : : : :


Flight Cycle Functional Check Flight Crew Operating Manual Flight Crew Rest Compt. Flight Hours Forward Generator Control Unit Generator Line Contactor Ground Power Control Unit Ground Proximity Warning System Ground Support Equipment Weight variant group “x” General Visual Inspection Heading High Intensity Radiated Fields Hour Integrated Drive Generator Introduction Immediate Operational Request (Inspection) Service Bulletin Integrated Stand By Instrument System Landing Lower Deck Lower Deck Facility Lower Deck Lavatory GLOSSARY

Page : 8/11

A330 Maintenance Schedule LDMCR LEP LGCIU LH LU LTA LWR MAN MCDU MH MO MOD MPD MPG MRB MSG MSI MSN N NDT NR NT NTM P-BCRC PCU

: : : : : : : : : : : : : : : : : : : : : : : : :


Lower Deck Mobile Crew Rest List of Effective Pages Landing Gear Control and Interface Unit Left Hand Lubrication German Airworthiness Directive Lower Manufacturer Advisory Notice (PW engines) Multipurpose Control and Display Unit Man hours Month(s) Modification Maintenance Planning Document Maintenance Planning Guide (PW engines) Maintenance Review Board Maintenance Steering Group Maintenance Significant Item Manufacturer Serial Number New Non Destructive Testing National Requirements Note Non Destructive Testing Manual Partial Bulk Crew Rest Compartment Power Control Unit GLOSSARY

Page : 9/11

A330 Maintenance Schedule POB PREP QAD R RH RII RMP RR RS RSVR S SIL SOV SRM SSI SYS SV TBD TCAS THS TOC TPIS TPS TR UD

: : : : : : : : : : : : : : : : : : : : : : : : :


Pressure off Brakes Preparation Quick Attach Detach Revised Right Hand Required Inspection Items Radio Management Panel Rolls Royce Restoration Reservoir Sampling Size Service Information Letter Shut off Valve Structure Repair Manual Structure Significant Item System Servicing To be determined Traffic Collision Avoidance System Trimmable Horizontal Stabilizer Table of Content Tire Pressure Indication System Temporary Protection System Temporary Revision Upper deck GLOSSARY

Page : 10/11

A330 Maintenance Schedule ULB : Underwater Locating Beacon VR : Vendor Recommendation VC : Visual Check VCC : Video Control Center VHF : Very High Frequency YE : Year EASA AD, FAA AD, CN : Task originated by an Airworthiness Directive. ALI : Task originated by Airworthiness Limitation Items document (ALS Part 2). ASM : Task originated by Ageing Systems Maintenance document (ALS Part 4–3). FAL : Task originated by Fuel Airworthiness Limitations document (ALS Part 5). ISB, VSB : Task originated by an Inspection Service Bulletin (ISB), Vendor Service Bulletin (VSB). SIL, AOT : Task originated by Service Information Letter (SIL), All Operator Telex (AOT). MRB : Task originated from the MRB Report. For tasks resulting from a system/power plant analysis, the three letters "MRB" are followed by the corresponding Functional Failure Effect category (5 – 9). 5 : Evident Safety 6 : Evident Operational 7 : Evident Economic 8 : Hidden Safety 9 : Hidden Non Safety CMP : Task originated by CMP (Configuration Maintenance and Procedures) AI/EA 5000. This document lists the standards for ETOPS. CMR : Task is a Certification Maintenance Requirement (ALS Part 3). Its interval cannot be escalated by an Operator. Cannot be deleted from operator maintenance program. MAN : Task originated by a Maintenance Advisory Notice (for PW engines). CPCP : Task originating from Corrosion Prevention and Control Program. ISSUE 10 AMENDMENT 01

GLOSSARY

Page : 11/11

A330 Maintenance Schedule SAMPLING PROGRAM A. INTRODUCTION The Sampling Program is designed to detect systematic deterioration caused by the environment and/or fatigue, on a group of aircraft selected from those which have the highest age within a considered fleet. The Sampling Program is applicable to both Fatigue Damage (FD) and Environmental Deterioration (ED) SSIs, where the deterioration, should it occur, is considered as being progressive with age or operating usage. SSIs which are susceptible to Accidental Damage (AD) are not considered for the Sampling Program. Structure inspections fall into the following 3 categories: 100% Fatigue tasks where calculation and/or test indicate a high fatigue sensitivity, are not selected for sampling. These tasks have a 100% threshold only. e.g. SSI 531154-01-2 Fatigue or corrosion tasks where accidental damage is likely, are not selected for sampling. These tasks have a 100% threshold only. e.g. SSI 534139-01-3 Corrosion tasks where in-service experience indicates that damage is likely are not selected for sampling. These tasks have a 100% threshold only. e.g. SSI 533191-01-1 100% + SAMPLING Fatigue tasks where calculation and/or test indicate a medium fatigue sensitivity, are selected for sampling. These tasks have a sampling threshold and a 100% threshold. All aircraft not inspected as sampling aircraft must be inspected at the 100% threshold. e.g. 533104-01-3 Corrosion tasks where in-service experience indicates that damage is not likely are selected for sampling. These tasks have a sampling threshold. All aircraft not inspected as sampling aircraft must be inspected at the 100% threshold (20 years). e.g. 545126-02-1 SAMPLING ISSUE 10 AMENDMENT 01 A330 – Sampling Program

Page 1

A330 Maintenance Schedule Fatigue tasks where calculation and/or test indicate a low fatigue sensitivity, are selected for sampling. These tasks have a sampling threshold only. e.g. 574804-02-4 Based on the results of Sampling Program inspections: – In case of findings, each operator should take appropriate corrective actions, such as change of program concept to 100%, decrease of interval, application of TPS etc.... – In case of no findings, the current inspection program continues to apply. B. SELECTION OF AIRCRAFT FOR SAMPLING PROGRAM For each operator, the Sampling Program inspections are to be performed on the oldest 1/5 of the operator's A330 aircraft. The oldest aircraft are defined as the aircraft with the highest age in years since their initial manufacturer's delivery date. For operators with more than one aircraft type in their fleet, e.g. A330 and A340, the Sampling Program aircraft must be determined per aircraft type, e.g. 1/5 of the oldest A330 aircraft + 1/5 of the oldest A340 aircraft. For operators with more than one weight variant group in their fleet, the Sampling Program aircraft have to be determined per weight variant group, e.g. 1/5 of the oldest Group 33A aircraft and 1/5 of the oldest Group 33B aircraft. If the 1/5 sample of the operators aircraft is not a whole number of aircraft, the number is to be decreased to the next lowest whole number. A minimum of one aircraft per operator must be selected for the Sampling Program. The maximum number of aircraft to be sampled per operator is 5 aircraft per aircraft type even if the total fleet size would lead to a higher number applying the 20% rule. NOTE: Operators operating the same aircraft type in similar operational conditions and having established common rules acceptable to each operators' Airworthiness Authority may combine their fleets to form one fleet for the Sampling Program. A minimum of one aircraft must be selected from each operator in the group, if not already selected by the above rule.

ISSUE 10 AMENDMENT 01 A330 – Sampling Program

Page 2

A330 Maintenance Schedule Any aircraft in a fleet is protected by the respective sample aircraft of this operator’s fleet. If a “non-sampling” aircraft would be integrated into a new operator’s fleet it could become a sampling aircraft. However, no retroactive maintenance is required i.e. all inspections are to be performed at their next due. Example: An aircraft which was not a sample A/C is 7 years old has been acquired by another operator. All inspections with an interval of 6 YE would be due at the next 6 YE check; which is 12 YE after entering service. Any significant changes to an operator's fleet will require a review of the Sampling Program aircraft. This includes buying and/or selling aircraft and retiring aircraft from the fleet. Operators may contact Airbus for advice in the selection of the Sampling Program aircraft. The momentary selected aircraft are as follows : Operator

MSN

WV REG Sampling A/C GROUP Vietnam Airlines 275 32A VN-A371 VN-A371 For A/C belong to the group 32E (VN-A376 MSN 943; VN-A377 MSN 962; VN-A378 MSN 1019; VNA379 MSN 1256; VN-A381 MSN 1266; VN-A383 MSN 946) all effect tasks are to be inspected at the Sample Threshold/Interval due to requirement of LESSOR C. ARRANGEMENT OF INSPECTIONS For the selected A/C, the inspections commence at the Sample Threshold and continue at each subsequent repeat interval. The selected Sampling Program aircraft are to be inspected at the Sample Threshold. The same aircraft are to be inspected at each subsequent repeat interval. NOTE: The 100% Threshold is the threshold for all aircraft not selected for sampling (Refer to the suitable example on following pages). D. SAMPLING PROGRAM ILLUSTRATIONS A chart presenting the way to deal with the sample, 100% threshold and interval is shown on the next page together with a set of illustrations showing the arrangement of Sampling Program inspections for some typical ISSUE 10 AMENDMENT 01 A330 – Sampling Program

Page 3

A330 Maintenance Schedule structure inspection tasks are shown on the following pages. The Sampling Program aircraft should first be selected before the subsequent planning of the SSI details:


Page 4



Page 5



Page 6



Page 7



Page 8



Page 9

A330 Maintenance Schedule OPERATIONAL PROGRAMMES: Dependent on the operational profile of an operator an AMS shall include following operational programmes: RVSM According to the AIRBUS MPD/MRB the RVSM capability is an inherent function of the basic design standard of the aircraft. Scheduled tasks necessary for these operations have been considered in the development of the MPD. Due to this no special RVSM programme needs to be introduced into this AMS as it shall include all applicable MPD tasks in any case. ALL WEATHER OPERATION CAT III According to the TCH’s MPD the CAT II/III capability is an inherent function of the basic design standard of the aircraft. Scheduled tasks necessary for these operations have been considered in the development of the MPDs. Due to this no special “All Weather Operation CAT III” programme needs to be introduced in this AMS as it shall include all applicable MPD tasks in any case. HIRF In the MRBR Appendix 9 the HIRF/Lightning related scheduled tasks are defined, which are also incorporated in the AIRBUS’s MPD Section 2 ATA 20. The AMS includes all HIRF tasks as published in the MRBR or MPD


MAINTENANCE CHECKS

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A330 Maintenance Schedule ETOPS MAINTENANCE PROGRAM All ETOPS tasks of the CMP AI/EA5000 maintenance procedures are marked with “NOTE: CMP TASK” in task description (ETOPS SCHEDULED CHECK REQUIREMENTS).

ETOPS SCHEDULED CHECK REQUIREMENTS ITEM

1

DESCRIPTION

CMP NUMBER

CMP INTERVAL

VNA TASK NUMBER

VNA INTERVAL

REFERENCE

APPLICABILITY

AVIONICS EQUIPMENT VENTILATION

CMP 21-2-0000-004

24 MO

212600-02-2

24 MO

212600-710-806

ALL

CMP 21-2-0000-001

2500 FH

212800-01-2

2500 FH

212800-710-804

ALL

CMP 21-2-0000-002

2500 FH

212800-02-2

2500 FH

212800-710-805

275, 294, 299, 366, 1256, 1266, 946

CMP 22-2-0000-001

42 MO

221000-01-2

42 MO

221000-710-801

ALL

OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION 2

LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING (FWD, AFT AND BULK) OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF ISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN CASE OF SMOKE WARNING

3

LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING (FWD, AFT AND BULK) OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD AIR VALVE IN CASE OF SMOKE WARNING

4

AUTOPILOT/FLIGHT DIRECTOR OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION


MAINTENANCE CHECKS

Page : 1/7

A330 Maintenance Schedule 5

INTEGRATED DRIVE GENERATOR SYSTEM DISCARD SCAVENGE FILTER AND DRAIN AND REPLENISH INTEGRATED DRIVE GENERATOR OIL SYSTEM NOTE : - REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL. - DO NOT PERFORM THE SERVICING ON BOTH IDG AT THE SAME TIME BUT ON ONE UNIT ONLY. SERVICING ON THE OTHER IDG TO BE PERFORMED AFTER 400FH. - IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE OTHER IDG.


CMP 24-2-0000-001

800 FH OR NOTE

MAINTENANCE CHECKS

242100-13-1

800 FH OR NOTE

121324-612-807 SIL SUN 236 SIL SUN 279 SIL SUN 346 SIL 24-049

ALL

Page : 2/7


INTEGRATED DRIVE GENERATOR SYSTEM

CMP 24-2-0000-001

800 FH OR NOTE

242100-13-2

800 FH

121324-612-807 SIL SUN 236 SIL SUN 279 SIL SUN 346 SIL 24-049

ALL

CMP 24-2-0000-011

50 FH

242400-01-3

TERMINAL CHECK

242400-710-801

ALL

CMP 24-2-0000-010

50 FH

APPLY TASK 242400-01-3

TERMINAL CHECK

242400-710-801

APPLY TASK 242400-01-3

CMP 24-2-0000-005

42 MO

242400-03-2

42 MO

242400-710-803

ALL

DISCARD SCAVENGE FILTER AND DRAIN AND REPLENISH INTEGRATED DRIVE GENERATOR OIL SYSTEM NOTE : - REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL. - DO NOT PERFORM THE SERVICING ON BOTH IDG AT THE SAME TIME BUT ON ONE UNIT ONLY. SERVICING ON THE OTHER IDG TO BE PERFORMED AFTER 400FH. - IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE OTHER IDG.

7

AC EMERGENCY GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM

8

AC EMERGENCY GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM

9

AC EMERGENCY GENERATION OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS


MAINTENANCE CHECKS

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AC EMERGENCY GENERATION

CMP 24-2-0000-002

24 MO OR 4000 FH

242400-04-2

24 MO OR 4000 FH

242400-710-806

ALL

CMP 24-2-0000-003

650 FH

242800-01-2

650 FH

242800-710-801

ALL

CMP 24-2-0000-007

VR

243852-01-2

1 YE

243852-280-801 SIL SAFT 0398 SIL 24-062

ALL

CMP 25-2-0000-002

8 DY

255200-01-1

WEEKLY CHECK

255200-210-801

ALL

CMP 25-2-0000-002

8 DY

255300-01-1

WEEKLY CHECK

255300-210-801

ALL

CMP 24-2-0000-006 CMP 36-2-0000-001

24 MO

262100-14-1

24 MO

262100-710-811

ALL

CMP 26-2-0000-001

1A

262200-01-3

1A

262200-710-801

ALL

OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC CONNECTION 11

STATIC INVERTER AC GENERATION OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS SUPPLY

12

BATTERY DC GENERATION REMOVE BATTERY 3 (APU) FOR OVERHAUL.

13

LOWER DECK FORWARD CARGO COMPARTMENT VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS, PROTECTION PLATES, DECOMPRESSION PANELS, CENTER LINE COVER PLATES AND ACCESS DOORS. (NOTE 11)

14

LOWER DECK AFT CARGO COMPARTMENT VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS, PROTECTION PLATES, DECOMPRESSION PANELS, CENTER LINE COVER PLATES AND ACCESS DOORS. (NOTE 11)

15

ENGINE FIRE EXTINGUISHING OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW FUNCTION

16

APU FIRE EXTINGUISHING OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM


MAINTENANCE CHECKS

Page : 4/7


APU FIRE EXTINGUISHING

CMP 26-2-0000-002

42 MO

262200-03-2

42 MO

262200-710-806

ALL

CMP 28-2-0000-005

42 MO

262200-06-1

42 MO

262200-710-805

ALL

CMP 28-2-0000-004

36 MO OR 4800 FH

262200-07-3

36 MO OR 4800 FH

262200-710-803

ALL

CMP 26-2-0000-003

4C

262241-03-1

4C

262241-280-803

ALL

CMP 28-2-0000-010

2 MO NOTE 1

281100-02-1

2 MO NOTE 1

123228-281-803

ALL

CMP 28-2-0000-013

7 DY NOTE 1

281100-10-1

TERMINAL CHECK

123228-281-810

ALL

CMP 28-2-0000-008

1A

282200-07-4

1A

123228-281-807

ALL

CMP 28-2-0000-012

4600 FH

282200-08-1

4600 FH

282200-710-808

ALL

OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 18

APU FIRE EXTINGUISHING OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION

19

APU FIRE EXTINGUISHING OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA MCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF, 6WF)

20

APU FIRE EXTINGUISHING FUNCTIONAL TEST OF APU FIRE EXTINGUISHER PRESSURE SWITCH SETTING

21

TANKS OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER FROM TRIM TANK AND TRIM VENT SURGE TANK

22

TANKS OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS

23

APU FUEL PUMP SYSTEM OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO DRAIN ANY ACCUMULATED WATER.

24

APU FUEL PUMP SYSTEM OPERATIONAL CHECK OF RELAYS 12QC AND 14QC


MAINTENANCE CHECKS

Page : 5/7


CROSSFEED SYSTEM

CMP 28-2-0000-001

36 MO

282300-02-1

36 MO

282300-710-803

ALL

CMP 32-2-0000-001

4A

324000-04-1

4A

324400-710-802

ALL (ALL POST 46321)

CMP 36-2-0000-003

20000 FH

361100-03-1

20000 FH

361153-720-808

ALL

CMP 36-2-0000-002

36 MO

361100-05-1

36 MO

361100-710-815

ALL

CMP 36-2-0000-004

50 MO OR 3600 FC

361200-01-3

3600 FC

361200-710-802

ALL

CMP 49-2-2003-002

1000 AH NOTE

493100-01-3

1000 AH NOTE

493241-210-801

ALL

CMP 49-2-2003-003 CMP 49-2-2003-004

500 AH

499100-01-2

WEEKLY CHECK

499141-210-801

ALL

OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL MOTORS 26

BRAKES AND WHEELS OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE

27

ENGINE AIR BLEED VALVE FUNCTIONAL CHECK OF OVERPRESSURE VALVE

28

ENGINE BLEED AIR SUPPLY OPERATIONAL CHECK OF MANUAL BLEED SHUT OFF.

29

APU BLEED AIR VALVE AND CROSSBLEED OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE

30

APU FUEL DISTRIBUTION VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR BUTTON ON FUEL FILTER NOTE : - TASK TO BE ACCOMPLISHED AT 150FH, 400FH, AND 800FH AFTER AIRCRAFT DELIVERY. THEREAFTER EVERY 1000 AH. - TASK TO BE ACCOMPLISHED AT 150FH AND 400FH AFTER MAJOR TANK REPAIR. THEREAFTER EVERY 1000AH.

31

APU OIL SYSTEM CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON - ON LUBE FILTER - ON GENERATOR SCAVENGE FILTER.


MAINTENANCE CHECKS

Page : 6/7


HIGH PRESSURE TURBINE GROUP

CMP 72-2-0204-007

NOTE

725200-P3-1

NOTE

VSB PW4G-100-72195

ENG PRE SB PW 72206

CMP 72-2-0204-009

1000 FC

771300-P1-1

1000 FC

732134-280-801 MAN PW4G-100-2-00

ALL

BORESCOPE INSPECTION OF SECOND STAGE HIGH PRESSURE TURBINE VANES NOTE: - REFER TO VSB PW4G-100-72-195 FOR THRESHOLD AND INTERVAL

ENGINE PRESSURE RATIO (EPR) INDICATING SYSTEM INSPECTION AND CLEANING OF CONDENSATION TRAP ASSEMBLIES (WATER TRAPS), FOR OBSTRUCTIONS OR BLOCKAGE 33

The ETOPS Maintenance procedures are prescribed in the A330 ETOPS Maintenance Procedures Manual. In order to minimize the risk of a dual engine failure event which is related to a common source, maintenance procedures must be established to preclude simultaneously maintenance activities on both engines, on identical components, of ETOPS-critical systems are listed in A330 ETOPS Significant Systems List (below)


MAINTENANCE CHECKS

Page : 7/7

A330 ETOPS Significant Systems List The following list defines the A330 systems / functions which are ETOPS significant, as per the following criteria: All Systems in the list below should be tracked as "ETOPS Significant" in the Reliability Program and may be reported as "ETOPS relevant" in case of failure Systems marked as "dual" should be treated as "ETOPS Parallel Systems" for dual maintenance (Refer to enclosed Dual Maintenance Matrix for additonal guidelines)

ATA Chapter

ATA Sect. / Descr.

21-26

Avionics Equipment Ventilation

ETOPS Significant Functions of the selected system(s) Ventilation of Avionic system

Rationale for selecting ETOPS Significant Systems/Functions

Regulatory Reference EASA / FAA

Dual

Integrity of the avionic system during an ETOPS diversion

Additional information on typical "ETOPS Relevant" events to be reported Complete loss of avionics cooling

A330 Pax: Cabin Air Distribution and Recirculation 21-21 A330-200F: Main Deck and Courier Ventilation 21-22

Cockpit Air Ventilation

21-31

Pressure Control and Monitoring

21-51

Flow Control and Indicating

21-52

Air Conditioning (Packs)

21-53

Pack Control and Indicating

21-63

Cockpit and Cabin Temperature Control

22-10

Autopilot

22-30

Autothrust

21 - Air Conditioning

22 - Auto Flight

23 - Communication

24 - Electrical Power

- Aircraft pressurization capability - Cabin and cockpit environmental control capability (temperature and ventilation)

Autopilot function

Autopiloti s cons idere d asi mportant to ma i nta i n accepta bl e p il ot workload over an ETOPS diversion.

Autothrust function

Autothrust is considered as important to maintain acceptable pilot workload over an ETOPS diversion.

Fuel prediction functions

- FMS fuel prediction functions are considered more important for management of an ETOPS flight (provide additional in flight fuel monitoring function). - Specific FMS functions used for diversion decision making (ETP, EEP,…). See 22-10

Flight Management System

22-81

Flight Control Unit (FCU)

Interface with Autopilot

22-82

Multipurpose Control and Display Unit (MCDU)

Interface with FMS

HF System

23-28

SATCOM System

23-73

24-21

One HF (voice) is required for all ETOPS flights.

SATCOM voice function

One SATCOM (voice) is required for ETOPS beyond 180 min.

CIDS (for A/C not fitted with SDCU)

Cargo Fire Detection function

Spurious warning can cause diversion.

AC Main Generation

AC Main generation function(s)

- The 2 IDGs and associated GCU, the APU Gen and associated GCU and the CSM/G constitute 4 independent electrical power sources for ETOPS (including ETOPS beyond 180 min.)

AC Auxiliary Generation

24-24

AC Emergency Generation

- Loss of pressurization - Loss of temperature control - Loss of ventilation - Loss of pack

AC Auxiliary generation function AC Emergency Generation function

AMC 20-6 Rev 2 Ch II.7.5 and Ch II.7.7 / AMC 20-6 Rev 1 §8.b.5 and §8.b.7 / FAR §K25.1.2

See 22-70

HF voice function

24-23

AMC 20-6 Rev 2 Ch II.8.3.(v) and Ch II.8.3.(vi) / AMC 20-6 Rev 1 §8.c.8 and §8.c.9 / FAR §K25.1.2

X

22-70

23-11

- Minimize occurrence of depressurization which leads to an ETOPS diversion at depressurized FL. It has subsequent impact on fuel consumption and exposure to more severe outside atmospheric conditions (icing). - Minimize occurrence of loss of cockpit and cabin or courier area temperature and ventilation control during an ETOPS diversion.

X

Loss of system / function

X AMC 20-6 Rev 2 Ch II.7.7 / AMC 20-6 Rev 1 §8.b.7 / FAR §K25.1.2 AMC 20-6 Rev 2 Ch III.7.2.3.(ii) / AMC 20-6 Rev 1 §10.d.3.(ii) / FAR §121.122 AMC 20-6 Rev 2 Ch II.8.3.(iv) / AMC 20-6 Rev 1 §8.c.6 / FAR §K25.1.2

Non recoverable total loss of long-range voice communication in flight

- Failure of smoke/fire detection (except lavatories), spurious warning X

AMC 20-6 Rev 2 Ch II.7.8 / AMC 20-6 Rev 1 §8.b.8 / FAR §K25.1.3.b

Failure of IDG(s), APU Gen, CSM/G X X

Page 1 of 4


ATA Chapter

26 - Fire Protection

ATA Sect. / Descr.

26-12

Engine Fire and Overheat Detection

26-13

APU Fire and Overheat Detection

26-15

ETOPS Significant Functions of the selected system(s)


Engine Fire and Overheat Detection function

Spurious warning can cause IFSD (diversion).

APU Fire and Overheat Detection function.


Avionics Compartment Smoke Avionics Compartment Fire and Detection Overheat Detection function.

Dual

LDCC Smoke Detection



26-19

MDCC Smoke Detection (A330-200F only)



26-23

LDCC Fire Extinguishing

Cargo Fire Extinguishing function

The cargo fire protection time is an ETOPS diversion time limitation.

28-21

Engine Feed Fuel Pump System

Provide adequate fuel pressure and flow at engine inlet

Additional information on typical "ETOPS Relevant" events to be reported

X

- Failure of smoke/fire detection (except lavatories), spurious warning - Failure of cargo fire suppression system - Fire occurrence (detected or undetected)

AMC 20-6 Rev 2 Ch II.8.3.(iv) / Spurious warning can cause diversion.

26-16

AMC 20-6 Rev 1 §8.c.6 / FAR §K25.1.2

- Fuel pump(s) failure - Fuel leaks

Ensure fuel availability, at adequate fuel pressure and flow at X engine inlet in case of ETOPS diversion.

28-22

APU Fuel System

Provide fuel to APU

In-flight APU start and run reliability are more important for ETOPS flights.

28-23

Cross-feed System

Cross-feed function

Ensure fuel availability to complete a diversion in case of fuel system or engine failure.

28-40

Fuel Quantity Indicating

Provide accurate fuel quantity and fuel temperature information

Fuel quantity information is considered as more important for ETOPS flight (for in flight fuel monitoring). Fuel temperature indication is more important for polar flights.

28 - Fuel


- Trapped fuel - Over spillage FAR §K25.1.4.a

X

Failed APU start due to no fuel feed

Failed Crossfeed Valve

AMC 20-6 Rev 2 Ch II.7.10 / AMC 20-6 Rev 1 §8.b.9 / FAR §K25.1.4.a

FQI failure

29-11 29 - Hydraulic Power

29-12

Engine Driven Pump (Green/Blue/Yellow)

Provide hydraulic power to Green/Blue/Yellow Hydraulic System

Minimize loss of hydraulic system(s)

AMC 20-6 Rev 2 Ch II.7.6 / AMC 20-6 Rev 1 §8.b.6

Hydraulic system(s) failure (low level, low X pressure, overheat)

29-13

30-11

Wing Ice Protection

30-21

Engine Air Intake Ice Protection

30 - Ice & Rain Protection

34 - Navigation

Loss of wing anti-icing capability

Provide anti-ice protection capability 30-31

Probe Ice Protection

30-42

Windshield Anti-Icing and Defogging

34-41

Weather Radar System

Airframe and propulsion ice protection systems must provide adequate capability for ensuring a safe ETOPS diversion and landing in icing conditions.

AMC 20-6 Rev 2 Ch II.7.7.(iii) and Ch II.7.7.(xiii) / AMC 20-6 Rev 1 §8.b.7.(iii) and §8.b.7.(xiii)

X

Loss of air intake anti-icing capability

X

Loss of probe heating capability in more than one system Failure of cockpit window anti-icing

Weather radar function

Weather radar considered as more important to conduct an ETOPS diversion.

AMC 20-6 Rev 2 Ch II.7.7 / AMC 20-6 Rev 1 §8.b.7.(iii)

Weather radar failure

Page 2 of 4


ATA Chapter

ATA Sect. / Descr.

35-10 35 - Oxygen (A330-200F only)

Crew Oxygen (A330-200F only)

ETOPS Significant Functions of the selected system(s) Provide oxygen to flight crew

Passenger Oxygen (A330-200F only)

Provide oxygen to courier area occupants

Provide oxygen to the courier area occupants during the whole time of a diversion in case of fire in the main deck cargo compartment.

36-11

Engine Bleed Air Supply System

Provide pressure and temperature regulated airflow

- Provide air to minimize occurrence of depressurization. - Provide air at adequate temperature to maintain adequate cockpit and cabin temperature during an ETOPS diversion. Provide air to wing ice protection systems.

- Provide back-up air-flow - Cross bleed function

- APU Bleed more important for ETOPS to pressurize the aircraft during an ETOPS diversion following dual engine Bleed failure. - Crossbleed system more important to maintain pressurisation, temperature control and wing anti-ice capability in ETOPS diversion scenario.

Leak detection function

Leak detection can affect the wing anti-ice capability during an ETOPS diversion.

Loss of oxygen supply to one or several flight crew members Loss of oxygen supply to one or courier area occupants

X

Loss of bleed air system(s)

X

Loss of APU bleed

AMC 20-6 Rev 2 Ch II.8.3.(v) and Ch II.8.3.(vi) / AMC 20-6 Rev 1 §8.c.8 and §8.c.9

36-22

Leak Detection

49-10

APU Power Plant

X

49-20

APU Engine

X

49-30

APU Engine Fuel and Control

49-40

APU Ignition and Starting

49-51

APU Air Bleed

49-60

APU Engine Controls

49-70

APU Indicating

49-90

APU Oil System

71-50

Electrical Harness

74 75 76 77 78-30 79

All items related to engine ATA chapters are ETOPS Significant except ATA 71 other than 7150, ATA 78 other than 78-30, and ATA 80.

Loss of leak detection system without warning

X All APU functions necessary to: - Start the APU in-flight after cold soak Preclude APU in-flight shutdown Provide pressurized air

- In-flight APU start and run reliability more important during ETOPS flight. - APU Bleed more important for ETOPS to pressurize the aircraft during an ETOPS diversion following dual engine bleed failure.

Additional information on typical "ETOPS Relevant" events to be reported

AMC 20-6 Rev 2 Ch II.7.6 / AMC 20-6 Rev 1 §8.b.6

APU Bleed Air Supply and Cross Bleed systems

AMC 20-6 Rev 2 Ch II.7.4 / AMC 20-6 Rev 1 §8.b.4 / FAR §K25.1.4.b

X X

- Uncommanded shut down - APU failure - Significant overspeed / over EGT - Uncontained burst (compressor / turbine cooling fan) - No relight in flight - Loss of APU bleed

X - Severe fuel / oil leak in the APU compartment X

73

Non ATA related

Dual

36-12

72

70 to 80 - Engine ATA


Provide oxygen to the flight crew during the whole time of a diversion in case of fire in the main deck cargo compartment.

35-20

36 - Pneumatic

49 - Auxiliary Power Unit


All engine's functions necessary to: Preclude In-flight shutdown - Obtain and control desired thrust - Provide power to accessories

Minimize occurrence of In-Flight Shut Down (IFSD), i.e. when an engine ceases to function (when the airplane is airborne) and is shutdown, whether self induced, flight crew initiated or caused by an external influence. Engine failures on ground (e.g. during taxi), also not counted as IFSDs, are to be reviewed and reported as well. IFSD examples: flameout, internal failure, flight crew initiated shutdown, foreign object ingestion, icing, inability to obtain or control desired thrust or power, and cycling of the start control, however briefly, even if the engine operates normally for the remainder of the flight. Although not counted as IFSDs, airborne cessation of the functioning of an engine when immediately followed by an automatic engine relight and when an engine does not achieve desired thrust or power are to be reviewed and reported in the

Severe chaffing

AMC 20-6 Rev 2 Appendix 1 / AMC 20-6 Rev 1 Appendix 1 / FAR K25.2.2

- Uncommanded power loss / changes - Nacelle fire warning / fuel leaks X - Inability to control the engine power - Surges - Loss of engine parameters sensing/indicating - Severe oil leak

- Aborted Take-Off - Diversion - Air turn back

Page 3 of 4

Dual Maintenance Matrix This matrix provides additional guidance for dual maintenance performed on ETOPS Significant Systems identified as "dual". Category (1) X Simultaneous maintenance actions on the same element of identical parallel ETOPS Significant Systems (e.g. maintenance on IDG1 and IDG2) must comply with dual maintenance considerations as per EASA AMC 20-6, EASA Part 145.A.65, FAA AC 120-42B §301.(d). Category (2) X Simultaneous maintenance actions on "substantially similar" ETOPS Significant Systems (i.e. engine driven/mounted components on both engines, e.g. maintenance on IDG1 and EDP2 (Green or Yellow)) must comply with dual maintenance considerations as per FAA AC 120-42B §301.(d). Category (3) X Simultaneous maintenance actions on redundant systems not falling in category 1 above (e.g. maintenance on IDG and APU GEN) should comply with dual maintenance considerations.

Maintenance Action on

ATA 21 - Air Conditioning

22 - Auto Flight

Pack 1 Pack 2

FMS MCDU

ATA 24 - Electrical Power IDG 1

IDG 2

CSM/G

ATA 26 - Engine Fire and Overheat Detection Detection Detection Function Eng 1 Function Eng 2

ATA 28 - Fuel

APU Fire Main Pumps Main Pumps Detection Left Right N/A N/A N/A

ATA 30 - Ice and Rain Protection

ATA 29 - Hydraulic Power APU

EDP1

EDP1

EDP2

Green N/A

Green N/A

Yellow N/A

Eng 1 Eng 2 Probes

ATA 36 Pneumatic

ATA 49 APU

Bleed 1 Bleed 2

ATA 70 to 80 Engine Eng 1 Eng 2

Pack 1

N/A

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

EDP2 Blue N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

Pack 2

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

FMS

N/A

N/A

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

MCDU

N/A

N/A

N/A

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

IDG 1

N/A

N/A

N/A

N/A

N/A

X

X

N/A

X

X

N/A

X

X

N/A

X

X

X

N/A

X

N/A

N/A

X

X

N/A

X

IDG 2

N/A

N/A

N/A

N/A

X

N/A

X

X

N/A

X

X

N/A

X

X

X

X

N/A

X

N/A

N/A

X

N/A

X

X

N/A

CSM/G

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

X

N/A

N/A

N/A

N/A

X

X

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

X

ATA 21 - Air Conditioning

22 - Auto Flight

ATA 24 - Electrical Power

ATA 26 - Engine Fire and Overheat Detection

ATA 28 - Fuel

Detection Function Eng 1 Detection Function Eng 2 APU Fire Detection Main Pumps Left Main Pumps Right

N/A

X

N/A

N/A

X

N/A

X

X

N/A

N/A

N/A

N/A

X

N/A

N/A

N/A

X

N/A

N/A

X

X

X

N/A

N/A

N/A

N/A

X

X

X

N/A

N/A

X

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

X

X

X

N/A

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

X

N/A

X

N/A

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

X

N/A

X

N/A

N/A

N/A

X

N/A

N/A

X

X

N/A

N/A

X

N/A

N/A

X

X

N/A

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

APU

N/A

N/A

N/A

N/A

X

X

X

N/A

N/A

N/A

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

EDP1 Blue

N/A

N/A

N/A

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

X

X

N/A

X

N/A

N/A

X

N/A

N/A

X

EDP1 Green

N/A

N/A

N/A

N/A

X

X

X

N/A

X

X

N/A

X

X

X

N/A

X

X

N/A

X

N/A

N/A

X

X

N/A

X

EDP2 Green

N/A

N/A

N/A

N/A

X

X

X

X

N/A

X

X

N/A

X

X

X

N/A

X

X

N/A

N/A

X

N/A

X

X

N/A

EDP2 Yellow

N/A

N/A

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

X

X

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

Eng 1

N/A

N/A

N/A

N/A

N/A

N/A

N/A

ATA 29 - Hydraulic Power

ATA 30 - Ice and Rain Protection

N/A

X

Eng 2

N/A

N/A

N/A

X

N/A

Probes

N/A

N/A

N/A

N/A

N/A

N/A

Bleed 1

N/A

N/A

N/A

N/A

N/A

Bleed 2

N/A

N/A

N/A

N/A

X

APU

N/A

N/A

N/A

N/A

X

X

Eng 1

N/A

N/A

N/A

N/A

N/A

Eng 2

N/A

N/A

N/A

N/A

X

N/A N/A

N/A X

X N/A

N/A

X

X N/A

N/A

X

X

N/A

N/A

X

N/A

X

X

X

N/A

N/A

N/A

N/A

N/A

X

X

X

N/A

N/A

X

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N/A

N/A

N/A

N/A

X

N/A

N/A

X

X

N/A

N/A

X

N/A

N/A

N/A

N/A

X

X

X

N/A

X

X

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X

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N/A

X

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X

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N/A

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X

X

N/A

N/A

N/A

N/A

N/A N/A

X N/A

N/A X

X

N/A

N/A

N/A

N/A

N/A

N/A

X

X

N/A

N/A

N/A

X

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N/A

N/A

X

X

N/A

N/A

N/A

X

N/A X

X

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X

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N/A

N/A

X N/A

N/A N/A

N/A X

X N/A

N/A

N/A

N/A

N/A

N/A

X

X

N/A

X

X

N/A

X

X

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X

X

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X

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X

N/A

N/A

X

N/A

N/A

X

N/A

N/A

X

N/A

ATA 36 - Pneumatic

ATA 49 - APU

ATA 70 to 80 - Engine


A330 SPECIAL INSPECTION TASKS STT 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

DESCREPTION Inspection after Hard/Overweight Landing Inspection After Landing Gear Extension at More than the Gear Down Limiting Speed. Inspection After Flap/Slat Limiting Speed Exceeded Inspection of the Aircraft after a Bird or a Hail Strike Inspection of the Aircraft after a Tire Burst or Tread Throw or Wheel Failure Inspection After Brake Overheat Inspection after Flight in Excessive Turbulence or in Excess of VMO/MMO Inspection after Lightning Strike Inspection after Engine Bird Strike or Slush Ingestion Inspection after Tail Runway impact Inspection after NLG Towing Overload or Overrun Inspection of the Nose Landing Gear after a NLG Steering Angle of more than 95 Inspection after Leaving a Runway or a Taxiway Inspection after Flight through Dust Storm or Dust contamination on Ground Inspection after Flight through Volcanic Ash or Volcanic Ash contamination on Ground Inspection after Engine Failure Inspection after Impact on Engine Cowls Inspection after Spillage Inspection after Abnormal Pax/Crew Door Movement. Inspection after Engine Windmilling (after Engine In-Flight Shut-Down) Inspection after Overweight Taxiing Inspection after Very High Winds on Ground Inspection after Work On System Electrical Installation Inspection after flight with high lateral loads

ISSUE: 10 AMENDMENT: 01

AMM REFERENCE TASK 05-51-11-200-802 TASK 05-51-12-200-801 TASK 05-51-13-200-801 TASK 05-51-14-200-801 TASK 05-51-15-200-801 TASK 05-51-16-200-801 TASK 05-51-17-200-801 TASK 05-51-18-200-801 TASK 05-51-19-200-801 TASK 05-51-21-200-801 TASK 05-51-22-200-801 TASK 05-51-23-200-801 TASK 05-51-24-200-801 TASK 05-51-25-200-802 TASK 05-51-25-200-803 TASK 05-51-26-200-801 TASK 05-51-27-200-801 TASK 05-51-28-200-801 TASK 05-51-29-200-801 TASK 05-51-34-200-802 TASK 05-51-41-200-801 TASK 05-51-42-200-801 TASK 05-51-43-700-801 TASK 05-51-44-200-801

Page 1


PROCEDURES FOR PARKING AND STORAGE OF THE AIRCRAFT Generally, when an aircraft is parked or stored, the procedures and accompanying maintenance practices for short term parking, extended parking or storage, which ever apply, need to be performed in accordance with the A330 AMM chapter 10. In addition, the following rules apply. A. The aircraft is parked / stored and does not remain in airworthy condition: 1. All maintenance actions described in the A330 maintenance program, which become due during the parking- / storage-period because of an applicable calendar limit, do not need to be performed at the moment they become due. This is valid for e.g. the Daily Check, a letter-check for which a calendar limit applies and the Outstanding Works with a calendar interval. However, each scheduled maintenance task of the A330 maintenance program, which becomes due during the period the aircraft is parked / stored, should be performed once at the moment the aircraft is prepared for it’s return to service. E.g.: In case a letter-check interval includes a calendar-limit, several checks might become due during the period the aircraft is stored. Some tasks might return in each of these subject checks. Each of these tasks needs to be performed only once during the preparation of the aircraft for its return to service. 2. Each engineering order will be separately evaluated in order to decide on whether it will be accomplished during the parking- / storage-period or at the moment the aircraft is prepared for its return to service. 3. Each AD, which becomes due during the parking- / storage-period, will generally be performed before the due date. However, when it would be impossible to perform the AD due to the parking- / storage-conditions, VNA agrees to have the AD performed at the moment the aircraft is prepared for its return to service. This only on condition that the operator gets the approval from its Civil Aviation Authorities to postpone the performance of the subject AD to that moment.


Page 1


4. In case the aircraft is stored for a period of several months, an engineering judgement needs to be made concerning the impact of the environmental conditions,valid during the storage-period, on the calendar-limit for major checks like the C-check. B. The aircraft is parked / stored and has to remain in airworthy condition: 1. All maintenance actions, described in the A330 maintenance program, which become due during the parking- / storage-period, need to be performed at the moment they become due. 2. No attention will be given to the parking- / storage-condition of the aircraft regarding the performance of engineering orders. 3. Each AD, which becomes due during the parking- / storage-period, will be performed before the due date. 4. In case the aircraft is stored for a period of several months, an engineering judgement needs to be made concerning the impact of the environmental conditions,valid during the storage-period, on the calendar-limit for major checks like the C-check.


Page 2


REQUIRED INSPECTION ITEMS REQUIRED INSPECTION ITEMS (RIIs) Tasks as RIIs. include those tasks that could result in a failure, malfunction, or defect that endangers the safe operation of the aircraft if the task is not completed properly or if operators use improper parts or material. If other persons perform maintenance task, operators may authorize them to accomplish their RII requirement, provided that manual satisfies the regulatory requirements a. List of Other Persons. Operator’s manual must include a list of persons with whom operators have arranged for the performance of any required inspections both within their organization and within other organizations that perform maintenance on their behalf. This listing must include a designation by occupational title of the personnel authorized to perform each required inspection. b. Certification. Operators grant an RII authorization to must hold an appropriate airman’s certificate. This is an air carrier qualification requirement; the individual does not exercise that certificate when accomplishing the RII. Operators must formally notify each of these individuals of their RII authorization as well as its scope. c. RII Requirements. Operators should clearly identify RII requirements on work forms, job cards, engineering orders, etc., or by any other method consistent with their maintenance program. A primary concept of the RII function is to prevent any person who performs any item of work from performing any required inspection of that work. Therefore, it is important that operators identify RIIs whenever possible so that everyone knows that an RII is required. d. Standards and Limitations. Operators must set procedures, standards, and limits necessary for required inspections and acceptance or rejection of the RII. Operators should have those procedures, standards, and limits necessary for the accomplishment of required inspections. Operators must also have those procedures, standards, and limits necessary for the acceptance or rejection of each of RIIs. e. Procedures. Operators’ manual must include procedures to ensure that you perform and complete all required inspections before releasing the aircraft to service. Tasks required RIIs will be noted as RII tasks.


Page 1

RII LIST

TASK NUMBER

ITEM

272149-01-1

DESCRIPTION

RUDDER MECHANICAL CONTROL

REFERENCE

APPLICABILITY

272149-200-801

275, 294, 299, 366

272451-200-801

275, 294, 299, 366

292452-960-801

ALL

321111-920-801

ALL

322111-920-801

ALL

341100-170-801 SIL 34-084

ALL

341100-790-801

ALL

341100-170-804 SIL 34-084

ALL

341100-170-803 SIL 34-084

275, 294, 299, 366

FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR WORKSHOP CHECK

1 272400-05-2

RUDDER HYDRAULIC ACTUATION REMOVE RUDDER SERVO CONTROL FOR WORKSHOP CHECK OF INTERNAL SEALS

2 292400-04-1

RAM AIR TURBINE REMOVAL OF RAM AIR TURBINE (RAT) FOR OVERHAUL. NOTE: - FIT A RAT THAT HAS NOT ACCUMULATED 20 YE SINCE LAST OVERHAUL.

3 321100-01-1

MAIN GEAR SPECIAL DETAILED INSPECTION (OVERHAUL) OF MLG (OFF AIRCRAFT).

4 322100-02-1

NOSE GEAR SPECIAL DETAILED INSPECTION (OVERHAUL) OF NLG (OFF AIRCRAFT).

5 341300-03-1

AIR DATA FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES NOTE: - THIS TASK PRECLUDES TASK 341300-04-1.

6 341300-04-1

AIR DATA

341300-06-1

LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS AIR DATA

7

CLEANING OF 1 OUT OF 3 PITOT PROBES. NOTE: TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3.

8 342100-01-1

STANDBY ALTITUDE AND AIRSPEED DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS NOTE: - THIS TASK PRECLUDES TASK 342100-02-1.

9 342100-02-1

STANDBY ALTITUDE AND AIRSPEED

341100-790-802

275, 294, 299, 366

342200-01-1

LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)

342225-170-801 SIL 34-084

MSN 943, 962, 1019, 1256, 1266, 946

342225-790-801

MSN 943, 962, 1019, 1256, 1266, 946

523100-720-801

ALL

10

DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS NOTE: - THIS TASK PRECLUDES TASK 342200-02-1.

11 342200-02-1

LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS

12 523100-02-1

13

INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)

FWD CARGO COMPARTMENT DOOR FUNCTIONAL CHECK OF : - LATCHING AND LOCKING HANDLE FORCES, - OVERCENTER POSITIONS, - WEAR OF LATCHING AND LOCKING MECHANISM, - ADJUSTMENT OF INTERLOCK MECHANISM.

RII LIST

ITEM

TASK NUMBER

523200-02-1

DESCRIPTION

AFT CARGO COMPARTMENT DOOR

REFERENCE

APPLICABILITY

523200-720-801

ALL

545118-200-815

275, 294, 299, 366

545118-200-815

MSN 943, 962, 1019, 1256, 1266, 946

545118-200-817

ALL

545117-200-814

ALL

545117-200-813

275, 294, 299, 366

545117-200-813

MSN 943, 962, 1019, 1256, 1266, 946

545117-200-818

ALL (ALL A330-200 POST 43271)

545117-230-801

ALL

FUNCTIONAL CHECK OF : - LATCHING AND LOCKING HANDLE FORCES, - OVERCENTER POSITIONS, - WEAR OF LATCHING AND LOCKING MECHANISM, - ADJUSTMENT OF INTERLOCK MECHANISM.

14 545101-02-1

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH THE FWD ENGINE MOUNT FITTING, HOLES AND SPOTFACES.

15 545101-02-2

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH THE FWD ENGINE MOUNT FITTING, HOLES AND SPOTFACES.

16 545102-05-1

PYLON BOX DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT RIB 8C

17 545170-02-1

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES, LINKS AND BOLTS AT RIB 12 (4 PLACES PER PYLON)

18 545174-04-1

PYLON TO WING FITTING DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING AND LINKS AT RIB 18A

19 545174-04-2


20 545180-03-2

PYLON TO WING FITTING DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON)

21 545180-04-6

PYLON TO WING FITTING SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON)

22 712101-03-1

MAIN STRUCTURE

712111-220-801

ALL

712106-01-1

DETAILED INSPECTION OF FORWARD ENGINE MOUNT. MAIN STRUCTURE

712111-280-801

ALL

712201-03-1

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT. MAIN STRUCTURE

712211-220-801

ALL

712204-02-1

DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. MAIN STRUCTURE

712211-220-802

ALL

723100-920-801

ALL

23

24

25

DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFE LINK NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH

26 723100-P3-1 27

PYLON TO WING LINKS

LOW PRESSURE COMPRESSOR GROUP DISCARD FAN HUB AND LPC DRUM ROTOR

RII LIST

ITEM

TASK NUMBER

723112-P1-1

DESCRIPTION

LOW PRESSURE COMPRESSOR (LPC) LUBRICATION OF THE 1ST STAGE LOW PRESSURE COMPRESSOR (LPC) BLADE ASSEMBLY (FAN BLADE) ROOT NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE.

28

REFERENCE

ALL

723200-P1-1

LPC / LPT COUPLING GROUP

723200-920-801

ALL

723500-P1-1

DISCARD LPC/LPT COUPLING HIGH PRESSURE COMPRESSOR (HPC)

723500-920-801

ALL

720000-290-833

ALL

720000-290-835

ALL

725200-920-801

ALL

VSB PW4G-100-72-195

ENG PRE SB PW 72206

725300-920-801

ALL

29

30 724100-P1-1

DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR DIFFUSER, COMBUSTION & TURBINE NOZZLE GROUP BORESCOPE INSPECTION OF INNER AND OUTER COMBUSTION CHAMBER ASSEMBLIES AND FIRST STAGE VANES

31 725200-P1-1

HIGH PRESSURE TURBINE GROUP BORESCOPE INSPECTION OF THE FIRST AND SECOND STAGE HIGH PRESSURE TURBINE BLADES

32 725200-P2-1


725200-P3-1

DISCARD LIFE LIMITED PARTS OF HP TURBINE HIGH PRESSURE TURBINE GROUP

33

BORESCOPE INSPECTION OF SECOND STAGE HIGH PRESSURE TURBINE VANES NOTE: - REFER TO VSB PW4G-100-72-195 FOR THRESHOLD AND INTERVAL

34 725300-P1-1 35

APPLICABILITY

710000-640-801 MAN PW4G-100-1-99

LOW PRESSURE TURBINE GROUP DISCARD LIFE LIMITED PARTS OF LP TURBINE


SECTION 2 LINE MAINTENANCE

FORM No: VNA-TE-F36 Issued: 00 /Mar. 2009

QUY TRÌNH KIỂM TRA TRƯỚC KHI BAY/GIỮA HAI LẦN BAY PRE-FLIGHT/TRANSIT CHECK Aircraft Type

A330

Effectivity A/C Reg. No:

Check Definitions and Notifications a)

A “PRE-FLIGHT/TRANSIT Check” shall be performed before each flight but not earlier than 2 hours before the flight. b) All fluids uplifted during the “PRE-FLIGHT/TRANSIT Check” must be recorded on the current page of the aircraft technical log ETOPS Sector All scheduled items in “ETOPS PRE-DEPARTURE SERVICE CHECK” must be accomplished within 2-4 hours of ETOPS departure and The aircraft must be verified as “ETOPS CHECK COMPLETED” prior to every “ETOPS” sector. Safety Pre-caution at aircraft arrival In accordance with Line Maintenance / Ground Handling Procedures Ensure parking area is clear of foreign objects or any other obstructions, check operation of aircraft exterior lights during taxiing in, chock nose wheels fore and aft. Item

Title / Task Description / Requirement

1

Remove all nose landing gear and main landing gear safety pins (Pre-flight only).

2

a. Review and action Technical Log Book and Cabin Defect Log Book, transfer entries to Technical Log Book where necessary (Transit only).

3

a.

Do a safety check of flight compartment for proper position of controls.

b.

Energize the aircraft electrical network(Pre-flight only)

4

Remove all protective covers and blanks (Pre-flight only).

5

a. Check battery 1 and 2 volts immediately before selection of GPU / APU or if power has been off more than six hours. BATT 1 AND 2 and APU BAT

CHECK OFF

BATT 1 AND 2 VOLTAGE and APU BAT

CHECK ABOVE 25.5V

Batteries voltage above 25.5V (battery capacity is above 50%). If batteries voltage below 25.5V, a charging cycle of about 15 minutes is required. BATT 1 AND 2 and APU BAT EXT POWER

AUTO ON

Check ECAM ELEC page, batteries contactor closed and batteries charging.

In accordance with AMS A330- Issue 10 Amd 01

Page 1 of 4

Item

Title / Task Description / Requirement b. Check ECAM status message including auto land downgrade status message, Check NO OIL FILTER “CLOG” Indication in ECAM PAGE/Status Check no “LOW OIL LEVEL” Message on ECAM APU page c. Check engine oil levels using ECAM /or sight glass (Physical Check) between 15 minutes and 2 hours after engine Shutdown and service as necessary, IWA AMM 12-13-79. Record exactly the uplift oil quantity to Tech log (if applicable) NOTE:ENG/APU oil consumption monitoring is critical to ETOPS operation, refer ENG/ APU oil consumption limit graphic d. Check hydraulic level, uplift and record in Technical Log Book if necessary (Transit only).

6

Inspect landing gear doors, wheels, brakes and tires for condition. Check Oleo extensions appear normal.

7

Do walk around inspection of the whole aircraft exterior and check for obvious signs of fluid leaks and damage, loose or missing parts, obstruction of inlets / outlets, fuselage tail skid for damage of ground contact during takeoff (Transit only), navigation / communication system antennae, static ports, TAT, pitot probes, AOA sensors, discharge indicators of oxygen and APU fire extinguisher.

8

General visual inspection of tires, wheels and brakes for hydraulic leaks IAW AMM task 32-41-00-210-803 ref. AMS task 324100-03-1

9

Check tire pressure IAW AMM task 32-41-00-220-802 ref. AMS task 324100-04-1 (before first flight of the day).

10

Examine the torque link assembly. Make sure that it is correctly installed and there is no damage or wear.

11

Do an external inspection of engines including fan, inlet cowl, turbine and exhaust nozzle and cowlings for security.

12

Drain water from each fuel tank (if the aircraft has been on the ground for six hours or more) I.A.W AMM: 12-32-28-281-810 ( ref AMS 281100-10-1). Obtain water free samples from bowser or “Refueling truck” prior to refueling.

13

Refuel the aircraft up to required dispatch quantity IAW AMM task 12-11-28 page block 3. Make sure that fuel uplift quantity discrepancy (between Aircraft’s indicator and Bowser’s indicator) is within limit (reference: APPENDIX 1).- Note : This requirement apply to all flights dispatched from

Vietnam’s Airport only Record uplift / content in the Technical Log Book. 14

Service toilet and fresh water systems as required, check for fluid leaks at toilet and water servicing panels. Rectify defects before flight.

15

Ensure any corrective actions made in the Technical Log Book have been cleared.

16

RVSM REQUIREMENTS: a.

Inspection / check from ground level of the status of TAT, AOA vanes, static probes and the pitot probe (9DA1, 9DA2, 9DA3) for obvious damage.


Page 2 of 4

Item

Title / Task Description / Requirement b.

Do a visual inspection around the static probes (left and right sides). Note: 

In order to help the operator to determine easily the area to be inspected, Airbus proposes to draw on the fuselage some red marks as defined in SIL 34-064 (corners of a squares).



These marks are for information only and aim at easing the pre-flight check. In addition, they are not mandatory to archive the RVSM certification. In case of scratches or dents around the static ports, the only applicable documentation is the SRM ATA 53.

17

Do security inspection of the whole aircraft as per “MECHANIC” section in the form VNA-SQ-F81-09 (Aircraft Normal Security Check Report) and take the signature.

18

DO FINAL WALK AROUND INSPECTION:

19

a.

Visually inspect cargo door (fwd/aft/bulk) seals for damage prior to closing the doors after aircraft loading has been completed

b.

Ensure all doors and panels are secured, landing gear pins removed and stowed, engine intakes and air inlets clear of foreign objects.

c.

Ensure no damage has been caused by ground equipment or during baggage loading.

d.

Remove wheel chocks (upon flight crew instruction).

DISPATCH Certify accomplishment of inspection and maintenance in Flight & Technical Log

APPENDIX 1: Fuel uplift quantity discrepancy limit (between Aircraft’s indicator and Bowser’s indicator) (by fuel uplift quantity)

Fuel uplift quantity (Kg)

Discrepancy (%)

Discrepancy (Kg)

0 ÷ 1000 Kg

≤ 5.8

≤ 58

1000 Kg ÷ 2000 Kg

≤ 4.5

≤ 90

2000 Kg ÷ 5000 Kg

≤ 3.8

≤ 190

(by aircraft’s indicator)


Page 3 of 4

5000 Kg ÷ 10000 Kg

≤ 2.6

≤ 260

10.000 Kg ÷ 20000 Kg

≤ 2.3

≤ 460

More than 20000 Kg

≤ 1.6

≤ 1600 (with uplift quantity less than 100,000 Kg)

Safety Pre-caution at aircraft departure Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures Prior to engine start, ensure area is free of any loose objects and obstruction, any remaining entry / service doors are secured closed and wheel chocks removed

“ETOPS Sectors” – If applicable Prior to every “ETOPS sector”, ensure the aircraft is “ETOPS CAPABLE” review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “ETOPS CAPABLE”. b) Check the ETOPS condition of the A/C has not been modified since last ETOPS CRS. Certify on the “ETOPS PREDEPARTURE SERVICE CHECK” form and the appropriate page of the aircraft technical log that the aircraft is “ETOPS CHECK COMPLETED”.

“RVSM Capability” Prior to every flight, review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM CAPABLE”. b) Write in technical log if the A/C is not RVSM capable.


Page 4 of 4

FORM No: VNA-TE-F37 Issued: 00 / Mar. 2009

QUY TRÌNH KIỂM TRA CUỐI NGÀY TERMINAL/DAILY CHECK OR EQUIVALENT Aircraft Type

A330

Affectivity A/C Reg. No:

Check Definitions and Notifications a) b) c)

The “TERMINAL Check” shall be performed in principle every day and in any case interval must not exceed 36 hours elapsed time. All fluids uplifted during the “TERMINAL CHECK” must be recorded on the current aircraft Technical Log page. Preflight/Transit check is included in this terminal check procedure. If time to next flight is more than two (02) hours, then it is required to perform preflight check again.

ETOPS Sector All scheduled items in “ETOPS PRE-DEPARTURE SERVICE CHECK” must be accomplished within 2-4 hours of ETOPS departure and The aircraft must be verified as “ETOPS CHECK COMPLETED” prior to every “ETOPS” sector. Safety Pre-caution at aircraft arrival In accordance with Line Maintenance / Ground Handling Procedures Ensure parking area is clear of foreign objects or any other obstruction, check operation of aircraft exterior lights during taxiing in, chock nose wheels fore and aft Item


ITEM

WORK TO BE CARRIED OUT

1

Carry out Transit Check IAW form A330 - PRE-FLIGHT / TRANSIT CHECK.

2

Install wheel chocks, nose landing gear and main landing gear safety pins.

3

Install all protective covers and blanks.

4

AMS 242400-01-3 (or 242400-01-2): Operational check of EMERGENCY GENERATION SYSTEMIAW. AMM : 24-24-00-710-801 Note: After test, don’t forget to push the P/B “Leak measurement valve “ Green.

5

Check seat covers and slide-raft covers for condition.

6

Do the following operational tests of: External lights: a. Landing light b. Runway Turnoff light c. Taxi and Takeoff light d. Logo Light e. Anti collision/ Strobe light f. Wing and Engine Scan light g. Emergency light Cabin lighting and passenger signs IAW AMM task 33-21-00-710-801

7

Do a general check of cockpit lighting and emergency torches, replenish spare bulb box as required.

8

Check Lavatories for general condition and functional operation a. Waste Disposal Lid Spring Retention & Waste Enclosure Door Close b. Operational condition of Wash Basin Drain. Check for cleanliness and evidence of water leakage. c. Lavatory Door Latch Sliding & Locking with Light On/Off. Check the door indicator d. Operational condition of Toilet Flushing

In accordance with AMS A330 Issue 10 Amd 01

Page 1 of 5

Item

Title / Task Description / Requirement e. Operational condition of Soap Dispenser and cleanliness. f. Condition of Waste Compartment Fire Ext, Temp Indicator g. Condition of No Smoking Placard, Ashtray h. Check the Passenger sign

9

AMS 324200-01-1:With parking brake applied, check heat pack wear indicator IAW AMM task 32-4000-210-802.

10

Do a general visual inspection of the landing-gear and the landing-gear doors from the ground during the aircraft walk around including: a. Nose landing gear and main landing gear proximity switches for security and cleanliness. b. Main landing gear shock absorber for signs of leakage and normal extension. c. Main landing gear sliding tube for scoring / damage and normal extension. d. Nose landing gear shock absorber for signs of leakage and normal extension. e. Wheels and tires (rim damage, sheared / missing tie bolts). f. Hydraulic leaks (gear doors closed). g. Nose landing gear taxi light for cleanliness.

11

In passenger cabin, do the following check of: a. Passenger cabin for general condition and cleanliness. b. Galleys for general condition, cleanliness and evidence of water leakage, and functional operation as below.

-

Galley Sink Drain, Clogging Operational condition and cleanliness of Galley Inserts (Oven, C/M, W/B, refrigerator) Cleanliness of inside of Oven Drain Clogging of inside of Ice Drawer Compartment

c. Check the Emergency equipment (Emergency Equipment Lits attached in Techlog book) for

-

Proper installation/Location Damaged Security Seal (if having)

d. First Aid Kit and Medical Kit for serviceable condition (seal, expiry date, condition,…) e. Wings upper surfaces and control surfaces through cabin windows for general condition and evidence of fluid leakage. 12

IFE Operation Check: Turn on the system Play VIDEO PA then check a) Monitor video quality. b) Handset display chanel number c) OVHD/Wall-mount monitor video quality d) Check PA operation from all Cabin Handset follow: - PA volume and PA quality - Normal operation of PA Latch and Release


Page 2 of 5

Item


13

Print out of the APU/ Eng hours and cycles stored in the PDIMU(10TV)/DMU(1TV) IAW AMM task 31-36-00-740-816. Write to the Tech-log

14

Around APU area, do a general visual inspection of:

15

a.

Air intake: flap closed.

b.

Door: closed and secured.

c.

Drain mast, drains and vents.

d.

Exhaust.

e.

Fire extinguisher overpressure indicator.

Do a general visual inspection of stabilizers and cone / rear fuselage from ground as far as visible IAW AMM task 05-23-00-200-801, 05-23-00-200-802 including: a. Trimmable horizontal stabilizers and elevators. b. Fin and rudder. c. Static dischargers.

16

Do a GVI of upper half of fuselage from the ground as far as visible IAW AMM task 05-22-00-200-803

17

Do a general visual inspection of lower half of fuselage from ground as far as visible IAW AMM task 0521-00-200-801 OR 53-35-00-200-801, including: a. Avionics equipment vent air inlet valve. b. All service panels and doors IAW AMM task 05-28-00-200-801. c. Fresh water and wastewater drain masts. d. Pitot probes, static ports, and AOA sensors. e. Exterior lights for cleanliness. f. Radome: latches positively locked. g. Crew oxygen cylinder overpressure indicator: green disc in place. h. Outflow valve: no obstruction. i. Antennas and beacon.

18

Do a general visual inspection of wings from ground as far as visible IAW AMM task 05-25-00-200-801, including: a. Leading edge slats. b. Leading edge ventilation air intake: no obstruction. c. Landing light for cleanliness. d. Surge tank air intake: no obstruction. e. Fuel tank overpressure protector disc: white cross in view. f. Navigation and strobe lights. g. Static dischargers. h. Control surfaces, flaps and track fairings for damage and fluid leakage. i. Lower wing surface: evidence of fuel leakage.


Page 3 of 5

Item 19

Title / Task Description / Requirement CARGO COMPARTMENT a. Visually check Forward / Aft / Bulk cargo compartment lining to verify integrity of compartment sealing Note: Check cargo compartment liners for tears or punctures after cargo compartments have been unloaded or prior to aircraft loading b. Visually inspect Forward /Aft / Bulk cargo compartment door seals and seal depressors for condition.

20

Do a GVI of power plants, nacelles and pylons (cowlings closed) from ground IAW AMM task 05-24-00200-801-(1), including: a. Cowlings: panels, air outlets, security of latches. b. Fan thrust reverser doors: latches secured (red indicator not protruding). c. Drain mast and pylon drains: no obstruction or fluid leakage. d. Access doors and over pressure doors: in place, closed and secured. e. Engine air inlets: lip skins, inner and outer intake cowls. f. Fan exhausts: acoustic lining, exit vanes and struts, thrust reverser blocker doors. g. Turbine exhausts: visible turbine blades, nozzle and plug (for damage and metal deposit).

21

Do the following: a) De-energize the aircraft electrical network IAW AMM task 24-41-00-740-801. b) Ensure all doors and service panels are properly closed and secured. c) Ensure all required protective covers and blanks installed.

22

AMS 281100-10-1 Operate water drain VLV to drain accumulated water from center, inner, outer and wing vent surge tanks I.A.W AMM: 123228-281-810

Safety Pre-caution at aircraft departure Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures Prior to engine start, ensure area is free of any loose objects and obstruction, any remaining entry / service doors are secured closed and wheel chocks removed

“ETOPS Sectors” – If applicable Prior to every “ETOPS sector”, ensure the aircraft is “ETOPS CAPABLE” review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “ETOPS CAPABLE”. b) Check the ETOPS condition of the A/C has not been modified since last ETOPS CRS. Certify on the “ETOPS PREDEPARTURE SERVICE CHECK” form and the appropriate page of the aircraft technical log that the aircraft is “ETOPS CHECK COMPLETED”.


Page 4 of 5

“RVSM Capability” Prior to every flight, review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM CAPABLE”. b) Write in techlog if the A/C is not RVSM capable.


Page 5 of 5

FORM No: VNA-TE-F38 Issued: 00 / Mar. 2009

QUY TRÌNH KIỂM TRA NGOẠI TRƯỜNG WEEKLY/LINE1/LINE2 CHECK OR EQUIVALENT Aircraft Type A/C Reg. No.

A330

Station

Affectivity A/C Reg. No:

Date

Tech Log page

Work Package

Check Definitions and Notifications a) The “Weekly Check” shall be carried out within every 07 days. b) All fluids uplifted during the “Weekly Check” must be recorded on the current aircraft Technical Log page. c) Preflight/Transit and Terminal check is included in this Weekly Check procedure. If time to next flight is more than two (02) hours, then it is required to perform Preflight/Transit check again. ETOPS Sector All scheduled items in “ETOPS PRE-DEPARTURE SERVICE CHECK” must be accomplished within 2-4 hours of ETOPS departure and The aircraft must be verified as “ETOPS CHECK COMPLETED” prior to every “ETOPS” sector. Safety Pre-caution at aircraft arrival In accordance with Line Maintenance / Ground Handling Procedures Ensure parking area is clear of foreign objects or any other obstruction, check operation of aircraft exterior lights during taxiing in, chock nose wheels fore and aft

Item


1

Carry out Terminal check IAW form A330 - TERMINAL/DAILY CHECK OR EQUIVALENT

2

Check Crew/ Attendant/ Passenger seats and belts for general condition, correct attachment and proper function.

3

Clean all CRT, LCD screens.

4

DAR (DIGITAL ACMS RECORDER) OPTICAL DISK: a.

Check for the presence of DAR maintenance status associated with fault message DAR cassette 2TV.

b.

Check the presence of the one spare optical disk in the flight green bag.(Only for A371, A372, A374, A375)

c

LOMS Requirement : Replacement of the QAR Disk (Apply for A/C use the Optical disk: A371, A372, A374, A375) IAW AMM task 31-36-52-600-803-A for flight data storage .

5

Cross check fluid level on each reservoir, on ECAM hydraulic page and ground service panel indicator IAW AMM task 29-31-00-200-801 ref. AMS task 293000-01-1.

6

COCKPIT AND CABIN INSPECTION:

a.

Do a visual inspection of passenger compartment, including seat track covers, ceiling panels, light covers, window panels, forward and aft partitions and stowage, literature pocket and magazine rack, attendant seats, shroud and cover on each lavatory

b.

Check that the switch is in armed position on ELT remote control panel in cockpit.

c.

Make sure that all push-buttons are in the normal position, mainly on the overhead panel. Note:


MECH

Page 1 of 3

INSP

Item




MECH

MAINTENANCE PANEL 285 VU

+ THE P/B LEAK MEASUREMENT VALVES ARE PUSHED AND UNLIGHTED.

d.

7

Check the LED function of Flashlight. If the monitoring circuit flash is dim or the flash interval exceeds ten seconds, replacement of the battery pack at the next convenient opportunity (not to exceed ten days)

CABIN SAFETY EQUIPMENT: Check the slide bottles pressure indication on PIM (CIDS energized).

 If message indicated on PIM is check slide pressure (x) (x) (x) (x) (on door page): it is necessary to perform a visual check of bottle pressure.

 If the needle is aligned with the cursor green band: no additional action is required.  If the needle is not aligned with the cursor green band: replace the escape slide. 8

a.

Cleaning of the toilet vacuum waste lines with chemical cleaning agent and crushed ice IAW AMM task 38-31-00-100-807 ref. AMS task 383100-04-1. At each toilet, perform a flush test as follow:

b.

c.

 Push and release the toilet flush switch.  Check that toilet flushes the bowl correctly without leaks and check you have correct vacuum. Operational check of soap dispensers, Replace if necessary

9

General visual inspection of the landing gears and the landing gear doors IAW AMM task 05-2710 PB 601; 05-27-30 PB 601

10

CARGO COMPARTMENTS: a.

LOWER DECK FORWARD CARGO COMPARTMENT: Visual check of linings, floor panels, sealing strips, protection plates, decompression panels and access door IAW AMM task 25-52-00-210-801 ref. AMS task 255200-01-1.

b.

LOWER DECK AFT CARGO COMPARTMENT: Visual check of linings, floor panels, sealing strips, protection plates, decompression panels and access doors IAW AMM task 2553-00-210-801 ref. AMS task 255300-01-1. LOWER DECK BULK CARGO COMPARTMENT: Visual check of

c.

 Linings, floor panels, sealing strips and access door IAW AMM task 25-54-00-210-801 ref. AMS task 255400-01-1.

 Decompression panels IAW AMM task 25-54-00-210-803. d.

Check automatic return of cargo door selector lever in stop / neutral position and stopping of yellow electric hydraulic pump after 10 seconds when the cargo door is in full closed position IAW AMM task 52-30-00-410-801.

e

LOWER DECK CARGO COMPARTMENT: Visual Inspection of the Cargo Compartment and the Component of the Cargo Loading System such as: PDU, Roller, Side wall Operational test proximity switches which control the longitudinal and/or the transverse Power Drive Units (PDU). IAW AMM task 25-51-00-710-801-A.

11

Check pressure of the portable oxygen cylinder by reading the gauge IAW AMM task 35-30-00210-801 ref. AMS task 353000-01-1.

12

a.

Check of the tamper seal / serviceability indication of the flight crew portable protective breathing equipment IAW AMM task 35-31-52-210-802 ref. AMS task 353100-01-1.


Page 2 of 3

INSP

Item

13

Title / Task Description / Requirement b.

Check of the tamper seal / serviceability indication of the cabin attendants portable protective breathing equipment IAW AMM task 35-30-00-210-802 ref. AMS task 35320002-1.

a

Check APU oil level on sight glass and service as required IAW AMM task 12-13-49-612801.

b

Check APU lube and generator scavenge filters differential pressure indicator position. (pop-out not protruding) Refer AMS task 499100-01-2, AMM 499141-210-801 *Do not APU re- start, if DPI pop-out or oil chip detected, until APU trouble shooting done.

14

LUBRICATION OF MLG BOGIE PIVOT PIN IAW AMM task 122232-640-801 ref AMS task 321000-04-1

15

I.A.W AMM 31-36-00-740-070-A. Test the ACMS Special function/Reprograming Procedures to make sure the message *ENABLE show below all the Report Note: password for A/C from A371-A375: PASSWD3 password for A/C from A376-A381: ENGI password for A383: LINE and ENGI

16

IFE Operation Check: Do the bite test for IFE system and send the record to MCC to upload to OEM website server.

MECH

INSP

Safety Pre-caution at aircraft departure Dispatch aircraft in accordance with Line Maintenance / Ground Handling Procedures Prior to engine start, ensure area is free of any loose objects and obstruction, any remaining entry / service doors are secured closed and wheel chocks removed “RVSM Capability” Prior to every flight, review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “RVSM CAPABLE”. b) Write in techlog if the A/C is not RVSM capable. “ETOPS Sectors” – If applicable Prior to every “ETOPS sector”, ensure the aircraft is “ETOPS CAPABLE” review the following and action as required: a) Aircraft technical log, all outstanding current and carried forward defects (ADD), Out-of-Phase Maintenance (OPM) sheets, Notice-To-Crew (NTC) and Minimum Equipment List (MEL) items to ensure the aircraft is “ETOPS CAPABLE”. b) Check the ETOPS condition of the A/C has not been modified since last ETOPS CRS. Certify on the “ETOPS PREDEPARTURE SERVICE CHECK” form and the appropriate page of the aircraft technical log that the aircraft is “ETOPS CHECK COMPLETED”. CERTIFICATE OF RELEASE TO SERVICE “The work recorded has been carried out in accordance with the requirements of VAR-145 for the time being in force and in respect to that work the aircraft / aircraft equipment is considered fit for service”. Date:

Signature:.......................... Stamp Holder:..............................Time (UTC):

The stamp / signature in the inspection column denote work has been carried out in accordance with the above requirements.


Page 3 of 3

A330 ETOPS PRE-DEPARTURE SERVICE CHECK A/C Reg. No.

Flight Hours

Item

Flight No.

Station

Date

Maintenance Task Check is to be completed within 2-4 hours of ETOPS departure

1 2

3

4 5 6

7 8 9

10 11

12

13 14

15

16

Review aircraft logbook for reported discrepancies and oil consumption for previous flights. Correct as necessary. Verify ECAM status level message (including auto land downgrade status message) and higher are resolved or approved dispatch paperwork is applied. ETOPS Qualification Required. General Visual Inspection (GVI) of the fuselage access/service panels, hatches, navigation/communication antennas and radome from ground level, for obvious damage and security.. GVI of the nose and main landing gear doors, tires, wheels and brakes for obvious damage and wear or hydraulic leak. Check Oleo extensions appear normal. GVI of the static ports, Total Air Temperature (TAT) probes, pitot static probes, ice detector probes (if installed) and angle-of-attack (AOA) sensors for obvious damage. GVI of the left and right wing leading edge and associated devices, trailing edge and associated devices, wing lower surface, wing tip area, and wing to fuselage section for general condition. GVI of the fuselage and APU in areas of drain masts and drains for fluid leakage. GVI of all air inlet/exhaust doors and cabin pressure outflow valve to ensure there are no obstructions. GVI of the vertical stabilizer, rudder, horizontal stabilizers, and elevators for obvious damage. Visually inspect cargo door (fwd/aft/bulk) seals for damage prior to closing the doors after aircraft loading has been completed GVI of the left engine thrust reverser, exhaust area, strut, and visible turbine blades for obvious damage and evidence of metal/oil accumulation. GVI of the left engine cowling, inlet cowl, nosedome and visible fan blades for obvious damage. GVI of access panels and blowout doors for condition and security. Also GVI for open latches and signs of fluid leakage. Verify the left engine oil level and service as necessary. ETOPS Qualification Required. Indicate amount added: _______________ GVI of the right engine thrust reverser, exhaust area, strut, and visible turbine blades for obvious damage and evidence of metal/oil accumulation. GVI of the right engine cowling, inlet cowl, nosedome and visible fan blades for obvious damage. GVI of access panels and blowout doors for condition and security. Also GVI for open latches and signs of fluid leakage. Verify the right engine oil level and service as necessary. ETOPS Qualification Required. Indicate amount added: _______________ Verify the APU oil level and service as necessary. It is acceptable to use flight deck

In accordance with AMS A330 iss 10 am01

ETOPS PDSC

Page 1 of 2

A330 ETOPS PRE-DEPARTURE SERVICE CHECK indications for this task. ETOPS Qualification Required. Indicate amount added: _______________ Final Check Sign-Off All ETOPS Checks performed by ETOPS qualified mechanic. Engine and APU oil consumption rate checked and acceptable to MCC. Note: Unless otherwise specified, all GVIs are to be performed from ground level.

In accordance with AMS A330 iss 10 am01

ETOPS PDSC

Page 2 of 2

SECTION 3

SCHEDULE COMPONENT MAINTENANCE

A330 maintenance schedule LIST OF EFFECTIVE PAGES TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

ENGINE LIFE LIMITED PART LIST

1-9

01/10

ALS PARTS 1 INTRODUCTION LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST

1 2 3 4 5 6

LANDINGEAR LIFE LIMITED PARTS LIST

7


8


9


10


PAGE

AMDT / ISSUE NO

SYSTEMS LIFE LIMITED COMPONENTS SYSTEMS LIFE LIMITED COMPONENTS SYSTEMS LIFE LIMITED COMPONENTS SYSTEMS LIFE LIMITED COMPONENTS SYSTEMS LIFE LIMITED COMPONENTS

01/10 01/10 01/10

TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE

01/10

01/10

01/10

13 14 15

AMDT / ISSUE NO

01/10 1 2 3 4 5

01/10 01/10 01/10 01/10 01/10

01/10

01/10

12

PAGE

01/10

01/10

11

TITLE/CHAPTER/ZONE

ALS PARTS 4 INTRODUCTION

01/10


LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST

TITLE/CHAPTER/ZONE

01/10 1 01/10 2 01/10 3 01/10 4 01/10 5

01/10 01/10 01/10 01/10 01/10

LIST OF EFFECTIVE PAGES

Page: 1

A330 maintenance schedule LIST OF EFFECTIVE PAGES TITLE/CHAPTER/ZONE LANDINGEAR LIFE LIMITED PARTS LIST LANDINGEAR LIFE LIMITED PARTS LIST

PAGE

16-20 11

AMDT / ISSUE NO

TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

AMDT / ISSUE NO

01/10

1

01/10

LLP-23

1

01/10

TCI-24

1

01/10

LLP-25

1

01/10

TCI-24

2

01/10

TCI-24

3

01/10

LLP-26

1

01/10

LLP-26

2

01/10

TCI-26

1

01/10

TCI-26

2

01/10

3

01/10

TCI-27

1

01/10

TCI-27

2

01/10

LLP-34

1

01/10

TCI-29

1

01/10

LLP-35

1

01/10

TCI-35

1

01/10

01/10 LLP-31

1

01/10 01/10

LLP-32


PAGE

01/10

TCI-21

TCI-26

TITLE/CHAPTER/ZONE

1

01/10 01/10

LLP-72

1

01/10

LLP-72

2

01/10


Page: 2


SECTION 3 GENERAL INTRODUCTION 1. GENERAL This section includes all the scheduled tasks related to Time Control Item and Life Limited Part. Task listed in table “TIME CONTROLLED ITEM TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE” are connected to the removal/installation of components/parts, which are to be restored/overhauled/tested in a workshop and then may be re-installed on a different A/C (rotables). This does not include components removed, cleaned and put back on the same A/C without going into a workshop.

Note: -

Refer to the AMS/CMM for threshold. For next scheduled removal: Refer to the certificate released to service of Component and related CMM. In case the Certificate of released to service of Component not available or not mention, refer to the table “TIME CONTROLLED ITEM TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE” for threshold/interval.


A330 ENGINE LIFE LIMITED PARTS LIST IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE PW4000 SERIES ENGINE MANUAL CHAPTER 5 THE PW4000 SERIES ENGINE MANUAL CHAPTER 5 IS THE REFERENCE.

No 1

2 3 4 5 6 7 8

Description Hub−LPC Assembly

Disk − Drum Rotor Assembly Disk − LPC, 1.3 Stage Disk − LPC, 1.6 Stage Disk − LPC, 2nd Stage Disk − LPC, 3rd Stage Disk − LPC, 4th Stage Coupling Assy. − Turbine Shaft

P/N 51B321 .51B301

Life Limit (CY) EFECTIVITY 15,000 ALL

52B021 .52B001

15,000 ALL

50B882−01 50B882−02 50B882−03 50B882−04 50B882−05 50B882−06 51A275 .51A274

15,000 15,000 15,000 15,000 15,000 15,000 15,000

51A030 .51A027 9 10

HPC Hub Front Disk − HPC, 5th Stage

11

HPC Disk − Drum Rotor Assembly (a) Part number obtained by reidentification in SB PW4G−100−72−105

(a)

ISSUE: 10, AMENDMENT: 01

Remarks

Reference Reference ALL ALL ALL ALL ALL ALL ALL Reference 7,000 ALL Reference

51H572 54H405 51H905 54H816−01

15,000 15,000 15,000 15,000

54H816−101

15,000 ALL

55H106−01 55H106−101

15,000 ALL 15,000 ALL

ALL ALL ALL ALL

Page 1



No

Description (a)

12 13

Disk − HPC, 6th Stage Disk − HPC, 7th Stage

14

Disk − HPC, 8th Stage

15


16 17

Disk − HPC, 10th Stage Disk − HPC, 11th Stage

18


19

Disk−Drum Rotor Assembly_Stage 13 thru 15


P/N 53H976−01 53H976−101 50S106−01 53H976−02 54H816−02 53H976−03 54H816−03 53H976−04 54H816−04 53H976−05 53H976−06 54H626−02 53H976−07 53H976−08 55H106−02

Life Limit (CY) 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000 15,000

50S813-01 54H803−01 56H013−01 53H973−01 54H803−001 54H803−002 53H973−001 56H013−001

14,900 15,000 15,000 15,000 15,000 15,000 15,000 15,000

EFECTIVITY ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

Remarks

PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A

Page 2



No

Description


P/N 58H236−01 50S813−001

Life Limit (CY) EFECTIVITY 15,000 PW4164, PW4168, PW4168A 14,900 PW4164, PW4168, PW4168A

54H803-004

14,900 PW4164, PW4168, PW4168A

54H803-005

14,900 PW4164, PW4168, PW4168A

54H803-006

15,000 PW4164, PW4168, PW4168A

56H013-002

15,000 PW4164, PW4168, PW4168A

58H236-001

14,900 PW4164, PW4168, PW4168A

58H236-002

14,900 PW4164, PW4168, PW4168A

Remarks

(b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241. (b) Part number obtained by reidentification in SB PW4G-100-72-241.

Page 3



No

20

21

22

Description

P/N 58H236-00

Life Limit (CY) EFECTIVITY 15,000 PW4164, PW4168, PW4168A

50S813-01

15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

53H973−02 56H013−02 50S813−02

15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A 15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

53H973−03 56H013−03 50S813−03

15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A 15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

54H803−03 56H013−04 53H973−04

15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A

Remarks (b) Part number obtained by reidentification in SB PW4G-100-72-241.





Page 4



No

Description

P/N 50S813−04

50S813-04 23

Life Limit (CY) EFECTIVITY 15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170 14,900 PW4164, PW4168, PW4168A

Remarks

Hub − HPC, 15th Stage

24

Shaft − HPC Drive

25

Seal − Air Diffuser

26

Hub − Turbine Front Assembly (1st stage)


58H236−02 54H803−02 53H973−05 50S813−05

15,000 15,000 15,000 15,000

54H767 53H347 54H792 53H431

15,000 15,000 15,000 15,000

52L301 .51L901

15,000 PW4164, PW4168, PW4168A

PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170 ALL ALL ALL ALL

Reference

Page 5



No

27

28

Description

P/N 55L111 .55L061

Life Limit (CY) EFECTIVITY 15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D,PW4170 , PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D,PW4170

52L402 52L802 .52L002

15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A

55L102 .55L112

15,000 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170, PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

50L485 50L879

15,000 PW4164, PW4168, PW4168A 15,000 PW4164, PW4168, PW4168A

Remarks

Hub − Turbine Rear (Stage 2)

Seal − Air, HPT, 1st Stage (Outer Rotating)


Page 6



No

Description

P/N

Life Limit (CY) EFECTIVITY 12,600 PW4164, PW4168, PW4168A

50L879

29

Plate − Ring, HPT Blade 2nd Stage

30

Seal − Air, HPT, 2nd Stage


50L242

12,900 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170 15,000 ALL

50L195 53L027

15,000 PW4164, PW4168, PW4168A 1,000 PW4164, PW4168, PW4168A

Remarks Refer to AD 2011-2509 and ASB 72-236: reduce the limit at the first piece part exposure after the effective date of the AD (10-Jan-12).

The total cycles that the air seal can accumulate as PN 53L027 is 1,000 cycles but the combined life as PN 50L195 a PN 53L027 can not be more than the life cycles of PN 50L195 as listed. For HPT air sealing ring which has been worked to remove crack indications and is reidentified to PN 53L027 by Alert Service Bulletin

Page 7



No

Description

P/N

Life Limit (CY) EFECTIVITY

Remarks PW4G−100−A72−80. PN 53L027 sealing ring can be continued in service for an additional 1000 cycles after which the ring must be retired.

53L030

31

32

15,000 PW4164, PW4168, PW4168A 13,900 PW4164, PW4168, PW4168A

53L030

12,700 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

50L664 50L664

15,000 PW4164, PW4168, PW4168A 14,800 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170 15,000 ALL

Refer to AD 2011-2509 and ASB 72-236: reduce the limit at the first piece part exposure after the effective date of the AD (10-Jan-12).

Ring − Air Sealing, HPT, 1st stage (Inner Rotating)

Disk − LPT, 3rd Stage


50N803

The air seal must be replaced along with the brush seal when MFlange is separated.

Page 8



No 33

Description Disk − LPT, 4th Stage

P/N

Life Limit (CY) EFECTIVITY

(a)

50N924 50N424 51N404 51N304

(b)

50N924/D

34

Hub − LPT, 5th Stage

51N405 51N505

15,000 ALL 15,000 ALL

35

Disk − LPT, 6th Stage 50N686 50N886 51N706 50N587 50N487 50N521

15,000 15,000 15,000 15,000 15,000 15,000

36

Disk − LPT, 7th Stage

37

Seal − Air, LPT, 3rd Stage (Outer Rotating)

38

Seal − Air, LPT, 4th Stage 50N478 or 50N478−001


Remarks

15,000 9,500 15,000 15,000

ALL ALL ALL ALL

Part number obtained by reidentification in SB PW4G−100−72−105. Disk, PN 50N924 Rev D, see SB PW4G−100−72−105 for the applicable serial numbers that have the reduced cycle life.

7,500 ALL

PW4164, PW4168, PW4168A PW4164, PW4168, PW4168A ALL ALL ALL ALL

4,500 PW4164, PW4168, PW4168A PW4164−1D, PW4164C−1D,

Post SB 72-218

Refer to AD 2001−05−07: Fewer

Page 9



No

Description

P/N

Life Limit (CY) EFECTIVITY PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170. 1,500 CIS after the effective date of this AD

6,000 CSN

39

40

41

51N038

15,000

50N419 50N419

15,000 PW4164, PW4168, PW4168A 9,520 PW4164−1D, PW4164C−1D, PW4164C/B−1D, PW4168−1D, PW4168A−1D, PW4170

51A117−01 51A377−01 52A402−01 52A519−01 50N420

15,000 15,000 15,000 15,000 15,000

Remarks than or equal to 3,000 CSN. Refer to AD 2001−05−07: More than 3,000 CSN but fewer than or equal to 4,500 CSN Refer to AD 2001−05−07: More than 4,500 CSN but fewer than 6,000 CSN

Seal − Air, LPT, 5th Stage

Front Compressor Drive Turbine (LPT) Shaft

Seal − Air, LPT, 3rd Stage (Inner Rotating)

PW4164, PW4168 PW4164, PW4168, PW4168A ALL ALL ALL


10

Page

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IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE ALS PART 1, THE ALS PART 1 IS THE REFERENCE. (*) Whichever occurs first. LIFE LIMITS (*)

Explanation notes are located under the assy title

A330-2xx Nomenclature

Part Number

FH

LDG

Cal.

WV02x

WV05x WV06x

ATA 32-11-00 MAIN LANDING GEAR (FIG. 01 to 06)

X

X

MAIN STRUT AND DRESSINGS (FIG. 01 & 02)

X

X

(1) Embodiment of MOD 46902/SB A330-32-3096 introduces a different PNR. MOD 46902 factory embodied on original landing gear of MSN 271 and subsequent. (2) Embodiment of MOD 46903/SB A330-32-3096 introduces a different PNR. MOD 46903 factory embodied on original landing gear of MSN 271 and subsequent. (3) Embodiment of MOD 46904/SB A330-32-3095 introduces a different PNR. MOD 46904 factory embodied on original landing gear of MSN 271 and subsequent. (4) Parts that have been installed on any A330-300 series aircraft must not be fitted to any A340 aircraft models. (6) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437

Forward pintle pin

201489623 (2)

75000

50000

10 Ye

X

X

Upper torque link pin

201489600 (1)

60000

19700

10 Ye

X

X

Upper torque link

201489303

57000

13200

N/A

X

X (6)

Lower torque link

201489304

57000

13200

N/A

X

X (6)

Lower torque link pin

201489601 (1)

60000

14300

10 Ye

X

X

Bogie beam pivot pin

201489621 (3)

19000

4000

5 Ye

X

X

X

X

X

X

ATA 32-11-00 MAIN LANDING GEAR (FIG. 01 to 06) MAIN STRUT (FIG. 01 to 03)

(1) Embodiment of MOD 46904/SB A330-32-3095 introduces a different PNR. MOD 46904 factory embodied on original landing gear of MSN 271 and subsequent. (2) Parts that have been installed on any A330-300 series aircraft must not be fitted to any A340 aircraft models. (3) Rework in accordance with SB A330-32-3053/VSB A33/34-32-90 (MOD 45480) introduces a different PNR. (4) Rework in accordance with VSB A33/34-32-82 (MOD 45479) introduces a different PNR. (5) Both FH and LDG limits apply from the time the part was reworked in accordance with VSB A33/34-32-82. Nevertheless, the sum of the accumulated lives PRE and POST VSB A33/34-32-82 must not exceed 75000 FH / 50000 LDG. (6) Rework in accordance with SB A330-32-3215/VSB A33/34-32-257 (MOD 56498) introduces a different PNR. (7) These limits apply to parts identified as ‘S1’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (8) These limits apply to parts identified as ‘S3’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (9) These limits apply to parts on which SB A330-32-3215/VSB A33/34-32-257 (MOD 56498) has been performed at or before accumulation of 8750 LDG. (10) These limits apply to parts on which SB A330-32-3215/VSB A33/34-32-257 (MOD 56498) has been performed after accumulation of 8750 LDG. (11) These limits apply to parts identified as ‘S2C’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (12) These limits apply to parts NOT identified in notes (7), (8) and (11) above. (13) These limitations apply to parts on which SB A330-32-3215/VSB A33/34-32-257 (MOD 56498) has been performed at or before accumulation of 14000 LDG. (14) These limits apply to parts on which SB A330-32-3215/VSB A33/34-32-257 (MOD 56498) has been performed after accumulation of 14000 LDG. (15) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. Main fitting (LH)

201488301 (6)

53000

22000

N/A

X

X (15)

Main fitting (LH)

201488318 (6)

94520

22000

N/A

X

X (15)

Main fitting (LH)

201488320 (6)

94520

22000

N/A

X

X (15)

Main fitting (LH)

201488322 (6)

53000

22000

N/A

X

X (15)

Main fitting (LH)

201488324 (6)

46870

13750

N/A

X (7)

X (7)

Main fitting (LH)

201488324 (6)

57000

16685

N/A

X (8)

X (8) (15)

REF: ALS PART 1 R07 SUB PART 1-2




Part Number

FH

LDG

Cal.

WV02x

WV05x WV06x

Main fitting (LH)

201488324 (6)

N/A

N/A

31-Mar-09

X (11)

X (11)

Main fitting (LH)

201488324 (6)

94520

22000

N/A

X (12)

X (12) (15)

Main fitting (LH)

201488326 (6)

94520

22000

N/A

X

X (15)

Main fitting (LH)

201488329

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488329

94520

22000

N/A

X (14)

X (14) (15)

Main fitting (LH)

201488331

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488331

94520

22000

N/A

X (14)

X (13) (15)

Main fitting (LH)

201488333

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488333

94520

22000

N/A

X (14)

X (14) (15)

Main fitting (LH)

201488335

46870

23500

N/A

X (7) (9)

X (7) (9)

Main fitting (LH)

201488335

46870

13750

N/A

X (7) (10)

X (7) (10)

Main fitting (LH)

201488335

57000

16685

N/A

X (8)

X (8) (15)

Main fitting (LH)

201488335

N/A

N/A

31-Mar-09

X (11)

X (11)

Main fitting (LH)

201488335

120000

29330

N/A

X (12) (13)

X (12) (13) (15)

Main fitting (LH)

201488335

94520

22000

N/A

X (12) (14)

X (12) (14) (15)

Main fitting (LH)

201488337

53000

35000

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488337

65850

20000

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488337

53000

22000

N/A

X (14)

X (14) (15)

Main fitting (LH)

201488339

65850

20000

N/A

X (13)

X (13) (15)

Main fitting (LH)

201488339

53000

22000

N/A

X (14)

X (14) (15)

Main fitting (RH)

201488300 (6)

53000

22000

N/A

X

X (15)

Main fitting (RH)

201488319 (6)

94520

22000

N/A

X

X (15)

Main fitting (RH)

201488321 (6)

94520

22000

N/A

X

X (15)

Main fitting (RH)

201488323 (6)

53000

22000

N/A

X

X (15)

Main fitting (RH)

201488325 (6)

46870

13750

N/A

X (7)

X (7)

Main fitting (RH)

201488325 (6)

57000

16685

N/A

X (8)

X (8) (15)

Main fitting (RH)

201488325 (6)

N/A

N/A

31-Mar-09

X (11)

X (11)

Main fitting (RH)

201488325 (6)

94520

22000

N/A

X (12)

X (12) (15)

Main fitting (RH)

201488327 (6)

94520

22000

N/A

X

X (15)

Main fitting (RH)

201488330

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (RH)

201488330

94520

22000

N/A

X (14)

X (14) (15)

Main fitting (RH)

201488332

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (RH)

201488332

94520

22000

N/A

X (14)

X (14) (15)

Main fitting (RH)

201488334

120000

29330

N/A

X (13)

X (13) (15)

Main fitting (RH)

201488334

94520

22000

N/A

X (14)

X (14) (15)

Main fitting (RH)

201488336

46870

23500

N/A

X (7) (9)

X (7) (9)

Main fitting (RH)

201488336

46870

13750

N/A

X (7) (10)

X (7) (10)

Main fitting (RH)

201488336

57000

16685

N/A

X (8)

X (8) (15)

Main fitting (RH)

201488336

N/A

N/A

31-Mar-09

X (11)

X (11)

Main fitting (RH)

201488336

120000

29330

N/A

X (12) (13)

X (12) (13) (15)

Main fitting (RH)

201488336

94520

22000

N/A

X (12) (14)

X (12) (14) (15)

Main fitting (RH)

201488338

65850

20000

N/A

X (13)

X (13) (15)

Main fitting (RH)

201488338

53000

22000

N/A

X (14)

X (14) (15)

Main fitting (RH)

201488340

65850

20000

N/A

X (13)

X (13) (15)

Main fitting (RH)

201488340

53000

22000

N/A

X (14)

X (14) (15)

201488610 (1)

19000

4000

5 Ye

X

X

Pin SM7





Part Number

FH

LDG

Cal.

Pin SM8

201488607 (1)

19000

4000

Pin SM9

201488606 (1)

19000

4000

WV02x

WV05x WV06x

5 Ye

X

X

5 Ye

X

X


X

X


X

X

SHOCK STRUT (FIG. 03 & 04)

X

X

(1) The 10-year limit applies to parts that have been operated on any A330 before 31-Oct-1998, regardless of subsequent applications they have been fitted to. (2) Rework in accordance with SB A330-32-3204/VSB A33/34-32-233 or VSB A33/34-32-234 (MOD 55801) introduces a different PNR. (3) These limits apply to parts identified as ‘S1’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (4) These limits apply to parts NOT identified in note (3) above. (5) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. Sliding piston

201487300 (2)

67500

18900

N/A

X

X (5)

Sliding piston

201487307 (2)

42180

11810

N/A

X (3)

X (3) (5)

Sliding piston

201487307 (2)

67500

18900

N/A

X (4)

X (4) (5)


X

X

BOGIE AND DRESSINGS (FIG. 01)

X

X

BOGIE ASSEMBLY (FIG. 01)

X

X

(1) These limits apply to parts identified as ‘S2A’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (2) These limits apply to parts identified as ‘S2B’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (3) These limits apply to parts identified as ‘S2C’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul-2012. (4) These limits apply to parts NOT identified in notes (1), (2) and (3) above. (5) These limits apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. (6) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437.

Bogie beam

201272302

72300

50000

N/A

X

X (6)

Bogie beam

201272304

42610

28405

N/A

X (1)

X (1)

Bogie beam

201272304

12710

8470

N/A

X (2)

X (2)

Bogie beam

201272304

N/A

N/A

31-Mar-09

X (3)

X (3)

Bogie beam

201272304

72300

50000

N/A

X (4)

X (4) (6)

Bogie beam

201272306

72300

50000

N/A

X

X (6)

Bogie beam

201272307

42610

28405

N/A

X (1)

X (1)

Bogie beam

201272307

12710

8470

N/A

X (2)

X (2)

Bogie beam

201272307

N/A

N/A

31-Mar-09

X (3)

X (3)

Bogie beam

201272307

72300

50000

N/A

X (4)

X (4) (6)

Bogie beam

201485300

72300

50000

N/A

X

X (6)

Bogie beam

201485301

72300

50000

N/A

X

X (6)

Bogie beam

50-2117002-00

122360

44600

N/A

X (1) (2)

X (1) (2) (6)

Bogie beam

50-2117002-00

72500

30000

N/A

Bogie beam

50-2117002-00

N/A

N/A

31-Mar-09

Bogie beam

50-2117002-00

122360

44600

N/A

X (4)

X (4) (6)

Bogie beam

50-2117002-01

122360

44600

N/A

X (1) (2)

X (1) (2) (6)

Bogie beam

50-2117002-01

N/A

N/A

31-Mar-09

X (3)

X (3)

Bogie beam

50-2117002-01

122360

44600

N/A

X (4)

X (4) (6)


X (1) (2) (5) X (3)

X (3)




Part Number

FH

LDG

Cal.

WV02x

WV05x WV06x


X

X

COMPLETE SIDE STAY (FIG. 01, 05 & 06)

X

X

(BASIC) SIDE STAY (FIG. 05)

X

X


X

X


X

X

X

X

Lower lock link

201482300

N/A

35500

N/A

X

X

Lower lock link

201482305

N/A

35500

N/A

X

X

ATA 32-21-00 NOSE LANDING GEAR (FIG. 07 & 08)

X

X

NOSE LANDING GEAR LEG (FIG. 07)

X

X

MAIN FITTING-SHOCK ABSORBER STRUCTURE (FIG. 07 & 08)

X

X X

LOCK LINK (FIG. 06)

Restrictor valve

D65060

N/A

N/A

1-Jan-16

X

Restrictor valve

D67237

N/A

N/A

1-Jan-16

X

X

Support tube

D64020-1

N/A

N/A

1-Jan-16

X

X

Support tube

D67232-1

N/A

N/A

1-Jan-16

X

X


IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE ALS PART 1, THE ALS PART 1 IS THE REFERENCE. (*) Whichever occurs first. Explanation notes are located under the assy title

DEMONSTRATED FATIGUE LIVES (*) A330-2xx

Nomenclature

Part Number

FH

LDG


WV02x

WV05x WV06x

X

X

(1) ‘xx’ at the end of the PNR stands for any number between 00 and 99, including unused digits. (2) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (3) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (4) These limitations apply to parts fitted to aircraft PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (5) These limitations apply to parts fitted to aircraft POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). Aft pintle pin (LH) (1)

F32155011000xx

130000

40000

X

Aft pintle pin (LH) (1)

F32155021000xx

130000

40000

X (4)

Aft pintle pin (LH) (1)

F32155021000xx

125000

46800

Aft pintle pin (RH) (1)

F32155011001xx

130000

40000

X


F32155021001xx

130000

40000

X (4)


F32155021001xx

125000

46800

Aft pintle pin nut

SLN40927

130000

40000

Aft pintle pin nut

SLN40927

125000

50000

Aft pintle pin nut

SLN41180

130000

40000

Aft pintle pin nut

SLN41180

125000

50000

X X (3) X X (3)

X (4) X (3) X (4) X (3)


X

X


X

X

1) These limits apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. (2) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. Forward pintle pin

201489752

130000

40000

X

X (2)

Forward pintle pin

55-2105042-00

75000

40000

X

X (2)

Forward pintle pin lock bolt

201275895

130000

40000

X

X (2)


201589601

130000

40000

X

X (2)


55-2105058-00

75000

40000

X

X (2)


201489753

130000

40000

X

X (2)


55-2105055-00

75000

40000

X

X (2)

Upper torque link

201676300

120000

30000

X

X (2)

Upper torque link

50-2105021-00

75000

40000

X

X (2)

Torque link apex pin

201489602

130000

40000

X

X (2)


201676600

120000

30000

X

X (2)


55-2105054-00

75000

40000

X

X (2)

Torque link apex pin nut

201269656

130000

40000

X

X (2)


201269699

130000

40000

X

X (2)


X (2)

55-2105072-00

75000

40000

X

Lower torque link

201676301

120000

30000

X

X (2)

Lower torque link

50-2105020-00

75000

40000

X

X (2)


201489754

130000

40000

X

X (2)


55-2105056-00

75000

40000

X

X (2)




Nomenclature

Part Number

FH

LDG


201489751

130000

40000

X

X (2)


55-2105029-00

75000

40000

X

X (2)

Brake rod pin

201489619

N/A

50000

X

X

Brake rod pin

WV02x

WV05x WV06x

55-2105091-00

N/A

40000

X

X (2)

Brake rod

201254352

N/A

50000

X

X

Brake rod

201490300

N/A

50000

X

X

Brake rod

50-2105025-00

N/A

40000

X

X (2)


X

X


X

X

MAIN STRUT (FIG. 01 to 03)

X

X

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (3) These limitations apply to parts fitted to aircraft PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (4) These limitations apply to parts fitted to aircraft POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (5) These limitations apply to parts identified as ‘S1’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul2012. (6) These limitations apply to parts identified as ‘S3’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated 20-Jul2012. (7) These limitations apply to parts NOT identified in notes (5) and (6) above. (8) These limits apply to parts fitted on aircraft Post-MOD 58860 or Post-MOD 201437. (9) These limits do NOT apply to parts fitted on aircraft Post-MOD 58860 or Post-MOD 201437. Main fitting (LH)

201488341

120000

29330

X

X (9)

Main fitting (LH)

50-2107001-00

46870

25000

X (5)

X (5) (9)

Main fitting (LH)

50-2107001-00

75000

40000

X (6)

X (6) (9)

Main fitting (LH)

50-2107001-00

75000

40000

X (7)

X (7) (9)

Main fitting (RH)

201488342

120000

29330

X

X (9)

Main fitting (RH)

50-2108001-00

46870

25000

X (5)

X (5) (9)

Main fitting (RH)

50-2108001-00

75000

40000

X (6)

X (6) (9)

Main fitting (RH)

50-2108001-00

75000

40000

X (7)

X (7) (9)

Aft pintle bearing

201042565

130000

40000

X (3)

Aft pintle bearing

201042565

75000

40000

Aft pintle bearing

450250952

130000

40000

X

X (9)

Aft pintle bearing

450250953

130000

40000

X

X (9)

Aft pintle bearing

450250954

130000

30000

X

X (9)

Aft pintle bearing

450250955

130000

40000

X

X (9)

Aft pintle bearing

450250956

130000

40000

X

X (9)

Aft pintle bearing

450250957

130000

40000

X

X (9)

Pin SM7

201488652

80700

30000

X

X (9)

Pin SM7

201488685

80700

30000

X

X (9)

Pin SM7

55-2107009-00

75000

40000

X

X (9)

201488302

118100

30000

X

X (9)

Shortening link (upper)


X (2) (9)



Nomenclature

Part Number

FH

LDG


201488328

118100

30000

X

X (9)


50-2107003-00

75000

40000

X

X (9)

Pin SM8

201488651

109830

30000

X

X (9)

Pin SM8

201488690

109830

30000

X

X (9)

Pin SM8

201488707

109830

30000

X

X (9)

Pin SM8

55-2107008-00

75000

40000

X

X (9)

Shortening link (lower)

201488304

120000

30000

X

X (9)

Shortening link (lower)

50-2107002-00

75000

40000

X

X (9)

Pin SM9

201488650

114030

30000

X

X (9)

Pin SM9

201488691

114030

30000

X

X (9)

Pin SM9

201488699

114030

30000

X

X (9)

Pin SM9

55-2107007-00

75000

40000

X

X (9)

Pin SM9

55-2107093-00

75000

40000

WV02x

WV05x WV06x

X

X (9)


X

X


X

X

SHOCK STRUT (FIG. 03 & 04)

X

X

(1) These limitations apply to parts identified as ‘S1’ in Messier-Bugatti-Dowty Service Letter A33-34 A20 revision 07, dated20-Jul2012. (2) These limitations apply to parts NOT identified in note (1) above. (3) These limits apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. (4) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. Upper piston

201487301

100430

30000

X

X (4)

Upper piston

201487304

100430

30000

X

X (4)

Upper piston

201487306

100430

30000

X

X (4)

Upper piston

201496300

75000

50000

X

X

Upper piston

201496301

100430

30000

X

X (4)

Upper piston

201496302

100430

30000

X

X (4)

Upper piston

50-2109002-00

125000

50000

X

X

Recoil nut

201270730

N/A

50000

X

X

Recoil nut

201411604

N/A

50000

X

X

Recoil nut

50-2109008-00

N/A

47130

X

X

Sliding piston

201487308

130000

34600

X

X (4)

Sliding piston

201487309

46870

28375

X (1)

X (1)

Sliding piston

201487309

130000

34600

X (2)

X (2) (4)

Sliding piston

201487310

130000

34600

X

X (4)

Sliding piston

50-2109001-01

46870

25000

X (1)

X (1) (4)

Sliding piston

50-2109001-01

75000

40000

X (2)

X (2) (4)


X

X

BOGIE AND DRESSINGS (FIG. 01)

X

X

BOGIE ASSEMBLY (FIG. 01)

X

X

X

X (2)

(1) These limits apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. (2) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. Wheel axle

201272644

116100

30000




Nomenclature

Part Number

FH

LDG

Wheel axle

201272649

116100

Wheel axle

201485601

116100

Wheel axle

201485615

Wheel axle

55-2117003-00

WV02x

WV05x WV06x

30000

X

X (2)

30000

X

X (2)

116100

30000

X

X (2)

75000

40000

X

X (2)


X

X


X

X

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (3) These limitations apply to parts fitted to aircraft PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (4) These limitations apply to parts fitted to aircraft POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (5) Must be replaced by a new one every time it is removed from the upper side stay. Pivot link center pin

201442614

N/A

35500

X

Pivot link center pin

201442651

N/A

35500

X (3)

X

Pivot link center pin

201442651

N/A

50000

Pivot link bracket

201441605

N/A

35500

X

X

Pivot link bracket

201457607

N/A

35500

X

X

Pivot link bracket

X (2)

55-2119008-00

N/A

50000

X

X

Pivot link bracket bolt

NAS6606D10

N/A

(5)

X

X

Lock link/Side stay pin

201482609

N/A

35500

X (3)

Lock link/Side stay pin

201482609

N/A

50000

X (2)


X

X


X

X

(BASIC) SIDE STAY (FIG. 05)

X

X

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (3) These limitations apply to parts fitted to aircraft PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (4) These limitations apply to parts fitted to aircraft POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). (5) Must be replaced by a new one every time it is removed from the upper side stay. (6) These limits apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437. (7) These limits do NOT apply to parts fitted on aircraft POST MOD 58860 or POST MOD 201437.

R

Upper cardan nut

201267639

130000

40000

X

Upper cardan nut

201267642

130000

40000

X

X (7)

Upper cardan nut

55-1221042-01

75000

40000

X

X (7)

Upper cardan pin

201483600

130000

40000

X

X (7)

Upper cardan pin

55-2121003-00

75000

40000

X

X (7)

Side stay upper pin

201483602

130000

40000

X

X (7)

Side stay upper pin

55-2121005-00

75000

40000

X

X (7)

201483301

130000

40000

X

X (7)

Upper side stay


X (7)



Nomenclature Upper side stay

Part Number

FH

LDG

WV02x

WV05x WV06x

50-2121001-00

75000

40000

X

X (7)

Upper spring bracket

201441602

N/A

35500

X

X


201483636

N/A

35500

X

X


55-1221012-01

N/A

50000

X

X

Lower spring bracket

201441604

N/A

35500

X

X


201458611

N/A

35500

X

X


55-1221026-01

N/A

50000

X

X

Spring bracket upper bolt

MS21250H06016

N/A

(5)

X

X

Spring bracket lower bolt

201441607

N/A

35500

X

X


201458612

N/A

35500

X

X


55-1221029-01

N/A

50000

X

X

Side stay center pin

201483605

130000

40000

X (3)

Side stay center pin

201483605

75000

40000

Lower side stay

201483606

130000

40000

X

X (7)

Lower side stay

55-2121002-00

75000

40000

X

X (7) X (7)

X (2) (7)

Side stay lower pin

201483609

130000

40000

X

Side stay lower pin

55-2121007-00

125000

50000

X

X

Lower cardan pin

201483304

120000

30000

X

X (7)

Lower cardan pin

50-2121004-00

75000

40000

X

X (7)

Lower cardan nut

201483621

130000

40000

X

X (7)

Lower cardan nut

201483635

130000

40000

X

X (7)

Lower cardan nut

55-2121009-00

75000

40000

X

X (7)


X

X


X

X

LOCK LINK (FIG. 06)

X

X

(1) These limitations apply to parts fitted to aircraft PRE MOD 54500 and PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (2) These limitations apply to parts fitted to aircraft POST MOD 54500 or POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288) (3) These limitations apply to parts fitted to aircraft PRE SB A330-32-3212 (MOD 56214) or POST SB A330-32-3222 (MOD 57288). (4) These limitations apply to parts fitted to aircraft POST SB A330-32-3212 (MOD 56214) and PRE SB A330-32-3222 (MOD 57288). Cardan link pin

201442618

N/A

35500

Cardan link pin

201442618

N/A

50000

X (3) X (2)

Cardan link

201442617

N/A

35500

X

X

Cardan link

55-2123003-00

N/A

50000

X

X

Lock link upper pin

201482612

N/A

35500

X (3)

Lock link upper pin

201482612

N/A

50000

Upper lock link

201482301

N/A

35500

X

X

Upper lock link

201482304

N/A

35500

X

X

Upper lock link

X

X (2)

50-2123001-00

N/A

50000

X

Lock link center pin

201482610

N/A

35500

X (3)


201482610

N/A

50000


X (2)



Nomenclature

Part Number

FH

LDG

WV02x

WV05x WV06x

Lower lock link

201482312

N/A

35500

X

X

Lower lock link

50-2123002-00

N/A

50000

X

X

Connecting link/Lock link/Upper spring pin

201442633

N/A

35500

X

X


201442646

N/A

35500

X (3)


201442646

N/A

50000

Connecting link

201442606

N/A

35500

X (2) X

X

Connecting link

201442649

N/A

35500

X

X

Connecting link

55-1223011-01

N/A

50000

X

X

Connecting link/Pivot link pin

201442615

N/A

35500

X

X


201442650

N/A

35500

X (3)


201442650

N/A

50000

Pivot link

201442609

N/A

35500

X

X

Pivot link

201442648

N/A

35500

X

X

Pivot link

55-1223013-01

N/A

50000

X

X

201442613

N/A

35500

X

X

Lower spring/Pivot link pin

X (2)


201442647

N/A

35500

X

X


55-1223029-01

N/A

50000

X

X

X

X

ATA 32-21-00 NOSE LANDING GEAR (FIG. 07 & 08) (1) ‘xx’ at the end of the PNR stands for any number between 00 and 99, including unused digits. Pintle pin (1)

F53112339200xx

75000

50000

Pintle pin (1)

F53112339200xx

125000

41250

Pintle pin (1)

F53120581200xx

75000

50000

Pintle pin (1)

F53120581200xx

125000

41250

X X X X


X

X

DRAG STAY UPPER ARM ASSEMBLY (FIG. 07)

X

X

Drag stay upper pin

D64034

75000

50000

Drag stay upper pin

D64034

125000

50000

Drag stay upper arm

D64033

75000

50000

Drag stay upper arm

D64033

125000

50000

Drag stay center pin

D64036

75000

50000

Drag stay center pin

D64036

125000

50000

X X X X X X


X

X


X

X

Drag stay lower arm

D64037

75000

50000

Drag stay lower arm

D64037

125000

50000

X X


X

X


X

X

X

X

Drag stay lower arm/Main fitting pin

D64007

46400

30950

X

X

Drag stay lower arm/Main fitting pin

D66331

75000

50000

X

X

Upper flange

D64000

75000

50000

X

Upper flange

D64000

125000

50000

Turning sleeve

D63998

75000

50000

Turning sleeve

D63998

125000

50000

MAIN FITTING-SHOCK ABSORBER STRUCTURE (FIG. 07 & 08)


X X X



Nomenclature

Part Number

Turning sleeve

D63998-1

75000

50000

Turning sleeve

D63998-1

125000

50000

Turning sleeve

D67634

75000

50000

Turning sleeve

D67634

125000

50000


D64006

75000

50000


D64006

125000

50000

Upper torque link

D64002

75000

50000

Upper torque link

D64002

125000

50000


D62660

75000

50000


D62660

125000

50000

Lower torque link

D64001

75000

50000

Lower torque link

D64001

125000

50000


D64005

75000

50000


D64005

125000

50000


D67247

75000

50000


D67247

125000

50000


D67247-1

75000

50000


D67247-1

125000

50000


D67790

75000

50000


D67790

125000

50000

Sliding tube

D65046

75000

50000

X

X

Sliding tube

D67201

75000

50000

X

X

Sliding tube

D67338

75000

50000

X

X

Restrictor valve

D68053

75000

50000

X

Restrictor valve

D68053

125000

50000

Restrictor valve

D68053-1

75000

50000

Restrictor valve

D68053-1

125000

50000

Restrictor valve

D68346

75000

50000

Restrictor valve

FH

LDG

WV02x

WV05x WV06x

X X X X X X X X X X X X X X X X X X X X

X X X X

D68346

125000

50000

Support tube

D68052-1

75000

50000

X

Support tube

D68052-1

125000

50000

Support tube

D68100-1

75000

50000

Support tube

D68100-1

125000

50000

Restrictor

D61720

N/A

50000

X

X

Restrictor

D61720-1

N/A

50000

X

X

Restrictor

D67241

N/A

50000

X

X

Restrictor

D67241-1

N/A

50000

X

X

Restrictor

D68345

N/A

50000

X

X

Restrictor

D68347

N/A

50000

X

X

Main fitting

D63996

75000

50000

X

X

Main fitting

X

X X X X

D63996-10

75000

50000

X

Main fitting hinge pin

D64003

75000

50000

X

Main fitting hinge pin

D64003

125000

50000



X X

X



Nomenclature

Part Number

FH

LDG

WV02x

WV05x WV06x


X

X

LOCK LINK (FIG. 07)

X

X

Lock link upper arm/Main fitting pin

D61693

75000

50000


D61693

125000

50000


D61693-1

75000

50000


D61693-1

125000

50000


D67788

75000

50000


D67788

125000

50000

Lock link upper arm

D61845

75000

50000

Lock link upper arm

D61845

125000

50000


D61870

75000

50000


D61870

125000

50000


D61870-1

75000

50000


D61870-1

125000

50000


D67789

75000

50000


D67789

125000

50000

Lock link lower arm

D61846

75000

50000

Lock link lower arm

D61846

125000

50000

ATA 57-00-00 WING STRUCTURE (FIG. 09)

X X X X X X X X X X X X X X X X X

X

(1) This item is not transferable from an aircraftto another: Traceability at aircraft level is authorized. (2) ‘xx’ at the end of the PNR stands for any number between 00 and 99, including unused digits. Gear support rib (LH) (1) (2)

F57555013000xx

100000

33000

X

X

Gear support rib (LH) (1) (2)

F57555013002xx

100000

33000

X

X

Gear support rib (LH) (1) (2)

F57555114000xx

100000

33000

X

X

Gear support rib (RH) (1) (2)

F57555013001xx

100000

33000

X

X


F57555013003xx

100000

33000

X

X


F57555114001xx

100000

33000

X

X

Forward pintle fitting (LH) (1) (2)

F57555024002xx

100000

33000

X

X

Forward pintle fitting (RH) (1) (2)

F57555024003xx

100000

33000

X

X

Side stay fitting (LH) (1) (2)

F57555017000xx

100000

33000

X

Side stay fitting (LH) (1) (2)

F57555017002xx

100000

33000

X

Side stay fitting (RH) (1) (2)

F57555017001xx

100000

33000

X

Side stay fitting (RH) (1) (2)

F57555017003xx

100000

33000

X

X

Retraction jack fitting (LH) (1) (2)

F57550028000xx

100000

33000

X

X

Retraction jack fitting (LH) (1) (2)

F57551977000xx

100000

33000

Retraction jack fitting (RH) (1) (2)

F57550028001xx

100000

33000

X

X

Retraction jack fitting (RH) (1) (2)

F57551977001xx

100000

33000


X

X X

A330 AIRWORTHINESS LIMITATIONS SECTION

ALS Part 4 Ageing Systems Maintenance

AIRBUS SAS 2013. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS SAS. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein) without the express written consent of AIRBUS SAS. This document and its content shall not be used for any purpose other than that for which it is supplied.

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 4-0 INTRODUCTION 1.

GENERAL The data provided under Part 4 has been established with the following rules: Compliance with the requirements contained in this document is mandatory. No person may operate an aircraft to which an Airworthiness Limitations Section (ALS) applies except in accordance with the requirements of that ALS, unless otherwise agreed with the Authority of the State of aircraft registry. Consultation with the State of design should be made by the State of aircraft registry, in consideration of any deviation from the ALS requirements. This is indicated in the International Civil Aviation Organization (ICAO) Airworthiness manual (Doc. 9760), Volume II, Part A, Chapter 3. The procedures contained therein (ALS) must be taken into account when considering any variation requests. A.

R

ALS Part 4 applicability The applicability of this ALS Part 4 revision is restricted to the aircraft series, models and Weight Variants (WV) series listed in the table below: Aircraft series

R R R R R R R R R R R R R R R R R

A330-200

A330-200F

A330-300

Aircraft models A330-201 A330-202 A330-203 A330-223 A330-243 A330-223F A330-243F A330-301 A330-302 A330-303 A330-321 A330-322 A330-323 A330-341 A330-342 A330-343

Note:

WV WV020 series, WV050 series, WV060 series WV020 series, WV050 series, WV060 series WV020 series, WV050 series, WV060 series WV020 series, WV050 series, WV060 series WV020 series, WV050 series, WV060 series WV000 series WV000 series WV000 series, WV010 series, WV050 series WV050 series WV050 series WV000 series, WV010 series WV000 series, WV010 series WV020 series, WV050 series WV000 series, WV010 series WV000 series, WV010 series, WV020 series, WV050 series WV020 series, WV050 series

The engine Time Limits and Maintenance Checks are not included in this manual: Refer to the relevant Engine Manufacturer Chapter 05 manual.

A330 AIRWORTHINESS LIMITATIONS SECTION B.

Ageing Systems Maintenance (ASM)

R

Airbus’ definition of Ageing Systems Maintenance (ASM) primarily refers to preventative maintenance requirements (including replacements) and associated airworthiness limitations applicable to aircraft systems susceptible to ageing effects. Such ageing effects could change the characteristics leading to an increased potential for failure, which in isolation or in combination with one or more other specific failures or events, could result in an unsafe condition of the aircraft.

R

Failure-finding checks (addressing similar unsafe conditions) with airworthiness limitations will also be included to complement the mandatory preventative maintenance requirements (refer also to ALS sub-part 4-0, paragraph 1.D).

D Note: Items listed in this ALS Part 4 may originate from: Aircraft Maintenance Manual (AMM) chapter 05 Service Life Limits and Maintenance Checks (SLMC) section 05-11-00 Service Life Limits, subsequently transferred into the A330 ALS Part 1. Life extension study. Continued Airworthiness (operational safety) issues (in-service experience). All the maintenance requirements and associated airworthiness limitations indicated in this document were defined by a process agreed between AIRBUS and the European Aviation Safety Agency (EASA). The publication of this document precludes the necessity to publish individual Airworthiness Directives (AD) for each listed item and its requirements. R D N N N R R R

N R R N N N N

C. A330 aircraft systems utilisation The limitations published in this document have been identified in consideration of a maximum number of Flight Hours (FH)/Flight Cycles (FC) that may be accrued by an individual aircraft, as follows: Aircraft series A330-200 series PRE 49144 (3)

OR

A330-200 series POST 49144 (3) A330-200F series A330-300 series PRE 49144 (3) A330-300 series POST 49144 (3)

OR

Flight Hours 060000 100000 (2) 100000 100000 060000 80000 (1) 100000 (2) 100000

Flight Cycles 40000 33000 (2) 33000 33000 40000 20000 (1) 33000 (2) 33000

Depending on fleet leader operation, the impact of a greater aircraft accumulated FH/FC value may subsequently be investigated and might demonstrate a need for new or revised limitations. As a consequence, should any operator envisage future aircraft operations beyond the quoted values, they must first contact Airbus for advice.

A330 AIRWORTHINESS LIMITATIONS SECTION N N

(1) Applies only to aircraft POST MODification (MOD) 58269/Service Bulletin (SB) A330-00-3068 R00.

R

(2) Applies only to aircraft POST MOD 200103/Service Bulletin (SB) A330-00-3068 R01.

N N N

(3) Within the context of ALS Part 4, MOD 49144 is used to identify WV050 and WV060 series aircraft (Enhanced aircraft) since this modification cannot be retrofitted on WV000, WV010 and WV020 series aircraft.

R

Note: When different sets of aircraft systems utilisation values are indicated for a given aircraft series, no combination of values extracted from different sets is permitted.

D D. ALS Part 3 and ALS Part 4 correlation R

At time of original Type Certification (TC) and Post TC design changes, an appraisal of aircraft systems is carried out within the frame of the Systems Safety Assessments. This may identify a need to schedule repetitive maintenance tasks within a defined interval so as to maintain the required safety objectives for individual failure conditions. A subset of these tasks, the majority of which detect latent failures, are identified as Certification Maintenance Requirements (CMR). These constitute operational limitations and are mandated through their location in the ALS Part 3.

D E.

Sub-part 4-2: SYSTEMS LIFE-LIMITED COMPONENTS Sub-part 4-2 is approved by the EASA.

R

Components/items listed under this sub-part are those affected by a replacement requirement associated to a life limitation and whose failure could contribute to an unsafe condition of the aircraft. For a given PNR, when more than one set of limitations (FH/FC/Calendar time) is published for the same application, it is the Operator/MRO’s responsibility to select the appropriate set depending on the aircraft utilisation. Combining the limitations from different sets is not permitted.

R R R R D

Sub-part 4-2-1: Life Limits Components/items listed under this sub-part are those having a life limit due to failure during tests and whose failure could result in an unsafe condition of the aircraft. Sub-part 4-2-2: Current Demonstrated Lives Components/items listed under this sub-part are those having a demonstrated life limitation, which is temporary waiting for completion of the tests.

A330 AIRWORTHINESS LIMITATIONS SECTION F.

Sub-part 4-3: SYSTEMS INSTALLATIONS MAINTENANCE REQUIREMENTS Sub-part 4-3 is approved by the EASA.

R R

The maintenance tasks given in this sub-part includes airworthiness limitations set to prevent the aircraft systems failures, which could contribute to an unsafe condition of the aircraft. Note: Credit may be taken for accomplishment of the Maintenance Review Board Report (MRBR) Systems and Powerplant section maintenance tasks, providing that they are performed with the same inspection level, at least as frequently as the inspection threshold and interval quoted in this document. Sub-parts 4-3-1 and 4-3-2 give maintenance requirements and airworthiness limitations at component level and aircraft (system) level respectively.

R

Sub-part 4-3-1: Controlled at component/sub-assembly level This sub-part identifies tasks controlled at component/item level. The recurrent maintenance requirements are applicable no later than the item, not the aircraft, reaching the airworthiness limitation. When items given in sub-part 4-3-1 reach the stated airworthiness limitations, the given task must be carried out. Any item removed from the aircraft for any reason, (such as failure of functional check, degradation of condition, etc) must be replaced by a serviceable item, which has not reached the stated airworthiness limitations. Sub-part 4-3-2: Controlled at aircraft system level This sub-part identifies tasks at aircraft level. The recurrent maintenance requirements are applicable no later than the aircraft, not the item, reaching the airworthiness limitation. The tasks listed in sub-part 4-3-2 must be carried out when the aircraft reaches the stated airworthiness limitation. Should a failure to reach the task requirements be detected, the appropriate trouble-shooting must be carried out and the relevant suspected items replaced in accordance with the Aircraft Maintenance Manual (AMM) procedures. Following any replacements, the listed tasks must be repeated until a successful task recording can be entered. G. Traceability and replacement/maintenance requirements In order to maintain aircraft airworthiness, it is mandatory to replace components/items listed under sub-part 4-2 at or prior to whichever of the life limitations occurs first, after any necessary adjustment of the stated life limitations. It is also mandatory to perform/repeat the maintenance requirements listed in sub-part 4-3 at or prior to whichever of the limitations threshold/interval occurs first, after any necessary adjustment of the stated airworthiness limitations.

A330 AIRWORTHINESS LIMITATIONS SECTION Airworthiness limitations (including life limitations) must be adjusted as necessary in accordance with the instructions of paragraph 1.H. of this ALS subpart 4-0. Therefore, it is necessary to assure traceability and monitoring of the components/items listed in the sub-parts 4-2 and 4-3-1. Non-compliance with these requirements could suspend the validity of the Certificate of Airworthiness. For a given component/item of the sub-parts 4-2 and 4-3-1, new PNRs may be introduced in the future as a result of modifications and/or Airbus Service Bulletin (SB) publishes. These new PNRs may not be listed in the sub-parts 4-2 and/or 4-3-1 of the current revision of the ALS Part 4. However, it is recommended to maintain traceability and monitoring of such components/items whatever their PNR in case of future introduction in the ALS Part 4. For further guidance, Operators are requested to contact Airbus. Note 1: In the context of the ALS Part 4, traceability means records that clearly demonstrate the history of components/items back to initial entry into service, so that airworthiness limitations are accurately applied. Traceability records may comprise, but are not limited to, the following: Application history (aircraft type, model, WV, MSN i.e. Manufacturer Serial Number, etc…), Maintenance actions carried out (Airworthiness Directives, modifications, repairs, inspections, etc…), Life accumulation (accounting for any individual aircraft to which a component/an item may have been fitted). Note 2: Where the partial/complete life history of a component/an item is not known, Operators are requested to refer to the applicable SIL for guidance. Such SIL provide the means to manage such components/items. They have been issued in agreement with the EASA. Note 3: Traceability and monitoring of component/item listed in sub-part 4-2 is not required for consumable component (for which replacement is controlled at assembly/aircraft level). N N N

In addition to the mandatory traceability and monitoring of the components/items listed in the sub-parts 4-2 and 4-3-1, refer to SIL 05-014 for the Recommended Tracking of components/items, which could be subject to future Airworthiness Limitation. H. Transfers of components/items between aircraft applications The airworthiness limitation(s) for a component/item fitted to an application (aircraft type, aircraft model, etc…) may be different when this component/item is transferred to

A330 AIRWORTHINESS LIMITATIONS SECTION another application. In this case, the component’s/item’s remaining operational life must be calculated using the following formula:

Ca Tr i with: Tri = Caj = Cpj = Cpi =

1

Cp

j j

Cp

i

component/item’s remaining life for operation on current application i. component/item’s accumulated life on previous application j. component/item’s airworthiness limitation in previous application j. component/item’s airworthiness limitation in current application i.

When a component/item has been installed on an application where the ALS Part 4 does not impose an airworthiness limitation, the aircraft systems utilisation values (refer to ALS sub-part 4-0, paragraph 1.C) of the relevant ALS Part 4 for that application must be used.

R R

Note 1: When using the above formula, Tri, Caj, Cpj, and Cpi are expressed in the same usage parameter (FH or FC or landings): Usage parameters cannot be mixed in the same calculation. Note 2: The remaining life calculation must be reassessed every time the component’s/item’s airworthiness limitation(s) change(s) for current and/or previous aircraft application(s) to which the component/item is/was fitted. I.

R

Disposal/quarantine action When the components/items listed in the sub-parts 4-2 and/or 4-3-1 reach the life limitations, disposal/quarantine action must be taken depending on the following categories: For component/item listed in sub-part 4-2-1: They must be mutilated beyond repair limits to prevent rework to appear to be airworthy. Note 1: Some means may exist to extend their potential life provided they are applied prior to reaching the life limit (e.g. Service Bulletin: POST SB PNR in the subpart 4-2-1). Note 2: It’s recommended that the organisation that mutilates a component/item should provide the original manufacturer with the data plate and/or serial number and final disposition of the component to maintain the records of serial numbers for “retired” certified life-limited components/items or other critical components/items.

A330 AIRWORTHINESS LIMITATIONS SECTION For component listed in sub-part 4-2-2 and/or 4-3-1: Appropriate means must be implemented to deter their installation on aircraft pending possible extension of the life limitations. Examples of these means are: Record keeping system, Non-permanent markings, Segregation (items stored separately from those currently eligible for installation). Note:

J.

When components/items are removed by way of a systematic replacement, they must be mutilated beyond repair limits to prevent rework to appear to be airworthy.

Occurrence reporting The ICAO Airworthiness manual (Doc. 9760), Volume II, Part B, Chapter 2 indicates: The concept of Continuing Airworthiness includes the reporting of defects and other significant maintenance and operational information by the Operator to the organisation responsible for the Type Design in accordance with the requirements of the State of aircraft registry.

Accountable persons or organizations shall report to the competent authority and Airbus, any identified condition of an aircraft or component that has resulted or may result in an unsafe condition that hazards seriously the flight safety (Refer to EASA Part M.A.202 and Part 145.A.60). This will enable Airbus to issue appropriate service instructions to all owners or Operators. “Hazard seriously the flight safety” means any instances where safe operation could not be assured or which could lead to an unsafe condition. It typically includes, but is not limited to, significant cracking, deformation, corrosion, any evidence of burning, electrical arcing, significant hydraulic fluid or fuel leakage and any emergency system or total system failure. The finding report should include at least the information stated below: Organisation name, Approval reference if relevant, ASM maintenance requirement reference, Aircraft MSN affected, Identification of the affected component/item, Overhaul, life since new (in FH and/or FC and/or landings and/or Calendar time, as applicable) accumulated by the affected system/component/item at the time of the finding, Location and detailed description of the finding, with indication of the size and orientation, Circumstance of detection and inspection method used. Note:

Report shall be made as soon as practical, but in any case within 72 hours of the organisation identifying the condition to which the report relates. (Refer to EASA Part M.A.202 and Part 145.A.60).

A330 AIRWORTHINESS LIMITATIONS SECTION K.

ALS Part 4 airworthiness limitations Airworthiness limitations quoted in the ALS Part 4 are applicable to the undamaged and unrepaired aircraft systems and components/items. They may need to be adapted in case of damage/repair.

L.

Production/Repair concessions and Alternative Methods Of Compliance Airworthiness limitations of the ALS sub-parts 4-2 and 4-3 may be negated by instructions given in either a Production concession, a Repair design Approval Sheet (RAS), an ALS Variation (AV) or an Alternative Method Of Compliance (AMOC). It is Operator’s responsibility to refer to the applicable limitations. When airworthiness limitations change in a revision of the ALS Part 4 subsequent to the issuance date of the Production concession/RAS/AV/AMOC, Operators are requested to contact Airbus for guidance. The restrictions of airworthiness limitation(s) indicated in the RAS/AV/AMOC (or absence thereof) depend on the component’s/item’s accumulated life considered during the original evaluation of the repair solution/AV/AMOC. Occasionally, repair solutions/AV/AMOC are evaluated on the basis of an accumulated life that includes a conservative life calculation (refer to the applicable Service Information Letter). Such AV/AMOC/repair solutions MUST be re-evaluated by Airbus before Operators can take credit of the history partially or completely rebuilt after application for the repair solution/AV/AMOC. Production concessions are provided to the initial Operator of the aircraft in the delivery documentation (Aircraft Inspection Report: “Recordable concessions”). Note: For spares, restrictions of airworthiness limitation(s), if any, are indicated in EASA Form 1 block “Remark” (directly or by reference to another document).

M. Modifications/Repairs not developed under Airbus DOA Certificate EASA.21J.031

R

R

If an aircraft/a sub-assembly/a component/an item has a modification or repair embodied that has not been developed under the Design Organisation Approval (DOA) Certificate EASA.21J.031 (e.g. under a Supplemental Type Certificate) and which affects the content of the ALS Part 4, the Operator is responsible for obtaining approval by the relevant Airworthiness Authority for any necessary adaptations of the airworthiness limitations. When such an aircraft/a sub-assembly/a component/an item is transferred from one Owner/Operator to another, the associated approvals and documents indicating the necessary adaptations of airworthiness limitations must be transferred as well.

A330 AIRWORTHINESS LIMITATIONS SECTION 2.

DEFINITIONS The initial entry into service is defined for the aircraft (systems installations) as: The date of Transfer of Title to the first Operator for airworthiness limitations in Calendar times, unless otherwise stated in any delivery documentation to the first Operator. The date of aircraft first flight for airworthiness limitations in flight hours and/or flight cycles and/or landings. The initial entry into service for the transferable systems components/items is defined as the date at which the component/item accomplishes the first flight for which it will undertake its intended function. Note: Unless otherwise stated, this means for transferable components/items delivered on new aircraft (i.e. from Airbus Final Assembly Line) that the life accumulated between aircraft first flight and the aircraft delivery date/transfer of title date (e.g. as a result of test flights) must be taken into account. Calendar times (Cal.):

Airworthiness limitations in Years (Ye), Months (Mo), etc… must be counted from the date of initial entry into service (unless otherwise stated). In considering the accumulated time since the initial entry into service, it should be noted that Calendar time usage parameter cannot be frozen (unless stated for individual components/items).

Exceptional Short Term Extension: An extension in an ASM airworthiness limitation that may be needed to cover an uncontrollable or exceptional unexpected situation. Flight Cycle (FC):

A complete takeoff and landing sequence.

Flight Hour (FH):

The accumulated time intervals between “wheels-off” and “wheels-on”.

Functional Check:

A quantitative check to determine if a component/an item performs one or more of its functions within specified limits.

Interval:

The period expressed in usage parameters like FH and/or FC and/or LanDinGs and/or Calendar time between consecutive accomplishments of a specific task, excluding any exceptional short-term extensions from calculations.

Landing (LDG):

An operation of an aircraft touching the runway and coming to a complete stop or performing a “touch and go”.

A330 AIRWORTHINESS LIMITATIONS SECTION D

3.

Operational Check:

A qualitative check to determine that a component/an item is fulfilling its intended purpose. It is a failurefinding task and does not require quantitative tolerances.

Threshold:

The initial accomplishment of a specific maintenance task from the initial entry into service. It may be expressed in usage parameters like FH and/or FC and/or LDG and/or Calendar time.

Touch and go:

A landing in which an aircraft touches the runway and does not come to a full stop prior to commencing an additional flight. In the sub-part 4-3, touch and go cycles can be neglected if they are less than 5% of the total number of FC up to threshold inspection or between two consecutive inspections. Each “Touch and go” above 5% is to be counted as one FC/LDG, up to threshold inspection or between two consecutive inspections.

RULES SPECIFIC TO SUB-PART 4-2 A. Authorised systems components/items ALS sub-part 4-2 tables provide the applicable life limitations only for systems components/items that have been authorised. These tables do not ensure that a PNR has been validated for a specific individual aircraft MSN. PNR are authorised for installation on individual aircraft MSN by SB and/or the associated modifications, which are published by Airbus. PNR provided by sub-parts 4-2-1 and 4-2-2 for ATA 32 items relate to detail parts. They may not all be listed in Illustrated Parts Catalogue (IPC) issued by Airbus. This is the case, for example, when the procurable replacement part is delivered as an assembly. Messier-Dowty SBs have been/will be issued to provide information on procurable replacement PNR, detail PNR and applicable SB: Messier-Dowty Ltd Service Bulletin number: A33/34-32-85 (main landing gear PRE MOD 43029 – ‘basic’), A33/34-32-88 (main landing gear POST MOD 43029 – ‘growth’ or POST MOD 47487 – ‘growth scallop’), A33/34-32-258 (main landing gear POST MOD 54500 – ‘enhanced’). Messier-Dowty SA Service Bulletin number: D23285-32-040 (nose landing gear).

A330 AIRWORTHINESS LIMITATIONS SECTION Detail parts are listed in the relevant Component Maintenance Manuals (CMM). The Messier-Dowty SB listed above provides the procurable replacement Part Numbers. B. Life limitation/Replacement time indication (1) General The life limitation indicated against PNR originally fitted is counted from the component’s/item’s initial entry into service. The life limitation indicated against PNR evolutions is also to be counted from the component’s/item’s initial entry into service (unless otherwise stated).

Note: Where component/item history is unknown/partially unknown, refer to Note 2 paragraph 1.G. In computing components’/items’ life, calculations must include flight hours and/or flight cycles and/or landings and/or Calendar time (as applicable) since the initial entry into service of the component/item (unless otherwise stated).

(2) ALS sub-part 4-2 life limitations The life limitation/replacement time indication is quoted on the same line/block of lines as the PNR. C. Life limitation applicability Life limitation applicability is allocated to aircraft affected (for all aircraft of the column in sub-part 4-2), according to: (1) Aircraft type, series and model, e.g. ALS sub-part 4-2 table headers indicate aircraft models. When ‘x’ is entered in the model number, it stands for any number within the limits of the list of models given in the paragraph 1.A. of this sub-part, e.g.: A330-30x

stands for:

A330-301, A330-302 and A330-303.

Life limitation applicability is allocated according to the aircraft model affected, e.g.: X

stands for:

-223

stands for:

excl. -341

stands for:

All A330 models defined by the applicability of the column. A330-223 model only, defined by the applicability of the column. All A330 models defined by the applicability of the column, excluding the A330-341 model.

A330 AIRWORTHINESS LIMITATIONS SECTION (2) Aircraft weight variant, e.g. ALS sub-part 4-2 table headers indicate aircraft WV. When ‘x’ is entered in the WV number, it stands for any number within the limits of the list of WV’s defined in the tables of the paragraph 1.A. above. (3) Aircraft Manufacturer Serial Number, e.g.

4.

XXX–YYY

stands for:

XYX, XXZ XZX excl. XXX

stands for: stands for: stands for:

From aircraft MSN XXX to aircraft MSN YYY (for all aircraft defined by the applicability of the column). For aircraft MSN XYX and aircraft MSN XXZ. For aircraft MSN XZX only. For all aircraft (defined by the applicability of the column), excluding MSN XXX.

RULES SPECIFIC TO SUB-PART 4-3 A. Airworthiness limitations (1) General

R R

In computing the life accumulated by the aircraft systems/components/items, calculations must include flight hours and/or flight cycles and/or landings and/or calendar time (as applicable) since the initial entry into service of the component/item (unless otherwise stated).

(2) ALS sub-part 4-3 airworthiness limitations The limitations must be applied from: The initial entry into service for the threshold and The original due date of the last accomplishment of the task, excluding any exceptional short-term extensions from calculations, for the interval. When alternative inspection methods are provided, the next interval applicable is the one associated with the inspection method used at last inspection. B. ALS sub-part 4-3 layout. The maintenance requirements and associated airworthiness limitations are presented in the ALS sub-part 4-3 in accordance with the following method: (1) Task Number The task numbering system follows a similar format to the Maintenance Planning Document (MPD) system and is described as follows: Each task is identified by a specific task number. When a task applies to two specific main zones located symmetrically to either side of the aircraft centerline,

A330 AIRWORTHINESS LIMITATIONS SECTION the task is assigned a single task number, but both LH and RH zones are indicated in "Zone" column. The task number comprises 13 digits organised as follows: XXXXXX-MEFYY-Z-E XXXXXX M E F

YY Z E

is ATA 100 task reference. is the selection methodologies used. It will always be “0”. is engine/APU/… manufacturer identification (where applicable, “0” is default value). is engine/APU type information when more than one engine from the same manufacturer is applicable to the program (where applicable, “0” is default value). is sequential number. is for technical solution applicable to the same task requirement. is “E” and stands for ASM (i.e. task related to an ageing systems function or Enhanced maintenance requirement).

(2) Zone column The zone column defines where the major part of the maintenance task requirement is to be carried out on the aircraft. (3) Description column This column provides the following information: (a) Task Description Contains basic description of the maintenance task to be performed. (b) Note Where given, it states further requirements and/or provides useful information. (4) Threshold/Interval columns These columns are used to record the selected threshold and interval for the task. The threshold and interval may be expressed in terms of usage parameters or notes. R R R

The repeat interval starts at the original due date of the last accomplishment of the task, excluding any exceptional short-term extensions from calculations. Usage parameters are defined in the sub-part 4-0 paragraph 2.

A330 AIRWORTHINESS LIMITATIONS SECTION (5) Reference column This column provides reference to Instructions for Continued Airworthiness where maintenance practices/procedures necessary for the task accomplishment are provided, e.g. the AMM. Where reference is made to an Airbus SB, it must be assumed that the latest approved revision of the SB is applicable, but any previous revision is acceptable. Where a particular revision is stated, the revision or any later approved revision must be used. (6) Limitations applicability columns These columns give the combination of component(s)/item(s) PNR and aircraft that requires the accomplishment of the task. (a) PNR ALS sub-part 4-3 tables provide the applicable airworthiness limitations only for systems installations that have been authorised. These tables do not ensure that a PNR has been validated for a specific individual aircraft MSN. PNR are authorised for installation on individual aircraft MSN by SBs and/or the associated modifications, which are published by Airbus. (b) Aircraft Applicability

ALL A330-xxx PRE nnnnn

Task applicable to

All A330 aircraft. A330-xxx series aircraft. All aircraft PRE MOD nnnnn. i.e. A330 that do not have MOD nnnnn embodied.

POST nnnnn

All aircraft POST MOD nnnnn. i.e. A330 that do have MOD nnnnn embodied.

POST nnnnn Sxxxxx

All aircraft POST MOD nnnnn (at least with mod proposal no. Sxxxxx embodied).

POST nnnnn All aircraft POST MOD nnnnn and POST MOD mmmmm. POST mmmmm i.e. A330 that do have MOD nnnnn and MOD mmmmm embodied. POST nnnnn OR PRE mmmmm

All aircraft that do have MOD nnnnn or aircraft that do not have MOD mmmmm.

A330 AIRWORTHINESS LIMITATIONS SECTION Applicability

A330-223 OR A330-341 PRE nnnnn A330-223 POST nnnnn OR A330-341 POST nnnnn PRE mmmmm

Task applicable to

All A330-223, or All A330-341 that do not have MOD nnnnn embodied.

All A330-223 that do have MOD nnnnn embodied, or All A330-341 that do have MOD nnnnn embodied and do not have MOD mmmmm embodied.

POST nnnnn (xx-yyyy)

All aircraft that do have MOD nnnnn embodied. (xx-yyyy) is the SB reference associated modification.

POST xx-yyyy

All aircraft that do have SB A330-xx-yyyy embodied (applicable only to retrofit solution).

GE

All aircraft equipped with GE CF6-80E engines.

PW

All aircraft equipped with PW4100 series engines.

RR

All aircraft equipped with RR Trent 700 engines.

to

the

C. Exceptional short-term extensions for components/items listed in sub-part 4-3. Since ALS sub-part 4-3 intervals are based on statistical averages and reliability rates, an exceptional short-term extension for a specific ALS sub-part 4-3 interval may be made on one aircraft for a limited period of time without compromising the safety objectives declared at Type Certification. Repeated use of such extensions, either on the same aircraft or on similar aircraft in the Operator's fleet, should not be used as a substitute for good management practices. Short-term extensions must not be used for fleet ASM escalation.

Unless noted adjacent to the airworthiness limitation, for all airworthiness limitations identified in the ALS sub-part 4-3, it has been accepted by the Primary Certification Authority (EASA) that short-term extensions up to the following maximum values may be granted without consultation with that office. (1) Controlled by Flight Hours (FH) Extensions up to 10% or 500 FH (whichever is the lesser) may exceptionally be granted on ASM airworthiness limitations quoted in terms of Flight Hours.

A330 AIRWORTHINESS LIMITATIONS SECTION (2) Controlled by Flight Cycles or LanDinGs (FC or LDG) Extensions up to 5% or 250 FC/LDG (whichever is the lesser) may exceptionally be granted on ASM airworthiness limitations quoted in terms of Flight Cycles or LanDinGs. (3) Controlled by Calendar Time (Ye, Mo, etc…) Where the repeat interval is 12 Months or less, extensions up to 10% or 1 month (whichever is the lesser) may exceptionally be granted on ASM airworthiness limitations quoted in terms of Months. Where the repeat interval is greater than 12 Months, extensions up to 2 Months may exceptionally be granted. It is the Operator’s responsibility to identify appropriate procedures with the Authority of the State of aircraft registry for the control and development of his Aircraft Maintenance Programme. Note:

No short-term extensions are permissible for tasks previously required by individual ADs. These items will highlighted by a note in the task description column.

IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE ALS PART 4, THE ALS PART 4 IS THE REFERENCE. LIFE LIMITS (Whichever occurs first)

Explanation notes are located under the assy title. Nomenclature

Part Number

FH

FC/LDG

ATA 26-23-00 FIRE PROTECTION – LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FIG. 01) Pressure reducer D41428 N/A N/A ATA 27-14-00 FLIGHT CONTROL – AILERON AND HYDRAULIC ACTUATION (FIG. 02)

Cal. 20 Ye

A330-2xx WV05x WV060 X X X X X X

WV02x

(1) Applicable to servo-controls in positions Functional Item Number (FIN) 7CS1, 8CS1, 7CS2 and 8CS2 for inboard servo-controls, and FIN 9CS1, 10CS1, 9CS2 and 10CS2 for outboard servo-controls (active and damping). (2) Embodiment of MOD 45512/SB A330-27-3054 introduces different PNR. MOD 45512 factory embodied on MSN 229 and subsequent. Inboard aileron servo-control (1) (2) 3337457-30 32000 Inboard aileron servo-control (1) (2) 3337457-31 32000 Inboard aileron servo-control (1) (2) 3337457-35 32000 Inboard aileron servo-control (1) (2) 3337457-36 32000 Inboard aileron servo-control (1) (2) 3337457-37 32000 Inboard aileron servo-control (1) (2) 3337457-38 32000 Outboard aileron servo-control (1) (2) 3337458-30 32000 Outboard aileron servo-control (1) (2) 3337458-31 32000 Outboard aileron servo-control (1) (2) 3337458-35 32000 Outboard aileron servo-control (1) (2) 3337458-36 32000 Outboard aileron servo-control (1) (2) 3337458-37 32000 Outboard aileron servo-control (1) (2) 3337458-38 32000 ATA 27-23 FLIGHT CONTROL – RUDDER AND PEDAL TRAVEL LIMITING ACTUATION (FIG. 03)

21600 21600 21600 21600 21600 21600 21600 21600 21600 21600 21600 21600

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

X X X X X X X X X X X X X

X

X X X

X

(1) FIN 24CS. (2) FIN 36CS. Rudder Travel Limitation Unit (RTLU) 341400M02 (1) 100000 33000 N/A Pedal Travel Limitation Unit (RTLU) 341400M02 (2) 100000 33000 N/A ATA 27-34-00 FLIGHT CONTROL – ELEVATOR AND HYDRAULIC CONTROL (FIG. 04) (1) Applicable to elevator servo-controls installed in positions FIN 2CS1, 2CS2, 3CS1 and 3CS2 (active and damping). Elevator servo-control (1) SC4800-2 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-3 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-4 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-6 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-7 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-7A N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-8 N/A N/A 31-Aug-04 Elevator servo-control (1) SC4800-9 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-10 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-11 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-72 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-73 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-92 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-93 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-103 N/A N/A 30-Jun-08 Elevator servo-control (1) SC4800-113 N/A N/A 30-Jun-08 ATA 27-44-00 FLIGHT CONTROL – TRIMMABLE HORIZONTAL STABILIZER (THS) HYDRAULIC ACTUATION (FIG. 05) (2) Embodiment of MOD 49590/SB A330-27-3085 introduces different PNR. MOD 49590 factory embodied on MSN 437 and subsequent. 31-Dec-03 THS Actuator 47172 N/A N/A ATA 27-54-00 FLIGHT CONTROL – FLAPS HYDRAULIC ACTUATION AND POWER TRANSMISSION (FIG. 06 & 07)

X X X X X X X X X X X X X X X X X

X X X X X X X X X X

X (2) X

X

X

(1) Embodiment of MOD 50044 and/orMOD 52591 (both associated to SB A330-27-3106) introduces different PNR. MOD 50044 and MOD 52591 factory embodied on MSN 506, MSN 509 thru 521, MSN 524 and subsequent. Flap Rotary Actuator – Type A 697510004 (1) Flap Rotary Actuator – Type A 697510005 (1) Flap Rotary Actuator – Type B 697511004 (1) Flap Rotary Actuator – Type B 697511005 (1) Flap Rotary Actuator – Type B 697511006 (1) Flap Rotary Actuator – Type B 697511007 (1) 953A0000-04 Flap Power Control Unit (PCU) 953A0000-05 Flap Power Control Unit (PCU) 953B0000-01 Flap Power Control Unit (PCU) ATA 27-64-00 FLIGHT CONTROL – SPOILER HYDRAULIC ACTUATION (FIG. 08)

N/A N/A N/A N/A N/A N/A N/A N/A N/A

REF: ALS PART 4-R04 SUB PART 4-2-1

18000 18000 18000 18000 18000 18000 N/A N/A N/A

12 Ye 12 Ye 12 Ye 12 Ye 12 Ye 12 Ye 31-Oct-14 31-Oct-14 31-Oct-14

X X X X X X X X X X

X



Part Number

FH

FC/LDG

Cal.

A330-2xx WV05x WV02x WV060

(1) Not applicable to aircraft POST MOD 44670 and delivered from 13-Jan-2006 onwards. Embodiment of MOD 51413/SB A330-27-3113 introduces different PNR. (2) FIN 13CS1 and 13CS2. (3) FIN 14CS1, 15CS1, 16CS1, 17CS1, 18CS1and 14CS2, 15CS2, 16CS2, 17CS2 and 18CS2. (4) For spoiler servo-controls with unknown history of life accumulation on 31-Aug-2006,their total accumulated life is calculated by addition of the life accumulated by the aircraft they are fitted to on 31-Aug-2006, to their actual life accumulated since. (5) When removed from aircraft, these servo-controls must be scrapped. (6) Applicable to aircraft up to and including MSN 588. For aircraft, which have accumulated on 05-Sep-08 less than or equal to 8500 FC since aircraft initial entry into service, modify all servo-control actuators in accordance with SB A330-27-3110 no later than 05-Mar-2010. For aircraft, which have accumulated on 05-Sep-08 more than 8500 FC since aircraft initial entry into service, modify the servo-control actuators in accordance with SB A330-27-3110: If 3 hydraulic circuits are affected: (a) On first circuit within 10400 FC since aircraft initial entry into service. (b) On second circuit within 10800 FC since aircraft initial entry into service. (c) On third circuit no later than 05-Mar-2010. If 2 hydraulic circuits are affected: (a) On first circuit within 10800 FC since aircraft initial entry into service. (b) On second circuit or no later than 05-Mar-2010. If 1 hydraulic circuit is affected: no later than 05-Mar-2010. (7) Embodiment of MOD 48956/SB A330-27-3094 introduces different PNR. MOD 48956 factory embodied on MSN 422, MSN 443 and subsequent.

Spoiler servo-control in position 1 (2) MZ4339390-01X (1) (5) N/A Spoiler servo-control in position 1 (2) MZ4339390-02X (1) (5) N/A Spoiler servo-control in position 1 (2) MZ4339390-10X (1) (5) N/A Spoiler servo-control in position 1 (2) MZ4339390-12 (1) (5) N/A Spoiler servo-control in position 1 (2) S4-3000470 (1) (5) N/A Spoiler servo-control in position 1 (2) S4-3000470-01 (1) (5) N/A Spoiler servo-control in position 1 (2) S4-3000470-02 (1) (5) N/A Spoiler servo-control in position 1 (2) S4-3000470-03 (1) (5) N/A Spoiler servo-control in position 1 (2) 1387A0000-01 (7) N/A Spoiler servo-control in position 1 (2) 1387B0000-01 (7) N/A Spoiler servo-control in positions 2 to 6 (3) MZ4306000-01X (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) MZ4306000-02X (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) MZ4306000-10X (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) MZ4306000-12 (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) S4-3000460 (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) S4-3000460-01 (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) S4-3000460-02 (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) S4-3000460-03 (1) (5) N/A Spoiler servo-control in positions 2 to 6 (3) 1386A0000-01 (7) N/A Spoiler servo-control in positions 2 to 6 (3) 1386B0000-01 (7) N/A ATA 27-84 LIFT AUGMENTING - SLATS HYDRAULIC ACTUATION AND POWER TRANSMISSION (FIG. 09) (1) Comply with these requirements no later than 31-Oct-2014. T-Gearbox (TGBx) 921A0000-01 N/A T-Gearbox (TGBx) 921B0000-01 (1) N/A T-Gearbox (TGBx) 921C0000-01 (1) N/A T-Gearbox (TGBx) 921D0000-01 (1) N/A ATA 32-11-00 MAIN LANDING GEAR (FIG. 11 to 13 & 16 to 17) MAIN STRUT AND DRESSINGS (FIG. 11 & 13)


11000 11000 11000 11000 11000 11000 11000 11000 N/A N/A 6000 6000 6000 6000 6000 6000 6000 6000 N/A N/A

N/A N/A N/A N/A N/A N/A N/A N/A 31-Dec-03 31-Dec-03 N/A N/A N/A N/A N/A N/A N/A N/A 31-Dec-03 31-Dec-03

X X X X X X X X X X X X X X X X X X X X X

X X X X X X X X X X X X X X X X X X X X X

N/A 32000 24000 24000

31-Oct-14 N/A N/A N/A

X X X X X X

X X X X X X



Part Number

FH

FC/LDG

Cal.

A330-2xx WV05x WV02x WV060

(7) Embodiment of MOD 46903/SB A330-32-3096 introduces a different PNR. MOD 46903 factory embodied on original landing gear ofMSN 271 and subsequent. (8) Embodiment of MOD 46904/SB A330-32-3095 introduces a different PNR. MOD 46904 factory embodied on original landing gear ofMSN 271 and subsequent. (9) Embodiment of MOD 48066/SB A330-32-3123 introduces a different PNR. MOD 48066 factory embodied on original landing gear ofMSN 366 and subsequent. (10) Life limit is the later of 900 aircraft FH counted from08-Jul-2009 or the accumulation of 11150 total LDG since initial entry into service of Pin W1 on any aeroplane. (11) Life limit is the earlier ofthe 10 year calendar limit or the limitation deduced from Note (10). (12) Embodiment of MOD 58527/SB A330-32-3229 introduces a different PNR.

Pin W Pin W Pin W Retraction link (LH) Retraction link (LH) Retraction link (RH) Retraction link (RH) Pin W1 Pin W1 Retraction bracket (LH) Retraction bracket (LH) Retraction bracket (RH) Retraction bracket (RH) Pin W2 Pin W2 Pin W2 Pin P Pin P RETRACTION ACTUATOR (FIG. 11 & 16)

201275796 (7) 201478613 201489770 201275317 (9) 201489311 (12) 201275318 (9) 201489312 (12) 201275673 (7) (11) 201478614 201428351 201428378 201428352 201428379 201275667 (8) 201478615 201478637 201275602 (7) 201478612

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

20000 42800 42800 35200 8400 35200 8400 (10) (10) 19800 19800 19800 19800 9400 42800 42800 20000 42800

10 Ye N/A N/A 36 Mo N/A 36 Mo N/A 10 Ye N/A N/A N/A N/A N/A 5 Ye N/A N/A 10 Ye N/A

X X X X X X X X X X X X X X X X X X X

X X X X X X X X X X X X X X X X X X X

8080 8080 5500 18000 18000 27790 22900 22900

31-Dec-07 31-Dec-07 N/A N/A N/A N/A N/A N/A

30000 30000 30000

N/A N/A N/A



N/A

20 Ye

X

X

N/A

20 Ye

X

(1) Rework in accordance with SB A330-32-3216 (MOD 56557) may introduce a different PNR. (2) Embodiment of MOD 200837/SB A330-32-3243 may introduce a different PNR. MOD 200837 factory embodied on original landing gear of MSN 1195 and subsequent for A330 series excluded A330-200F. MOD 200837 factory embodied on original landing gearof MSN 1092 and subsequent for A330-200F series. Retraction actuator piston rod 114256309 N/A Retraction actuator piston rod 114256321 (1) N/A Retraction actuator piston rod 114256323 N/A Retraction actuator piston rod 114256326 N/A Retraction actuator piston rod 114256328 N/A Retraction actuator gland 50-2113004-00 (2) N/A Retraction actuator cylinder 114256310 N/A Retraction actuator cylinder 114256320 N/A ATA 32-21-00 NOSE LANDING GEAR (FIG. 14 & 15) RETRACTION ACTUATOR (FIG. 15) Retraction actuator body D61954 N/A Retraction actuator body D61954-10 N/A Retraction actuator body D67876 N/A ATA 35-13-00 OXYGEN – CREW OXYGEN – CONTROL AND INDICATING (FIG. 18) Pressure switch CMK80-01 N/A ATA 35-23-00 OXYGEN – PASSENGER OXYGEN (GASEOUS) – CONTROL AND INDICATING (FIG. 19) Quantity calculation control unit E69027 80000


IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE ALS PART 4, THE ALS PART 4 IS THE REFERENCE. LIFE LIMITATIONS (Whichever occurs first)


Part Number

FH

FC/LDG

Cal.

ATA 27-14-00 FLIGHT CONTROL – AILERON AND HYDRAULIC ACTUATION (FIG. 02)

A330-2xx WV05x WV02x WV060 X X

(1) Applicable to servo-control installed in positions FIN 7CS1, 8CS1, 7CS2 and 8CS2 for inboard servo-controls, and FIN 9CS1, 10CS1, 9CS2 and 10CS2 for outboard servo-controls (active and damping). Inboard aileron servo-control (1) 3337457-59 110000 N/A Outboard aileron servo-control (1) 3337458-59 110000 N/A ATA 27-44-00 FLIGHT CONTROL – TRIMMABLE HORIZONTAL STABILIZER (THS) HYDRAULIC ACTUATION (FIG. 05)

N/A N/A

X X

X X

(1) Embodiment of MOD 54880/SB A330-27-3137 introduces different PNR. (2) Embodiment of MOD 200698/SB A330-27-3172 introduces different PNR. (3) Embodiment of MOD 58916/SB A330-27-3172 introduces different PNR. MOD 58916 factory embodied on MSN 1095 and subsequent. THS Actuator 47172-300 (1) THS Actuator 47172-300 (1) THS Actuator 47172-500 (2) THS Actuator 47172-500 (2) THS Actuator 47172-510 (3) THS Actuator 47172-510 (3) THS Actuator 47172-520 THS Actuator 47172-520 THS Actuator 47172-530 THS Actuator 47172-530 ATA 32-11-00 MAIN LANDING GEAR (FIG. 11 to 13 & 16 to 17) MAIN STRUT AND DRESSINGS (FIG. 11 & 13) (1) This PNR is common to pin W2 and pin P. Pin W 55-2105061-00 Retraction link (LH) 50-2105026-00 Retraction link (LH) 50-2105224-00 Retraction link (LH) 201489315 Retraction link (RH) 50-2106026-00 Retraction link (RH) 50-2106224-00 Retraction link (RH) 201489316 Pin W1 55-2105060-00 Pin W1 201478652 Retraction bracket (LH) 50-2105027-00 Retraction bracket (RH) 50-2106027-00 Pin W2 55-2105059-00 (1) Pin P 55-2105059-00 (1) COMPLETE SIDE STAY (FIG. 13) LOCK STAY ACTUATOR (FIG. 17) RETRACTION ACTUATOR (FIG. 11 & 16) (1) Must be replaced by a new one every time the piston head is removed from the piston rod. Retraction actuator piston rod 50-2113002-00 Retraction actuator gland 114256312 Retraction actuator gland 114256322 Retraction actuator gland 50-2113004-01 Retraction actuator piston head 114256308 Retraction actuator piston head 114256639 Retraction actuator piston head 50-2113003-00 Retraction actuator insert 114256629 Retraction actuator cylinder 50-2113001-00 ATA 32-21-00 NOSE LANDING GEAR (FIG. 14 & 15) (1) ‘xx’ at the end of the PNRs stands for any number between 00 and 99. Retraction actuator pin (airframe side) (1) F53112357200xx Retraction actuator pin (airframe side) (1) F53112357204xx Retraction actuator pin (airframe side) (1) F53112357204xx Retraction actuator pin (airframe side) (1) F53114022200xx Retraction actuator pin (airframe side) (1) F53114022200xx Retraction actuator pin (airframe side) (1) F53114023200xx Retraction actuator pin (airframe side) (1) F53120422200xx Retraction actuator pin (airframe side) (1) F53120422200xx NOSE LANDING GEAR LEG (FIG. 14) MAIN FITTING-SHOCK ABSORBER STRUCTURE (FIG. 14) Retraction actuator pin (Main fitting side) D61686 RETRACTION ACTUATOR (FIG. 15) Retraction actuator eye end D62588 Retraction actuator eye end D62588-1

60000 65000 60000 65000 60000 65000 60000 65000 60000 65000

40000 20000 40000 20000 40000 20000 40000 20000 40000 20000

25 Ye 25 Ye 25 Ye 25 Ye 25 Ye 25 Ye N/A N/A N/A N/A

X X X X X X X X X X X X

X X X X X X X X X X X X

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

46480 46480 46480 10700 46480 46480 10700 46480 25179 46480 46480 46480 46480

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

X X X X X X X X X X X X X X X X

X X X X X X X X X X X X X X X X


50000 50000 50000 27790 50000 50000 50000 (1) 50000


X X X X X X X X X

X X X X X X X X X

N/A N/A N/A N/A N/A N/A N/A N/A

50000 50000 41250 50000 41250 50000 50000 41250

N/A N/A N/A N/A N/A N/A N/A N/A

X X

N/A

50000

N/A

N/A N/A

50000 50000

N/A N/A


X X X X X X X X X X X

X X X X X X X

IN CASE OF INCONSISTENCY BETWEEN THIS FILE AND THE ALS PART 4, THE ALS PART 4 IS THE REFERENCE. LIFE LIMITATIONS (Whichever occurs first)

Explanation notes are located under the assy title. Nomenclature Retraction actuator eye end Retraction actuator bearing Retraction actuator bearing Retraction actuator bearing Retraction actuator bearing Retraction actuator sliding rod Retraction actuator sliding rod Retraction actuator sliding rod Retraction actuator plug Retraction actuator plug Retraction actuator plug Retraction actuator cylinder Retraction actuator cylinder Retraction actuator cylinder

Part Number

FH

FC/LDG

Cal.

D67840 D61950-1 D61950-10 D67839 D68397 D62328 D62328-1 D67837 D61952 D61952-1 D67838 D62587 D62587-1 D67836

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A

50000 50000 50000 50000 50000 50000 50000 50000 50000 50000 50000 50000 50000 50000

N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A


A330-2xx WV05x WV02x WV060 X X X X X X X X X X X X X X X X X X X X X X X X X X X X

TIME CONTROLLED ITEM TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE Refer to the AMS/CMM for threshold. For next scheduled removal: Refer to the certificate released to service of Component and related CMM. In case the Certificate of released to service of Component not available or not mention, refer to the table below. TASK NUMBER

COMPONENT

applicable P/N

213100-09-1

SAFETY VALVE

ALL

213100-09-1

SAFETY VALVE

ALL

215000-07-1

OZONE CONVERTER

40997003 40997002 40997001

VNA PART NUMBER (for reference only)

DESCRIPTION

215000-07-1

215800-01-1

OZONE CONVERTER

21-32-40

50000 FH OR 12 YE

ALL

REMOVE SAFETY VALVE FOR RESTORATION.

21-32-40

50000 FH OR 12 YE

ALL

20000 FH NOTE 1

ALL

20000 FH NOTE 1

ALL

OZONE CONVERTER

20000 FH NOTE 1

ALL

CSAS OZONE CONVERTER

6000 FH

1256, 1266

12000 FH

1256, 1266

42 MO OR 20000 FH

ALL

REMOVE CONDENSER AND REHEATER FOR CLEANING IN SHOP.

42 MO OR 20000 FH

ALL

REMOVE CONDENSER AND REHEATER FOR CLEANING IN SHOP.

EVERY 6 YEARS: ULB BATTERY REPLACEMENT.

ALL


ALL


ALL

7012-18088-03 40997003 REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK

40997003 40997002 40997001

40997002

40997003 40997002 40997001

40997001

REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK

REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK

ALL 3969A0000K01

215800-02-1

215200-01-1

215200-01-1

237135-01-1

237135-01-1

237135-01-1

CSAS HEAT EXCHANGER

CONDENSER

REHEATER

ULB BATTERY

ULB BATTERY

ULB BATTERY

REMOVE CSAS OZONE CONVERTER FOR CLEANING.

ALL

969A0000-02

968A0000-03

3968B0000K01 969A0000-02

REMOVE CSAS HEAT EXCHANGER FOR CLEANING.

968A0000-03

REFER ULB P/N: DK120 REFER ULB P/N: DK100 ELP362D

DK120


ELP362D


DK120

APPLICABILITY

REMOVE SAFETY VALVE FOR RESTORATION. 7012-18088

215000-07-1

100% INTERVAL

CMM

COCKPIT VOICE RECORDER (CVR)

23-70-03

DISCARD ULB BATTERY

COCKPIT VOICE RECORDER (CVR) DISCARD ULB BATTERY

COCKPIT VOICE RECORDER (CVR) DISCARD ULB BATTERY

AMS A330 I10 A01

23-70-04

TIME CONTROLLED ITEM TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE Refer to the AMS/CMM for threshold. For next scheduled removal: Refer to the certificate released to service of Component and related CMM. In case the Certificate of released to service of Component not available or not mention, refer to the table below. TASK NUMBER 237135-01-1

237135-02-1

COMPONENT ULB BATTERY

ULB

applicable P/N



ELP362D

DK120 DK100

DK120 DK100

DESCRIPTION

CMM



ULB

DK120 DK100

APPLICABILITY ALL

DISCARD ULB BATTERY


23-70-03

EVERY 3 MONTH: ALL BEACON CLEANING (MORE FREQUENTLY UNDER HIGH HUMIDITY CONDITIONS) EVERY 2 YEARS: BEACON CLEANING AND TESTING

23-70-04

EVERY 2 YEARS: ALL BEACON CLEANING AND TESTING

OPERATIONAL CHECK OF THE ULB

237135-02-1

100% INTERVAL

DK120 DK100

COCKPIT VOICE RECORDER (CVR) OPERATIONAL CHECK OF THE ULB

242100-14-1

IDG OIL COOLERS.

ALL

243851-01-1

BATTERY

4059

ALL

CLEAN (IN SHOP) INTEGRATED DRIVE GENERATOR OIL COOLERS. NOTE: TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE SHOP VISIT. NOTE: OFF A/C TASK PREP. : REMOVE IDG OIL COOLERS Z412; REMOVE IDG OIL COOLERS Z422;

4059 BATTERY DC GENERATION

ENGINE SHOP VISIT.

ALL

24-38-52

EVERY YEAR: GENERAL OVERHAUL IAW CMM

ALL

24-38-53

EVERY YEAR: GENERAL OVERHAUL IAW CMM (REPLACEMENT FULL SET OF VENT VALVE IS RECOMMENDED TO SUBSTITUTE VENT VALVE TEST)

ALL

REMOVE BATTERIES 1 AND 2 FOR OVERHAUL. 243851-01-1

BATTERY

405CH

405CH

BATTERY DC GENERATION REMOVE BATTERIES 1 AND 2 FOR OVERHAUL.

AMS A330 I10 A01


COMPONENT BATTERY

applicable P/N


4059

DESCRIPTION

4059 BATTERY DC GENERATION

CMM 24-38-52

REMOVE BATTERIES 1 AND 2 FOR CHECK IN WORKSHOP

100% INTERVAL EVERY 1000 OPERATING HOURS (800 FH): CLEANING, CHARGE BATTERY, ADJUST ELECTROLYTE LEVEL.

APPLICABILITY ALL

EVERY 2000 OPERATING HOURS (1600 FH) OR 6 MONTH: CLEANING, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL.

243851-02-1

BATTERY

405CH

405CH

BATTERY DC GENERATION

24-38-53

EVERY 3000 OPERATING HOURS (2400 FH): PERFORM A REGULAR CHECK INCL. PERIODICAL CHECK, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL.

ALL

24-38-52

EVERY YEAR: GENERAL OVERHAUL IAW CMM

ALL

24-38-53

EVERY YEAR: GENERAL OVERHAUL IAW CMM (REPLACEMENT FULL SET OF VENT VALVE IS RECOMMENDED TO SUBSTITUTE VENT VALVE TEST)

ALL

24-38-52

EVERY 1000 OPERATING HOURS (800 FH): CLEANING, CHARGE BATTERY, ADJUST ELECTROLYTE LEVEL.

ALL

REMOVE BATTERIES 1 AND 2 FOR CHECK IN WORKSHOP

243852-01-2

BATTERY

4059

4059


243852-01-2

BATTERY

405CH

405CH


243852-02-2

BATTERY

4059

4059

BATTERY DC GENERATION REMOVE BATTERY 3 (APU) FOR CHECK IN WORKSHOP

EVERY 2000 OPERATING HOURS (1600 FH) OR 6 MONTH: CLEANING, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL.

243852-02-2

BATTERY

405CH

405CH

BATTERY DC GENERATION REMOVE BATTERY 3 (APU) FOR CHECK IN WORKSHOP

AMS A330 I10 A01

24-38-53

EVERY 3000 OPERATING HOURS (2400 FH): PERFORM A REGULAR CHECK INCL. PERIODICAL CHECK, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL.

ALL


COMPONENT RESERVOIR

applicable P/N 5A3274-X

VNA PART NUMBER (for reference only) 5A3274-5

DESCRIPTION CABIN ESCAPE FACILITIES

CMM

RESERVOIR

5A3274-X

5A3274-8

CABIN ESCAPE FACILITIES

EVERY 3 YEARS: ALL PERFORM OVERHAUL OF RESERVOIR ASSEMBLY INCLUDING HYDROSTATIC TEST IAW CMM NOTE: SERVICE LIFE IS 15 YEARS

25-62-31

ALL EVERY 3 YEARS: PERFORM OVERHAUL OF RESERVOIR ASSEMBLY INCLUDING HYDROSTATIC TEST IAW CMM NOTE: SERVICE LIFE IS 15 YEARS

25-62-19

ALL EVERY 3 YEARS: PERFORM OVERHAUL OF RESERVOIR ASSEMBLY INCLUDING HYDROSTATIC TEST IAW CMM NOTE: SERVICE LIFE IS 15 YEARS

25-62-14

ALL Basic Maintenance Schedule Goodrich specifies that the units be maintained on a scheduled basis, with the time between overhauls not to exceed 36 months.

REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST

256241-01-1

RESERVOIR

4A3598-X

4A3598-X

CABIN ESCAPE FACILITIES REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST

256241-02-1

SLIDE/RAFT

7A1509-XXX

7A1509-027

CABIN ESCAPE FACILITIES RESTORATION OF LIFE RAFTS BY REMOVAL AND REPLACEMENT WITH OVERHAULED.

Special Provisions for Aging Evacuation Slides When the unit reaches 15 years of age, either replace the inflatable assembly or inspect the unit on an annual basis until the unit is retired or the inflatable assembly is replaced. Annual inspections should start within one calendar year (12 months) of the unit reaching 15 years of age. The minimum annual inspection is not considered an overhaul.

AMS A330 I10 A01

APPLICABILITY

25-62-31

REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST

256241-01-1

100% INTERVAL


COMPONENT SLIDE/RAFT

applicable P/N 7A1509-XXX


DESCRIPTION CABIN ESCAPE FACILITIES RESTORATION OF LIFE RAFTS BY REMOVAL AND REPLACEMENT WITH OVERHAULED.

CMM 25-62-14

100% INTERVAL

ALL Basic Maintenance Schedule Goodrich specifies that the units be maintained on a scheduled basis, with the time between overhauls not to exceed 36 months. Special Provisions for Aging Evacuation Slides When the unit reaches 15 years of age, either replace the inflatable assembly or inspect the unit on an annual basis until the unit is retired or the inflatable assembly is replaced. Annual inspections should start within one calendar year (12 months) of the unit reaching 15 years of age. The minimum annual inspection is not considered an overhaul.

AMS A330 I10 A01

APPLICABILITY






CMM 25-62-14

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-14

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY



applicable P/N 7A1539-xxx



CMM 25-62-21

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-21

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-21

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-21

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-12

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-12

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY






CMM 25-62-12

100% INTERVAL


AMS A330 I10 A01

APPLICABILITY



applicable P/N ALL

VNA PART NUMBER (for reference only) ALL

DESCRIPTION

CMM


EMERGENCY LOCATOR TRANSMITTER- 1151324-1 PORTABLE

1151324-1

EMERGENCY LOCATOR TRANSMITTERPORTABLE

25-60-10

EVERY 5 YEARS: RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION.

ALL

25-60-11


ALL

25-63-05


ALL

REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER (ELT(S)) FOR WORKSHOP CHECK.

256532-01-1

EMERGENCY LOCATOR TRANSMITTER- 01N65920 PORTABLE

01N65920

EMERGENCY LOCATOR TRANSMITTERPORTABLE REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER (ELT(S)) FOR WORKSHOP CHECK.

256532-01-1

EMERGENCY LOCATOR TRANSMITTER- S1823502-05 PORTABLE

S1823502-05

EMERGENCY LOCATOR TRANSMITTERPORTABLE REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER (ELT(S)) FOR WORKSHOP CHECK.

AMS A330 I10 A01

APPLICABILITY

Operationally check the ALL slide/raft in accordance with the following schedule: FWD Passenger/Crew Door 1 36 MTHS MID Passenger/Crew Door 1 36 MTHS AFT Passenger/Crew Door 1 36 MTHS Ower Wing Door 1 36 MTHS Emergency Exit 1 36 MTHS Checks may be performed on either side and do not all have to be performed on the same aircraft. RECORD THE RESULT OF "SLIDE DEPLOYMENT" FOR A330 FLEET

OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT

256532-01-1

100% INTERVAL


COMPONENT FIXED EMERGENCY LOCATOR TRANSMITTER

applicable P/N


DESCRIPTION

ELT96A2560000000 ELT96A2560000000 EMERGENCY LOCATOR TRANSMITTER SYSTEM

CMM

FIXED EMERGENCY LOCATOR TRANSMITTER

S1821502-02

S1821502-02

EMERGENCY LOCATOR TRANSMITTER SYSTEM

EVERY 4 YEARS: RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION. EVERY 12 YEARS: REPLACE UPPER AND LOWER SEAL

ALL

25-63-01


ALL

EVERY YEAR REPLACE BATTERIES

ALL

REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION.

256551-01-1

256652-01-1

MEGAPHONE

LIFE VESTS

REFFER TO MEGAPHONE P/N: A12SA, D2567019500065

REFFER TO MEGAPHONE P/N: A12SA, D2567019500065

MEGAPHONE

P0723E-XXX

P0723E105P

LIFE VESTS

DISCARD MEGAPHONE BATTERIES

25-60-12

EVERY 60 MONTHS: ALL AFTER ENTRY INTO SERVICE, BUT NOT LATER THAN 63 MONTH AFTER DATE OF MANUFACTURE PERFORM AN OVERHAULED. IAW CMM 25-60-12

25-60-12


RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT WITH OVERHAULED.

256652-01-1

LIFE VESTS

P0723E-XXX

P0723E105PW

APPLICABILITY

23-24-01

REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION.

256535-02-1

100% INTERVAL

LIFE VESTS RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT WITH OVERHAULED.

AMS A330 I10 A01


COMPONENT LIFE VESTS

applicable P/N P0723E-XXX

VNA PART NUMBER (for reference only) P0723-XXX

DESCRIPTION LIFE VESTS

CMM

LIFE VESTS

P0723E-XXX

P0723-103WC

LIFE VESTS


25-60-07


25-60-07


25-60-15


25-60-15



256652-01-1

LIFE VESTS

P0723E-XXX

P0723-111WC


256652-01-1

LIFE VESTS

P0640-XXX

P0640-101


256652-01-1

LIFE VESTS

P0640-XXX

P0640-103


AMS A330 I10 A01

APPLICABILITY

25-60-07


256652-01-1

100% INTERVAL


COMPONENT LIFE VESTS

applicable P/N P0640-XXX

VNA PART NUMBER (for reference only) P0640-105


CMM

LIFE VESTS

66601-XXX

66601-113

LIFE VESTS


25-64-05

AC-1 LIFE PRESERVER EVERY 5 YEARS: PERFORM A RECERTIFICATION


256652-01-1

LIFE VESTS

216201-0-XXX 216204-0-XXX

216201-0-XXX 216204-0-XXX


AMS A330 I10 A01

APPLICABILITY

25-60-15


256652-01-1

100% INTERVAL

ALL

AC-1000 LIFE PRESERVER EVERY 5 YEARS: IF SEWN CLOSED PACKED LIFE PRESERVER HAVE TO BE RECERTIFIED. EVERY 10 YEARS: IF VACUUM SEALED CLOSED PACKED LIFE PRESERVER HAVE TO BE RECERTIFIED.

25-65-03

10 YEARS AFTER ALL MANUFACTURING DATE: PERFORM AN OVERHAUL. EVERY 10 YEARS IF LIFE JACKET IS VACUUM PACKED IN A NEW CARRYING BAG AND/OR IF CARRYING BAG IS HF WELDED AND VACUUM PACKED: PERFORM AN OVERHAUL. EVERY 2 YEARS IF LIFE JACKET IS PACKED IN A NEW CARRYING BAG AND/OR IF CARRYING BAG IS SEWN: PERFORM AN OVERHAUL.


COMPONENT

applicable P/N


LIFE VESTS


CMM

00002333

IF the lifejacket assembly ALL has Part Number 00002256, 00002264, 00002288, 00002290, 00002291, 00002292, 00002333, 00002402, 00002404, 00002408, 00002409, 00002502, 00002503, 00002507, 00002508. — and its date of manufacture is less than ten years before the current date, then the date of the next Maintenance Check will be Current Date + 10 years.

25-60-21

EVERY 10 YEARS: PERFORM AN OVER PRESSURE TEST IAW CMM

26-22-40

ALL IF A FIRE EXTINGUISHING BOTTLE IS INSTALLED ON AN AIRCRAFT IT IS CLASSIFIED AS PART OF THE SYSTEM AND HAS A HYDROSTATIC TEST INTERVAL OF 10 YEARS.

00002333 LIFE VESTS

LIFE VESTS

A312306A02RFD A312306A02RFD 262100-10-1

ENGINE FIRE EXTINGUISHING

34600028-1

APPLICABILITY

25-60-91


256652-01-1

100% INTERVAL

34600028-1

RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT WITH OVERHAULED. ENGINE FIRE EXTINGUISHING REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING

AS SOON AS IT IS REMOVED FROM THE AIRCRAFT IT BECOMES A PRESSURE VESSEL AND AS SUCH IT HAS A HYDROSTATIC TEST INTERVAL OF 5 YEARS UNDER THE DOT REQUIREMENTS.

AMS A330 I10 A01

ALL


COMPONENT ENGINE FIRE EXTINGUISHING

applicable P/N 473850-1

VNA PART NUMBER (for reference only) 473850-1

DESCRIPTION ENGINE FIRE EXTINGUISHING

100% INTERVAL

CMM 26-21-62

REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING

APPLICABILITY

IF A FIRE EXTINGUISHING ALL BOTTLE IS INSTALLED ON AN AIRCRAFT IT IS CLASSIFIED AS PART OF THE SYSTEM AND HAS A HYDROSTATIC TEST INTERVAL OF 10 YEARS. AS SOON AS IT IS REMOVED FROM THE AIRCRAFT IT BECOMES A PRESSURE VESSEL AND AS SUCH IT HAS A HYDROSTATIC TEST INTERVAL OF 5 YEARS UNDER THE DOT REQUIREMENTS.

262100-15-1

CARTRIDGE

30903899

30903899


26-22-40

DISCARD CARTRIDGE 262100-15-1

CARTRIDGE

446201

446201 ENGINE FIRE EXTINGUISHING

ALL EVERY 10 YEARS: DISCARD CARTRIDGE


FIRE EXTINGUISHING

33600005-3

ALL EVERY 10 YEARS: DISCARD CARTRIDGE

33600005-3


26-20-05

10 YE

26-20-05

5 YE

26-20-76

10 YE

26-20-76

5 YE

ALL


262241-01-1A

FIRE EXTINGUISHING

33600005-3

33600005-3


#N/A

REMOVE BOTTLE FOR WEIGHT CHECK 262241-01-1

FIRE EXTINGUISHING

472412-1

472412-1


ALL


262241-01-1A

FIRE EXTINGUISHING

472412-1

472412-1


#N/A

REMOVE BOTTLE FOR WEIGHT CHECK 262242-01-1

CARTRIDGE

30903899

30903899 APU FIRE EXTINGUISHING DISCARD CARTRIDGE

AMS A330 I10 A01

ALL

26-20-76 EVERY 10 YEARS: DISCARD CARTRIDGE


COMPONENT CARTRIDGE

applicable P/N


446203

DESCRIPTION

446203 APU FIRE EXTINGUISHING

LOWER DECK CARGO COMPT FIREX

ALL

472625-1

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK)

APPLICABILITY ALL

26-21-34 EVERY 10 YEARS: DISCARD CARTRIDGE


100% INTERVAL

CMM

26-20-85

10000 FH

ALL

26-20-84

10000 FH

ALL

26-23-37

10000 FH

ALL

26-23-38

10000 FH

ALL

26-20-85

10 YE

ALL

26-20-84

10 YE

ALL

REMOVE BOTTLE FOR WEIGHT CHECK

262341-01-1


ALL

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR WEIGHT CHECK 472931-2

262341-01-1


ALL

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR WEIGHT CHECK 34900008-2

262341-01-1


ALL

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR WEIGHT CHECK

262341-02-1


472625-X 472931-X 34900008-X 35200003-X

35200003-2 472625-1

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR HYDROSTATIC TEST

262341-02-1


472625-X 472931-X 34900008-X 35200003-X

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR HYDROSTATIC TEST 472931-2

AMS A330 I10 A01


COMPONENT LOWER DECK CARGO COMPT FIREX

applicable P/N


472625-X 472931-X 34900008-X 35200003-X

DESCRIPTION LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK)

100% INTERVAL

CMM

APPLICABILITY

26-23-37

10 YE

ALL

26-23-38

10 YE

ALL

26-21-34

10 YE

ALL

26-23-37 26-23-38

10 YE

ALL

26-24-05

EVERY 2 YEARS: PERFORM AN INSPECTION IAW CMM INCLUDING WEIGHT CHECK

ALL

26-24-05

EVERY 2 YEARS: PERFORM AN INSPECTION IAW CMM INCLUDING WEIGHT CHECK

ALL

26-20-29

EVERY YEAR: PREFORM ALL INSPECTION AND A WEIGHT CHECK OR CHECK PRESSURE GAGE

26-20-29

EVERY YEAR: PREFORM ALL INSPECTION AND A WEIGHT CHECK OR CHECK PRESSURE GAGE

26-20-29

LIFE LIMIT: 10 YEARS

REMOVE BOTTLE FOR HYDROSTATIC TEST 34900008-2 262341-02-1


472625-X 472931-X 34900008-X 35200003-X

LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) REMOVE BOTTLE FOR HYDROSTATIC TEST 35200003-2

262343-01-1


446203

446203 LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) DISCARD CARTRIDGE UNIT

262343-01-1


LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND BULK) DISCARD CARTRIDGE UNIT 30903898

262400-01-1

PORTABLE FIRE EXTINGUISHER

30903898 PORTABLE FIRE EXTINGUISHER

74-00 74-20 74-21 76-00

REMOVE BOTTLES FOR WEIGHT CHECK 74-20

262400-01-1



74-00 74-20 74-21 76-00

REMOVE BOTTLES FOR WEIGHT CHECK 76-00

262400-01-1


BA21741XX-X BA51015 SERIES

PORTABLE FIRE EXTINGUISHER REMOVE BOTTLES FOR WEIGHT CHECK BA21741GSR-2

262400-01-1



PORTABLE FIRE EXTINGUISHER REMOVE BOTTLES FOR WEIGHT CHECK BA21741SR2

262400-02-1



PORTABLE FIRE EXTINGUISHER REMOVE BOTTLES FOR HYDROSTATIC TEST

BA21741GSR-2

AMS A330 I10 A01

(VENDOR RECOMMENDATION IS TO REPLACE THE EXTINGUISHER NO HYDROSTATIC TEST REQUIREMENT)

ALL


COMPONENT PORTABLE FIRE EXTINGUISHER

applicable P/N



DESCRIPTION PORTABLE FIRE EXTINGUISHER

100% INTERVAL

CMM

26-20-29

REMOVE BOTTLES FOR HYDROSTATIC TEST

LIFE LIMIT: 10 YEARS

APPLICABILITY ALL

(VENDOR RECOMMENDATION IS TO REPLACE THE EXTINGUISHER NO HYDROSTATIC TEST REQUIREMENT)

BA21741SR2 262400-02-1



74-00 74-20 74-21 76-00

26-24-05

10 YEARS ALL VENDOR RECOMMENDATION IS TO REPLACE THE EXTINGUISHER WHEN SECOND HYDROSTATIC TEST DUE (20 YEAR)

26-24-05

10 YEARS ALL VENDOR RECOMMENDATION IS TO REPLACE THE EXTINGUISHER WHEN SECOND HYDROSTATIC TEST DUE (20 YEAR)

26-25-12

60 MO

ALL

26-25-36

60 MO

ALL

27-51-20

12 YE

ALL

27-51-20

12 YE

ALL

RUDDER MECHANICAL CONTROL FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR WORKSHOP CHECK

42 MO OR 20000 FH

275, 294, 299, 366

MAIN HYDRAULIC POWER

6 YE


6 YE



74-20 262400-02-1

262541-01-1


LAVATORY FIRE EXTINGUISHING


74-00 74-20 74-21 76-00 ALL


76-00 BA21758

LAVATORY FIRE EXTINGUISHING REMOVE BOTTLE FOR WEIGHT CHECK

262541-01-1


ALL


275117-01-1

COMMAND SENSOR UNIT

065-50001-0100

BA24320A1 065-50001-0100

FLAPS REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE

275117-01-1

COMMAND SENSOR UNIT

065-50001-0200

FLAPS

065-50001-0200

REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 272149-01-1

SPRING-ROD

ALL

291100-05-1

HYDRAULIC FUSE

ALL

F2727156000200

C24960000-1 291100-05-1

HYDRAULIC FUSE

ALL

REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK MAIN HYDRAULIC POWER

2-8181-2

REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK

AMS A330 I10 A01


COMPONENT HYDRAULIC FUSE

applicable P/N


ALL

HYDRAULIC FUSE

ALL

291100-06-1

HYDRAULIC FUSE

ALL

291100-06-1

HYDRAULIC FUSE


6 YE


6 YE


6 YE


31-31-36

EVERY 6 YEARS: ULB BATTERY (AND ORING) REPLACEMENT.

ALL

31-31-36

EVERY 6 YEARS: ULB BATTERY (AND ORING) REPLACEMENT.

ALL

31-31-36

EVERY 2 YEARS: ALL BEACON CLEANING AND TESTING

REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK

REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK MAIN HYDRAULIC POWER

2-8181-2 ALL

REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK MAIN HYDRAULIC POWER

A25317-1 DK120

APPLICABILITY

6 YE


C24960000-1

100% INTERVAL

CMM


A25317-1 291100-06-1

DESCRIPTION

REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK

313300-01-1

ULB BATTERY

REFER TO ULB P/N: DK100-DK120

DIGITAL FLIGHT DATA RECORDING SYSTEM

313300-01-1

ULB BATTERY

REFER TO ULB DK100 P/N: DK100-DK120


313300-03-1

ULB

REFER TO ULB DK120 P/N: DK100-DK120


DISCARD ULB BATTERY

DISCARD ULB BATTERY

OPERATIONAL CHECK OF THE ULB

321100-01-1

MAIN LANDING GEAR

ALL

ALL

MAIN LANDING GEAR

17000 FC OR

10 YEARS

ALL

REMOVE MAIN GEAR FOR RESTORATION NOTE: - RESTORATION TO BE PERFORMED IN ACCORDANCE WITH AIRBUS APPROVED VENDOR SB

321100-02-1

HYDRAULIC FUSE

ALL

71178-2

FUNCTIONAL CHECK OF MLG BOGIE BEAM PITCH TRIMMER CONTROL MANIFOLD HYDRAULIC FUSE (OFF AIRCRAFT).

10 YE

ALL

321100-02-1

HYDRAULIC FUSE

ALL

71179-2

FUNCTIONAL CHECK OF MLG BOGIE BEAM PITCH TRIMMER CONTROL MANIFOLD HYDRAULIC FUSE (OFF AIRCRAFT).

10 YE

ALL

AMS A330 I10 A01


COMPONENT NOSE GEAR

applicable P/N ALL

VNA PART NUMBER (for reference only) ALL

DESCRIPTION

100% INTERVAL

CMM

NOSE GEAR

17000 FC OR

10 YEARS

APPLICABILITY ALL

REMOVE NOSE GEAR FOR RESTORATION NOTE: - RESTORATION TO BE PERFORMED IN ACCORDANCE WITH AIRBUS APPROVED VENDOR SB

351141-01-1

351200-06-1

OXYGEN CYLINDER

PRESSURE REDUCER TRANSMITTER

897-SERIES

89794015 CREW OXYGEN

ALL

35-21-93

EVERY 5 YEARS: PERFORM A HYDROSTATIC TEST

ALL

REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND FUNCTIONAL CHECK OF OXYGEN CYLINDER PRESSURE GAUGE.

MAX. SERVICE LIFE: 15 YEARS

CREW OXYGEN

72 MO

ALL

72 MO

ALL

72 MO

ALL

15 YE

ALL (PASSENGER OXYGEN ( CHEMICAL ))

no

10 YE

ALL

35-30-02

10 YE

ALL

35-10-25

10 YE

ALL

REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL CHECK (IN WORKSHOP). RCF6708 351315-01-1

OXYGEN MASK REGULATOR

ALL

CREW OXYGEN MASK REGULATOR REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK MF10-05-11

351315-01-1

OXYGEN MASK REGULATOR

ALL

CREW OXYGEN MASK REGULATOR REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK

352142-01-1

OXYGEN GENERATORS

ALL

MF20-534 ALL

PASSENGER OXYGEN (CHEMICAL) DISCARD CHEMICAL OXYGEN GENERATORS

353150-01-1

SMOKE HOOD

119003-11 E28180-XX 15-40F-11

119003-11

FLIGHT CREW PORTABLE BREATHING EQUIPT DISCARD PROTECTIVE BREATHING EQUIPMENT

353150-01-1

SMOKE HOOD

15-40F-11

15-40F11


353150-01-1

SMOKE HOOD

E28180-XX

FLIGHT CREW PORTABLE BREATHING EQUIPT DISCARD PROTECTIVE BREATHING EQUIPMENT E28180-10

AMS A330 I10 A01


COMPONENT SMOKE HOOD

applicable P/N


E28180-XX

DESCRIPTION FLIGHT CREW PORTABLE BREATHING EQUIPT

100% INTERVAL

CMM

APPLICABILITY

35-10-25

10 YE

ALL

35-35-52

EVERY 5 YEARS: PERFORM A HYDROSTATIC TEST OVERHAUL

ALL

DISCARD PROTECTIVE BREATHING EQUIPMENT E28180-20-0001 353200-07-1

PORTABLE OXYGEN CYLINDER

3552 SERIES

PORTABLE OXYGEN REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN REGULATOR (IN WORKSHOP).

SERVICE LIFE: 15 YEARS

3552AAAEAACXCD 353200-07-1


3552 SERIES

PORTABLE OXYGEN

35-35-52

REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN REGULATOR (IN WORKSHOP).

EVERY 5 YEARS: PERFORM A HYDROSTATIC TEST OVERHAUL

ALL

SERVICE LIFE: 15 YEARS

3552AAADAACXCD

353200-07-1


9700-SERIES 9800-SERIES


35-31-55

ALL EVERY 5 YEARS: PERFORM AN OVERHAUL FOR THE 9700-X SERIES AND 80366801 INCLUDING HYDROSTATIC TEST

35-31-55


35-31-55


no

10 YE

ALL

35-30-02

10 YE

ALL

REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST (IN WORKSHOP).

9700-C1A-BF23B

353200-07-1



PORTABLE OXYGEN CYLINDER REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST (IN WORKSHOP).

9700-A1A-BF23B

353200-07-1



PORTABLE OXYGEN CYLINDER REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST (IN WORKSHOP).

353250-01-1

SMOKE HOOD

119003-11 E28180-XX 15-40F-11

9700-C1A-BF23A 119003-11


353250-01-1

SMOKE HOOD

15-40F-11

15-40F11


AMS A330 I10 A01


COMPONENT SMOKE HOOD

applicable P/N


E28180-XX

DESCRIPTION FLIGHT CREW PORTABLE BREATHING EQUIPT

100% INTERVAL

CMM

APPLICABILITY

35-10-25

10 YE

ALL

35-10-25

10 YE

ALL

DISCARD PROTECTIVE BREATHING EQUIPMENT E28180-10 353250-01-1

SMOKE HOOD

E28180-XX


712101-03-1

FORWARD ENGINE MOUNT

ALL

E28180-20-0001 ALL

712106-01-1

FORWARD ENGINE MOUNT

ALL

ALL

DETAILED INSPECTION OF FORWARD ENGINE MOUNT.

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT.

712204-02-1

AFT ENGINE MOUNT

ALL

723100-P3-1

LOW PRESSURE COMPRESSOR GROUP

ALL

ALL

TASK SHOULD BE DONE AT THE OPPORTUNITY OF ENGINE SHOP VISIT, BUT NOT EXCEED "12 YE"

TASK SHOULD BE DONE AT THE OPPORTUNITY OF ENGINE SHOP VISIT, BUT NOT EXCEED "8000 FC OR 52000 FH"

DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFE LINK

TASK SHOULD BE DONE AT THE OPPORTUNITY OF ENGINE SHOP VISIT, BUT NOT EXCEED "8000 FC OR 52000 FH"


REFER TO ENGINE MANUAL

ALL


ALL


ALL


ALL


ALL

DISCARD FAN HUB AND LPC DRUM ROTOR

723200-P1-1


ALL

723500-P1-1

HIGH PRESSURE COMPRESSOR (HPC) ALL

LPC / LPT COUPLING GROUP DISCARD LPC/LPT COUPLING HIGH PRESSURE COMPRESSOR (HPC) DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR

725200-P2-1


ALL

HIGH PRESSURE TURBINE GROUP DISCARD LIFE LIMITED PARTS OF HP TURBINE

725300-P1-1

LOW PRESSURE TURBINE GROUP

ALL

LOW PRESSURE TURBINE GROUP DISCARD LIFE LIMITED PARTS OF LP TURBINE

AMS A330 I10 A01

TIME CONTROLLED ITEM TASK NUMBER AND COMPONENT PART NUMBER CROSS REFERENCE Refer to the AMS/CMM for threshold. For next scheduled removal: Refer to the certificate released to service of Component and related CMM. In case the Certificate of released to service of Component not available or not mention, refer to the table below. TASK NUMBER

COMPONENT

applicable P/N


DESCRIPTION

100% INTERVAL

CMM

APPLICABILITY

AM-256233-00

SURVIVAL KIT

ALL

4A3870-5

REPLACEMENT SURVIVAL KIT AND REVERSE OSMOSIS PUMP OVERHAUL

ITEMS

3 YEARS

ALL

AM-256233-00

SURVIVAL KIT

ALL

4A3870-6

REPLACEMENT SURVIVAL KIT AND REVERSE OSMOSIS PUMP OVERHAUL

ITEMS

3 YEARS

ALL

344100-01-1

RADOME

A9232060600700

A9232060600700

53-51-11 REMOVE RADOME FOR RADIO ELECTRICAL TEST NOTE: TASK APPLICABLE FOR A/C POST 44754 (34-3092) AND INSTALL KELVAR RADOME + A/C POST 44754 (34-3092): MSN 294; 299; 943; 962; 1019; 1256; 1266 + RADOME KELVAR P/N: A9232060600700

30 MONTHS

294, 299, 943,946,962, 1019, 1256, 1266 AND INSTALL KELVA RADOME

ALL

262300-05-1

PRESSURE REDUCER

D41428 ALL

FUNCTIONAL CHECK OF PRESSURE REDUCER (P/N: D41428; P/N E61751-00-0001) NOTE: P/N D41428 LIFE LIMIT 20 YE

ALL

26-20-10

14000 FH ALL

FUNCTIONAL CHECK OF PRESSURE REDUCER (P/N: D41428; P/N E61751-00-0001)

262300-05-1 292400-04-1

PRESSURE REDUCER RAM AIR TURBINE

ALL

E61751-00-0001 ALL

470000-02-1

AIR SEPARATOR MODULES.

ALL

272400-05-2

RUDDER SERVO CONTROL

272400-05-2

26-20-10

14000 FH

REMOVAL OF RAM AIR TURBINE (RAT) FOR OVERHAUL.

ALL

ALL

DISCARD AIR SEPARATOR MODULE

1256; 1266

ALL

31110-120

REMOVE RUDDER SERVO CONTROL FOR WORKSHOP CHECK OF INTERNAL SEALS

33 000 FH

275, 294, 299, 366

RUDDER SERVO CONTROL

ALL

31110-080

REMOVE RUDDER SERVO CONTROL FOR WORKSHOP CHECK OF INTERNAL SEALS

33 000 FH

275, 294, 299, 366

262100-10-1A


ALL

ALL

REMOVE BOTTLE FOR WEIGHT CHECK

5 YE

ALL

256500-01-1VNA

FLASH LIGHT BATTERY

ALL

Replace EMERGENCY FLASHLIGHT BATTERIES at manufacturer's recommendation. NOTE: FOR SUPPLIER DME CORP: SHELF LIFE 4YE

NT

ALL

ALL

AMS A330 I10 A01

A330 AIRCRAFT MAINTENANCE PROGRAM CHAPTER :

21

AIR CONDITIONING / PRESSURIZATION

Task Number

Zone

213100-09-1

210 270

Task Title

PRESSURE CONTROL AND MONITORING

Task code

RS

REMOVE SAFETY VALVE FOR RESTORATION. PREP. : ACCESS THROUGH PANEL OF REAR GALLEY; NOTE: TASK COMPONENT RELATED NOTE: ETOPS SIGNIFICATION SYSTEMS

Threshold Interval

I

50 000 FH

I

12 YE

References

Ctrl

Eff

N

AMM 213152-920-801

ALL

N

AMM 215153-280-801

ALL

N

AMM 215200-100-801 SIL 21-092

ALL

N

AMM 215800-200-801

1256

Check : PCI

Skills :

1.00 MHrs

2 AF 190

215000-07-1

AIR COOLING TEMPERATURE CONTROL

REM

I

20 000 FH

Check : PCI

REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 AF 191 192

215200-01-1

REM

AIR CONDITIONING REMOVE REHEATER AND CONDENSER FOR CLEANING AND LEAKAGE CHECK IN SHOP. NOTE: TASK COMPONENT RELATED NOTE: ETOPS PARALLEL SYSTEM

I

20 000 FH

I

42 MO

Check : PCI

Access panels :

192PB

193DB

Total access time :

4.48 Hrs

Skills :

2.00 MHrs

1 AF 190

215800-01-1

CONDITIONNED SERVICE AIR SYSTEM REMOVE CSAS OZONE CONVERTER FOR CLEANING.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

RFC

I

6 000 FH

1266

Check : PCI

Page : TCI - 21 [1 / 2] ATA

: 21


21


Task Number

Zone

215800-02-1

190

Task Title

CONDITIONNED SERVICE AIR SYSTEM REMOVE CSAS HEAT EXCHANGER FOR CLEANING.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Task code

RFC

Threshold Interval

I

12 000 FH

References

Ctrl

N

AMM 215800-100-801

Eff 1256 1266

Check : PCI

Page : TCI - 21 [2 / 2] ATA

: 21


23

COMMUNICATI0NS

Task Number

Zone

237135-01-1

160

Task Title

Task code

DIS

COCKPIT VOICE RECORDER

Threshold Interval

I

6 YE

References

Ctrl

Eff

N

AMM 237135-920-801

ALL

N

AMM 237100-710-804

ALL

Check : PCI

DISCARD ULB BATTERY NOTE : DATASONIC P/N : HONEYWELL P/N : ULB BATTERY P/N: P/N:

ELP362D 980-6022-001 DK120 DK100 266-E0305-00 NOTE: NATIONAL/VENDOR REQUIREMENT TASK Access panels :

162TW

823

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

2 RA 160

237135-02-1

OP

COCKPIT VOICE RECORDER OPERATIONAL CHECK OF THE ULB NOTE : CVR P/N: S200-0012-00 CVR P/N: 2100-102X-( ) APPLICABLE TO ULB P/N: DK100; DK120 REFER TO CROSS REFERENCE IN CHAPER 3 AMS A330 FOR DETAIL.

I

2 YE

Check : A04

Access panels :

162TW

823

Total access time :

0.00 Hrs

Skills :

0.15 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 23 [1 / 1] ATA

: 23


24

ELECTRICAL POWER

Task Number

Zone

242100-14-1

412 422

Task code

Task Title

CLN

INTEGRATED DRIVE GENERATOR

Threshold Interval

Ctrl

See note

N

AMM 242100-100-801

ALL

N

AMM 243851-280-801 SIL 24-062

ALL

References

Eff

Check : 4C

CLEAN (IN SHOP) INTEGRATED DRIVE GENERATOR OIL COOLERS. NOTE: TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE SHOP VISIT. NOTE: OFF A/C TASK PREP. : REMOVE IDG OIL COOLERS Z412; REMOVE IDG OIL COOLERS Z422; NOTE: ETOPS PARALLEL SYSTEM Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

1 ENG 120

243851-01-1

0.00 MHrs REM

DC GENERATION REMOVE BATTERIES 1 AND 2 FOR RESTORATION NOTE: CMP TASK

I

1 YE

Check : PCI

Skills :

0.15 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 24 [1 / 3] ATA

: 24


24

ELECTRICAL POWER

Task Number

Zone

243851-02-1

120

Task Title

Task code

Threshold Interval

REM

I

1 000 FH

REMOVE BATTERIES 1 AND 2 FOR CHECK IN WORKSHOP P/N: 4059 EVERY 1000 OH (800 FH): CHARGE BATTERY, ADJUST ELECTROLYTE LEVEL. EVERY 2000OH (1600 FH) OR 6 MOUNTH: CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL EVERY YEAR: BATTERY OVERHAUL P/N: 405CH EVERY 3000 OPERATING HOURS (2400 FH): PERFORM A REGULAR CHECK INCL PERIODICAL CHECK, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL. EVERY YEAR: BATTERY OVERHAUL NOTE:NATIONAL/VENDOR REQUIREMENT TASK

I

6 MO

BATTERY DC GENERATION

References

Ctrl

Eff

N

AMM 243851-280-802 SIL 24-062

ALL

N

AMM 243852-280-801 CMP 24-2-0000-007 SIL 24-062

ALL

Check : PCI

Access panels :

132AZ Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 EL 160

243852-01-2

REM

DC GENERATION(APU) REMOVE BATTERY 3 (APU) FOR RESTORATION NOTE: CMP TASK

I

1 YE

Check : PCI

Access panels :

162KW

162RW

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 24 [2 / 3] ATA

: 24


24

ELECTRICAL POWER

Task Number

Zone

243852-02-2

160

Task Title

Task code

Threshold Interval

CHK

I

1 000 FH

REMOVE BATTERY 3 FOR CHECK IN WORKSHOP P/N: 4059 EVERY 1000 OH (800 FH): CHARGE BATTERY, ADJUST ELECTROLYTE LEVEL. EVERY 2000OH (1600 FH) OR 6 MOUNTH: CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL EVERY YEAR: BATTERY OVERHAUL P/N: 405CH EVERY 3000 OPERATING HOURS (2400 FH): PERFORM A REGULAR CHECK INCL PERIODICAL CHECK, CAPACITY CHECK, ADJUST ELECTROLYTE LEVEL. EVERY YEAR: BATTERY OVERHAUL NOTE:NATIONAL/VENDOR REQUIREMENT TASK

I

6 MO

DC GENERATION(APU)

References

Ctrl

N

AMM 243852-280-801 SIL 24-062

Check : PCI

Access panels :

162KW

162RW

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 24 [3 / 3] ATA

: 24

Eff ALL


25

EQUIPEMENT & FURNISHING

Task Number

Zone

AM-256233-00

100

Task Title

RAR

SURVIVAL KIT REPLACEMENT SURVIVAL KIT OSMOSIS PUMP OVERHAUL

831 832 833 834 841 842 843 844

256241-01-1

Task code

I

3 YE

References

Ctrl

N

Eff ALL

Check : PCI

ITEMS AND REVERSE

FUC


Threshold Interval

I

3 YE

N

AMM 256200-780-801

ALL

N

AMM 256200-280-801

ALL

See note Check : PCI

REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST NOTE: NATIONAL/VENDOR REQUIREMENT P/N: 5A3274-XX 4A3598-XX NOTE: THE SERVICE LIFE IS 15 YEARs Skills :

16.00 MHrs

1 AF 831 832 833 834 841 842 843 844

256241-02-1

REM

CABIN ESCAPE FACILITIES REMOVE SLIDE/RAFT FOR RESTORATION NOTE: NATIONAL/VENDOR REQUIREMENT P/N: 7A1509-XXX 7A1539-XXX 7A1508-XXX 7A1510-XXX NOTE: SEE CROSS REFFERENCE & RELATED CMM FOR MORE DETAIL

I

3 YE

Check : PCI

Skills :

16.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 25 [1 / 4] ATA

: 25


25


Task Number

Zone

256241-03-1

000 200

Task Title

Task code

OP


OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT NOTE:NATIONAL/VENDOR REQUIREMENT Operationally check the slide/raft in accordance with the following schedule: FWD Passenger/Crew Door 1 36 MTHS MID Passenger/Crew Door 1 36 MTHS AFT Passenger/Crew Door 1 36 MTHS Ower Wing Door 1 36 MTHS Emergency Exit 1 36 MTHS Checks may be performed on either side and do not all have to be performed on the same aircraft.

Threshold Interval

I

36 MO

References

Ctrl

Eff

N

AMM 256200-710-801

ALL


Skills :

0.00 MHrs

1 AF N

256500-01-1VNA

200

MISCELLANEOUS EMERGENCY EQUIPMENT

DIS

Check : PCI

N

AMM 25-65-00PB001

ALL

FUC

I

N

AMM 256532-720-801

ALL

Replace EMERGENCY FLASHLIGHT BATTERIES at manufacturer's recommendation. NOTE: FOR SUPPLIER DME CORP .SHELF LIFE 4YE 200

256532-01-1

EMERGENCY LOCATOR TRANSMITTER-PORTABLE REMOVE EMERGENCY LOCATOR TRANSMITTER FOR FUNCTIONAL CHECK NOTE: IF PORTABLE ELT INSTALLED NOTE: TASK COMPONENT RELATED P/N: 1151324-1 P/N: 607690-5; 01N65920; S1823502-05 NOTE : REFER TO CROSS REFERENCE IN SECTION 3 FOR THRESHOLD AND INTERVAL.

5 YE

Check : PCI

Skills :

0.10 MHrs

1 CA Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 25 [2 / 4] ATA

: 25


25


Task Number

Zone

256535-02-1

200

Task Title

EMERGENCY LOCATOR TRANSMITTER

Task code

DIS

Threshold Interval

I

4 YE

References

Ctrl

Eff

N

AMM 256500-720-803

ALL

N

AMM 256500-720-803

ALL

N

AMM 256500-720-803

ALL

Check : PCI

REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION. EVERY 4 YEARS: REPLACE BOTH BATTERY PACKS NOTE: P/N: ELT96A2560000000 NOTE:NATIONAL/VENDOR REQUIREMENT TASK Skills :

1.00 MHrs

2 RA 256535-02-1A

200

EMERGENCY LOCATOR TRANSMITTER

DIS

200

EMERGENCY LOCATOR TRANSMITTER REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION. EVERY 5 YEARS:PERFORM BATTERY INTEGRITY TEST/REPLACEMENT NOTE: P/N: 01N6590() NOTE:NATIONAL/VENDOR REQUIREMENT TASK

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

6 YE

Check : PCI

REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT ACTIVATION. NOTE: P/N: S1820502-XX NOTE:NATIONAL/VENDOR REQUIREMENT TASK 256535-02-1B

I

DIS

I

5 YE

Check : PCI

Page : TCI - 25 [3 / 4] ATA

: 25


25


Task Number

Zone

256551-01-1

200

Task Title

Task code

DIS

MEGAPHONE

Threshold Interval

I

1 YE

References

Ctrl

Eff

N

AMM 256551-920-801

ALL

N

AMM 256652/4 AMT 256652-920-801 MRB MRB9

ALL

Check : PCI

DISCARD MEGAPHONE BATTERIES NOTE : FEDERAL SIGNAL P/N : A12SA NOTE : NATIONAL/VENDOR REQUIREMENT Skills :

0.12 MHrs

1 CA 200

256652-01-1

REM

LIFE VESTS RESTORATION OF LIFE VESTS NOTE : AIR CRUISERS (CREW) (PAX)

P/N : P0723E-XXX P/N : P0723-XXX P/N : P0640-XXX NOTE : REFER TO TIME CONTROL ITEM LIST IN SECTION 3 FOR THRESHOLD AND INTERVAL. NOTE: NATIONAL/VENDOR REQUIREMENT

Check : PCI

Skills :

5.88 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 25 [4 / 4] ATA

: 25


26

FIRE PROTECTION

Task Number

Zone

262100-10-1

450 460

Task Title

Task code

FUC


Threshold Interval

I

10 YE

References

Ctrl

Eff

N

AMM 262141-200-805

ALL

N

AMM 262100-040-808

ALL

N

AMM 262141-920-803

ALL

See note

REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING NOTE : PACIFIC SCIENTIFIC CO P/N : 34600028-1 NOTE: NATIONAL/VENDOR REQUIREMENT TASK

Check : PCI

Access panels :

453CL

453CR

Total access time :

463CL 463CR 0.00 Hrs

Skills :

2.00 MHrs

1 AV 262100-10-1A

262100-15-1

450 460


450 460


FUC

I

See note

REMOVE BOTTLE FOR WEIGHT CHECK NOTE : PACIFIC SCIENTIFIC CO P/N : 34600028-1 NOTE: NATIONAL/VENDOR REQUIREMENT TASK DIS

DISCARD CARTRIDGE NOTE : PACIFIC SCIENTIFIC CO P/N : 34600028-1 CARTRIDGE P/N:30903899 NOTE: NATIONAL/VENDOR REQUIREMENT TASK

5 YE

I

10 YE

Check : PCI

Access panels :

453CL

453CR

Total access time :

463CL 463CR 0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 26 [1 / 6] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262241-01-1

310

Task Title

Task code

FUC


Threshold Interval

I

10 YE

References

Ctrl

Eff

N

AMM 262241-280-802

ALL

N

AMM 262241-280-801

ALL

N

AMM 262241-280-803 CMP 26-2-0000-003

ALL

See note

REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING NOTE: NATIONAL/VENDOR REQUIREMENT TASK NOTE: P/N 33600005-3 472412-1

Check : PCI

Access panels :

313AL Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AV 262241-01-1A

310

FUC


310

Check : PCI

FUC

APU FIRE EXTINGUISHING FUNCTIONAL TEST OF APU FIRE EXTINGUISHER PRESSURE SWITCH SETTING NOTE : CMP TASK

5 YE See note

REMOVE BOTTLE FOR WEIGHT CHECK NOTE: NATIONAL/VENDOR REQUIREMENT TASK NOTE: P/N 33600005-3 472412-1 262241-03-1

I

I

72 MO

Check : PCI

Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AV Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 26 [2 / 6] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262242-01-1

310

Task Title

Task code

DIS


Threshold Interval

I

10 YE

References

Ctrl

Eff

N

AMM 262242-920-801

ALL

N

AMM 262300-720-803 CMR 262300-00001-1-C

ALL

Check : PCI

DISCARD CARTRIDGE CARTRIDGE P/N: 30903898; 446203 Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AV 130

262300-05-1

LOWER DECK CARGO COMPARTMENT FIRE EXTING FUNCTIONAL CHECK OF PRESSURE REDUCER (P/N: D41428; P/N E61751-00-0001) NOTE: ETOPS SIGNIFICATION SYSTEMS NOTE: P/N D41428 LIFE LIMIT IS 20 YEARS.

FUC

I

14 000 FH

Check : PCI

Access panels :

132SW

821

Total access time :

0.02 Hrs

Skills :

0.10 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 26 [3 / 6] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262341-01-1

132

Task Title


Task code

FUC

Threshold Interval

I

10 000 FH

References

Ctrl

Eff

N

AMM 262341-280-801

ALL

N

AMM 262341-280-802

ALL

Check : PCI

REMOVE BOTTLE FOR WEIGHT CHECK NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

132SW

821

Total access time :

0.02 Hrs

Skills :

1.00 MHrs

1 AV 132

262341-02-1

LOWER DECK CARGO COMPT FIREX REMOVE BOTTLE FOR HYDROSTATIC TEST NOTE: ETOPS SIGNIFICATION SYSTEMS NOTE: P/N: 472931-X 472625-X

FUC

I

10 YE See note

Check : PCI

Access panels :

132SW

821

Total access time :

0.02 Hrs

Skills :

1.50 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 26 [4 / 6] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262343-01-1

130

Task Title

LOWER DECK CARGO COMPARTMENT FIRE EXTING

Task code

DIS

Threshold Interval

I

10 YE

References

Ctrl

Eff

N

AMM 262342-920-801

ALL

N

AMM 262400-280-801

ALL

Check : PCI

DISCARD CARTRIDGE UNIT NOTE : P/N : 446203, M446203, 30903899 NOTE: NATIONAL/VENDOR REQUIREMENT TASK NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

132SW

821

Total access time :

0.02 Hrs

Skills :

0.50 MHrs

1 AV 120 200

262400-01-1


FUC

Check : PCI

REMOVE BOTTLES FOR WEIGHT CHECK NOTE: P/N BA51015 SERIES EVERY 12 MONTHS: PERFORM A CHECK IAW CMM 26-20-30 INCLUDING WEIGHT CHECK. COTAINER LIFE: 10 YEARS NOTE: P/N 74-20 74-00 76-00 EVERY 2 YEARS: PERFORM AN INSPECTION IAW CMM 26-24-05 P/N BA21741-XXX-X COTAINER LIFE: 10 YEARS EVERY YEAR: PREFORM INSPECTION AND A WEIGHT CHECK IF FIRE EXTINGUISHER WITHOUT PRESSURE GAUGE IS INSTALLED Skills :

0.13 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 26 [5 / 6] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262400-02-1

200

Task Title


Task code

FUC

Threshold Interval

I

10 YE

References

Ctrl

Eff

N

AMM 262400-280-802

ALL

N

AMM 262500-280-804

ALL

See note

REMOVE BOTTLES FOR HYDROSTATIC TEST NOTE: P/N 74-20; 74-00 BA21741XX-X; BA51015 SERIES EVERY 10 YEARS:PERFORM A HYDROSTATIC TEST (VENDOR RECOMMENDATION IS TO REPLACE THE EXTINGUISHER) NOTE:NATIONAL/VENDOR REQUIREMENT TASK

Check : PCI

Skills :

0.13 MHrs

1 AV 200

262541-01-1


Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

FUC

I

72 MO

Check : PCI

Page : TCI - 26 [6 / 6] ATA

: 26


27

FLIGHT CONTROLS - GENERAL

Task Number

Zone

272149-01-1

325

Task Title

Task code

OP

RUDDER MECHANICAL CONTROL REMOVE SERVO CONTROL ACTUATING SPRING ROD FOR WORKSHOP CHECK NOTE: RII TASK

Threshold Interval

I

20 000 FH

I

42 MO

References

Ctrl

N

AMM 272149-200-801

Eff 275 294 299

Check : PCI

366

Skills :

1.00 MHrs

1 AF 325

272400-05-2

REM

RUDDER HYDRAULIC ACTUATION REMOVE RUDDER SERVO CONTROL FOR WORKSHOP CHECK OF INTERNAL SEALS NOTE: RII TASK

I

33 000 FH

Check : PCI

N

AMM 272451-200-801 CMR 272400-00001-2-C

325DR

Total access time :

325EL

325GR

366

325JR

0.00 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294 299

Access panels :

325CR

275

Page : TCI - 27 [1 / 2] ATA

: 27


R

27


Task Number

Zone

275117-01-1

212

Task Title

Task code

REM

FLAPS REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE PREP. : MOVABLE FLAP TRACK FAIRING Z531; MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; MOVABLE FLAP TRACK FAIRING Z631; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634;

Threshold Interval

I

12 YE

References

Ctrl

N

AMM 275117-280-801

Check : PCI

Access panels :

114VU Total access time :

0.00 Hrs

Skills :

0.25 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 27 [2 / 2] ATA

: 27

Eff ALL


29

HYDRAULIC POWER

Task Number

Zone

291100-05-1

326

Task Title

GREEN MAIN HYDRAULIC POWER

Task code

FUC

Threshold Interval

I

6 YE

References

Ctrl

Eff

N

AMM 291146-750-801

ALL

N

AMM 291148-750-801

ALL

Check : PCI

REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK PREP. : VALVE NOTE: ETOPS PARALLEL SYSTEM Skills :

0.50 MHrs

1 AF 500 600

291100-06-1

GREEN MAIN HYDRAULIC POWER REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK PREP. : VALVE NOTE: ETOPS PARALLEL SYSTEM

FUC

I

6 YE

Check : PCI

Access panels :

575BB

675BB

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 29 [1 / 1] ATA

: 29


31

INDICATING & RECORDING SYSTEMS

Task Number

Zone

313300-01-1

312

Task Title

DIGITAL FLIGHT DATA RECORDING SYSTEM DISCARD ULB BATTERY NOTE : DUKANE P/N : DK100-DK120 HONEYWELL P/N : 980-4700-042 266-E0305-00 NOTE:NATIONAL/VENDOR REQUIREMENT TASK

Task code

DIS

Threshold Interval

I

6 YE

References

Ctrl

N

AMM 313355-920-801

Check : PCI

Access panels :

312AR Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 31 [1 / 1] ATA

: 31

Eff ALL


32

LANDING GEAR

Task Number

Zone

321100-01-1

731 741

Task Title

Task code

REM

MAIN LANDING GEAR RESTORATION OF MAIN GEAR REFER TO AD 2008-0152 NOTE: RII TASK

Threshold Interval

I

17 000 CY

I

10 YE

References

Ctrl

Eff

N

AMM 321111-920-801

ALL


Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

96.00 MHrs

4 AF R

731 741

321100-02-1

MAIN GEAR FUNCTIONAL CHECK OF MLG BOGIE BEAM PITCH TRIMMER CONTROL MANIFOLD HYDRAULIC FUSE (OFF AIRCRAFT).

REM OP

I

10 YE

N

AMM 321100-720-802

ALL

REM

I

17 000 CY

N

AMM 322111-920-801

ALL

I

10 YE

Skills :

2.66 MHrs

1 AF 711

322100-02-1

NOSE GEAR REMOVE NOSE GEAR FOR RESTORATION NOTE: - RESTORATION TO BE PERFORMED IN ACCORDANCE WITH AIRBUS APPROVED MESSIER-DOWTY SB D23581-32-051 NOTE: RII TASK


Skills :

8.00 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 32 [1 / 1] ATA

: 32


R

34

NAVIGATION

Task Number

Zone

344100-01-1

110

Task Title

WEATHER RADAR SYSTEM

Task code

CHK

Threshold Interval

I

30 MO

References

Ctrl

N

AMM 531511-760-802

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294 299

Check : PCI REMOVE RADOME FOR RADIO ELECTRICAL TEST NOTE: TASK APPLICABLE FOR A/C POST 44754 (34-3092; 34-3236) AND INSTALL KELVAR RADOME + A/C POST 44754 (34-3092;34-3236 ): MSN 294; 299; 943; 962; 1019; 1256; 1266; 946 + RADOME KELVAR P/N: A9232060600700

Issue No

Eff

943 946 962 1019 1256 1266

Page : TCI - 34 [1 / 1] ATA

: 34


35

OXYGEN

Task Number

Zone

351141-01-1

121

Task Title

Task code

FUC

CREW OXYGEN

Threshold Interval

I

5 YE

References

Ctrl

Eff

N

AMM 351141-750-801

ALL

N

AMM 351315-920-801

ALL

N

AMM 351241-720-801

ALL

See note

REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND FUNCTIONAL CHECK OF OXYGEN CYLINDER PRESSURE GAUGE. NOTE: TASK COMPONENT RELATED P/N: 897-SERIES EVERY 5 YEARS:PERFORM A HYDROSTATIC TEST MAX. SERVICE LIFE: 15 YEARS NOTE:NATIONAL/VENDOR REQUIREMENT TASK

Check : PCI

Access panels :

811 Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 122

351200-06-1

FUC

CREW OXYGEN

I

72 MO

Check : PCI

REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL CHECK (IN WORKSHOP). Skills :

0.30 MHrs

1 AF 210

351315-01-1

CREW OXYGEN MASK REGULATOR REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK PREP. : REGULATORS NOTE:NATIONAL/VENDOR REQUIREMENT TASK

FUC

I

72 MO

Check : PCI

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 35 [1 / 3] ATA

: 35


35

OXYGEN

Task Number

Zone

352142-01-1

200

Task Title

PASSENGER OXYGEN (CHEMICAL)

Task code

DIS

Threshold Interval

I

15 YE

References

Ctrl

Eff

N

AMM 352142-920-801

ALL

N

AMM 353152-920-801

ALL

N

AMM 353242-780-804

ALL

Check : PCI

DISCARD CHEMICAL OXYGEN GENERATORS NOTE : DRAEGERWERK P/N : E63420-00 NOTE:NATIONAL/VENDOR REQUIREMENT TASK Skills :

17.40 MHrs

1 AF 210

353150-01-1

FLIGHT CREW PORTABLE BREATHING EQUIPT

DIS

I

10 YE

Check : PCI

DISCARD PROTECTIVE BREATHING EQUIPMENT NOTE: P/N : 119003-11 P/N : E28180-XX P/N : 15-40F11 NOTE: NATIONAL/VENDOR REQUIREMENT Skills :

0.10 MHrs

1 AF 200

353200-07-1

PORTABLE OXYGEN REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN REGULATOR (IN WORKSHOP). NOTE: P/N 3552 SERIES EVERY 5 YEARS:PERFORM A HYDROSTATIC TEST, AND OVERHAUL SERVICE LIFE: 15 YEARS

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

FUC

I

5 YE

Check : PCI

Page : TCI - 35 [2 / 3] ATA

: 35


35

OXYGEN

Task Number

Zone

353250-01-1

200

Task Title

CABIN ATTENDANTS PORTABLE BREATHING EQ DISCARD PROTECTIVE BREATHING EQUIPMENT NOTE: P/N : 119003-11 P/N : E28180-XX P/N : 15-40F11 NOTE: NATIONAL/VENDOR REQUIREMENT

Task code

DIS

Threshold Interval

I

10 YE

References

Ctrl

N

AMM 353252-920-801

Check : PCI

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : TCI - 35 [3 / 3] ATA

: 35

Eff ALL


47

INERT GAS GENERATION SYSTEM

Task Number

Zone

470000-02-1

191

Task Title

INERT GAS SYSTEM DISCARD AIR SEPARATOR MODULE

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Task code

DIS

Threshold Interval

I

27 000 FH

References

Ctrl

N

AMM 471043-920-801

Eff 1256 1266

Check : PCI

Page : TCI - 47 [1 / 1] ATA

: 47


71

POWER PLANT - GENERAL

Task Number

Zone

712101-03-1

413 423

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FORWARD ENGINE MOUNT. TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE; FWD ENGINE MOUNT DISASSEMBLED; note:CPCP NOTE: RII TASK

Threshold Interval

T

12 YE

I

12 YE

T

52 000 FH

T

8 000 FC

I

52 000 FH

References

Ctrl

Eff

N

AMM 712111-220-801

ALL

N

AMM 712111-280-801

ALL

N

AMM 712211-220-802

ALL

Skills :

0.00 MHrs

1 EN 413 423

712106-01-1

413 423

712204-02-1

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT. NOTE: TASK SHOULD BE DONE WHEN ENG CHANGE PREP. : ENGINE FORWARD ENGINE MOUNT DISASSEMBLED NOTE: RII TASK

MAIN STRUCTURE DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL- SAFE LINK NOTE: TASK SHOULD BE DONE WHEN ENG CHANGE NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH PREP. : ENGINE MOUNT; ENGINE; NOTE: RII TASK

Amendment No Date

: 01 : 06/09/2014

I

8 000 CY See note Check : NT

DI

T

52 000 FH

T

8 000 FC

I

52 000 FH

I

8 000 CY See note

Check : NT

Page : TCI - 71 [1 / 1] ATA

: 71


72

ENGINE

Task Number

Zone

723100-P3-1

410 420


410 420


410 420

HIGH PRESSURE COMPRESSOR

410 420


723200-P1-1

723500-P1-1

725200-P2-1

Issue No

:

Date

:

10 01/12/2013

Task Title

Task code

DIS

Threshold Interval

Ctrl

See note

N

AMM 723100-920-801

ALL

N

AMM 723200-920-801

ALL

N

AMM 723500-920-801

ALL

N

AMM 725200-920-801

ALL

References

Check : PCI

DISCARD FAN HUB AND LPC DRUM ROTOR INTERVAL NOTE: IAW ENGINE SHOP MANUAL TIME LIMITS AND A330 AAIP VOL.1 CHAPTER 10.4 NOTE: RII TASK DIS


DISCARD LPC/LPT COUPLING INTERVAL NOTE: IAW ENGINE SHOP MANUAL TIME LIMITS AND A330 AAIP VOL.1 CHAPTER 10.4 NOTE: RII TASK DIS


DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR INTERVAL NOTE: IAW ENGINE SHOP MANUAL TIME LIMITS AND A330 AAIP VOL.1 CHAPTER 10.4 NOTE: RII TASK DIS

Check : PCI

DISCARD LIFE LIMITED PARTS OF HP TURBINE INTERVAL NOTE: IAW ENGINE SHOP MANUAL TIME LIMITS AND A330 AAIP VOL.1 CHAPTER 10.4 NOTE: RII TASK

Amendment No Date

: 01 : 06/09/2014

Eff

Page : LLP - 72 [1 / 2] ATA

: 72


72

ENGINE

Task Number

Zone

725300-P1-1

410 420

Task Title

LOW PRESSURE TURBINE GROUPP

Task code

Threshold Interval

DIS

Check : PCI

References

Ctrl

N

AMM 725300-920-801

DISCARD LIFE LIMITED PARTS OF LP TURBINE INTERVAL NOTE: IAW ENGINE SHOP MANUAL TIME LIMITS AND A330 AAIP VOL.1 CHAPTER 10.4 NOTE: RII TASK Skills :

1 ENG

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

0.00 MHrs

Page : LLP - 72 [2 / 2] ATA

: 72

Eff ALL

SECTION 4

SCHEDULE AIRCRAFT MAINTENANCE


SECTION 4 GENERAL INTRODUCTION I.

CONTENTS This Section contents 8 sub-sections: SYSTEMS_APU_AND_POWERPLANT 

Systems and Components (SYS)



Certification Maintenance Requirements (CMR)



Ageing Systems Maintenance (ASM)



Fuel Airworthiness Limitations (FAL)



Fuel saving (ECO)

STRUCTURE 

Structure Program (STR)



Airworthiness Limitation Items (ALI)

ZONAL  II.

Zonal Program (ZNL)

REMARK This Aircraft Maintenance Schedule is printed out from AMASIS. INTRODUCTION

III.

SYSTEMS_APU_AND_POWERPLANT: (sub-section SYS; CMR; ASM; FAL; ECO) provides the scheduled maintenance tasks and frequencies for all Systems, Power Plants and Auxiliary Power Unit. With respect to the evaluation procedures and the resulting tasks the following is noted: 1. Operational checks were not considered as forming part of Normal Operating Crew Duties when determining the evident or hidden aspects of functional failures (ref. Policy and Procedures Handbook (PPH) para 4.4.4.1). As a result some tasks given in this section may be considered as flight crew tasks in accordance with Note 5.


2. This section identifies some tasks with intervals less than A-check. These have been developed using the MSG-3 process and should be included in routine checks. With the exception of any task with CMR status, those tasks which are typical for all aircraft types may be scheduled by the operator in accordance with Regulatory Authority accepted standard practices, the quoted interval being given for the guidance of operators who do not have appropriate standards. 3. Cat II/Cat III landing capabilities and RVSM capability are inherent functions of the basic design standard of the aircraft. Scheduled tasks necessary for these operations have been considered in the development of this section. Operators should comply with National Requirements as applicable. 4. Lubrication requirements specified in this MPD do not represent the total lubrication provisions for the aeroplane. Accordingly, operators should refer to the manufacturer’s appropriate maintenance publications for additional lubrication information. 5. During the review of an aircraft system for the purpose of modifying or verifying the maintenance requirements, the reviewer must be aware that those functions associated with the ignition prevention features of all systems are identified and analyzed in MSI 2818-00 Ignition Prevention. Any review of an existing MPD task must therefore consider that it may be necessary to review MPD 281800 in addition to the specific system MSI identified. 6. Operators should take the opportunity of APU/Power Plant removal and disassembly to perform "off-wing" inspections and parts/assemblies restoration as per engine shop manuals. No scheduled basis for these tasks is defined in this MPD. 7. No threshold or opportunity inspection requirements are given for APU/Power Plant. Manufacturer may recommend such inspections in the event that late development or early in-service experience would indicate the desirability to examine specific components of individual engines or APU. If this is necessary, then direct negotiations between applicable operators and the APU/engine manufacturer will be arranged. Results of these inspections are to be made available by the manufacturer to other customer airlines as well as the Regulatory Authorities. 8. Limitations of life limited parts of the APU are controlled and published in GTCP 331-350 (c) Engine Component Maintenance Manual. 9. APU task intervals quoted in terms of APU HRS may be converted to another usage parameter in accordance with an appropriate conversion factor based on an operator's specific APU utilization. 10. No recommendation is made for scheduled fuel analysis. Operators who suspect the quality of their fuel supplies or who operate in an environment known to promote microbiological growth are recommended to introduce fuel sampling and consider the use of additives to minimize the potential for such growth. 11. limitations of life limited parts are controlled by the manufacturers and published in the following documents: - ALS part 1 Safe Life Airworthiness Limitation Items - ALS Part 4 Ageing Systems Maintenance - PW 4000 Engine Shop Manual Chapter 5 12. Tasks approved from Fuel Tank Safety (FTS) Requirements using the criteria established in Special Federal Aviation Regulation (SFAR88)/ EASA policy statement on the process for developing instructions for maintenance and inspection of fuel tank system ignition source prevention; are identified with (SFAR88) in parenthesis following the task


description in the MPD. This policy has been applied to Systems & Power Plant tasks listed under ATA 281800 in Section 2. Operators requesting revisions to the baseline FTS requirements may revise these tasks and intervals through their normal operator approval process. 13. Electrical Wiring Interconnection System (EWIS) tasks derived from the Enhanced Zonal Analysis Procedure (EZAP) in ATA 20 of Section Systems, Power Plants and Auxiliary Power Unit and standard zonal tasks with EWIS content are identified by (EWIS) in parenthesis following the task description in the MPD. Operators requesting revisions to the EWIS requirements may revise these tasks and intervals through their normal operator approval process. Tasks indicated with “(EWIS)” after the task description must not be deleted from the operator's maintenance program.. 14. Tasks arising from the Enhanced Zonal AnalysisProcedure (EZAP), (comprised of GVI tasks not fully covered by Zonal tasks and DI/RS tasks) are included within ATA chapter 20 of the System and Powerplant section of the MRBR and have no Failure Effect Category (FEC) quoted. The tasks are identified with “(EWIS)” following the task description (see “Electrical Wiring Interconnection System (EWIS)” for further details). These tasks remain under the responsibility of the Zonal Maintenance Working Group. NOTE (i): The term “EWIS” in the task description of ATA 20 tasks includes all electrical wiring and interconnection systems installations (e.g. cables, conduits, clamps, etc…) NOTE (ii): ATA 20 tasks must not be deleted from the operators maintenance program NOTE (iii): For advice on cleaning contaminated wiring, refer to the Airbus Electrical Standard Practices Manual (ESPM) chapter 20-55-20 “CLEANING OF WIRES (Airbus)”. Note: Operationally check the slide/raft in accordance with the following schedule: QUANTITY (PER DOOR/EXIT (RH OR LHSIDE) FLEET) FWD Passenger/Crew Door MID Passenger/Crew Door AFT Passenger/Crew Door Emergency Exit

1 1 1 1

CHECK INTERVAL 36 MTHS 36 MTHS 36 MTHS 36 MTHS

Checks may be performed on either side and do not all have to be performed on the same aircraft. As an ongoing continuous maintenance program the operator should continue the operational check sequence until this schedule has been revised by the MRB. Inadvertent deployments may not be used to satisfy the above requirements. STRUCTURE (STR; ALI): The purpose of this section is to maintain the continuous airworthiness of the aircraft structure and to control corrosion to Level 1 or better (refer to “CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)” for definition of Level 1 corrosion). INSPECTION PHILOSOPHY This section has been developed by considering the following sources of damage: 1. Metallics


FD) Fatigue Damage For FD, the damage initiation and subsequent damage growth is primarily dependant on the ground air ground loading variation, which occurs once per flight. Therefore, flight cycles (FC) are used as the unit for thresholds and repeat intervals. Some fatigue related SSI’s are also sensitive to flight duration. For these SSI’s, a FH limit is stated in addition to the FC limit. The inspection is to be performed at whichever limit is reached first. The structure inspection tasks selected for fatigue are derived from damage tolerance evaluation according to the criteria defined by FAR/JAR 25.571, Amendment 45. The FC and FH data is based on a combination of calculation, full-scale fatigue test tear down results, and in-service experience (where available). (ED) Environmental Deterioration Since deterioration caused by the environment (e.g. corrosion, stress corrosion) is mainly time dependant, the maintenance requirements are based on calendar time (Years). (AD) Accidental Damage For deterioration caused by accidental damage, it is considered that major damage such as that caused by bird impact, or ground handling equipment, will be detected by routine inspections. AD consists of minor damage which could result in fatigue and/or corrosion damage, and which could propagate undetected. In the analysis, the fatigue and environmental effects of the accidental damage are considered. A dedicated AD task is not selected; the AD requirement is consolidated into either the ED or the FD task, or both, according to the AD consequences. AD is therefore subject to maintenance requirements expressed in FC (and FH) or calendar time or both. 2. Non-metallics (AG) Ageing Deterioration Deterioration caused by ageing considers loading conditions and environmental conditions. Inspection intervals and thresholds are based on calendar time (AD) Accidental Damage Deterioration caused by accidental damage is subject to inspection intervals based on calendar time The frequency of inspection is dependant on static strength reduction caused by the selected damage, combined with the likelihood of the selected damage occurring more than once during the selected interval. As this kind of deterioration is random in nature, inspections shall be applied to all aircraft at each repeat interval without threshold. INSPECTION LEVELS According to the analysis procedure, for each Structural Significant Item (SSI), various inspection levels have been considered with the aim of selecting the lowest inspection level compatible with the type of damage and the expected damage growth. Therefore, one or more of the following inspection levels have been selected for each SSI: General Visual Inspection (GVI)


Detailed Inspection (DI) Special Detailed Inspection (SDI) ZONAL SECTION COMPATIBILITY When General Visual Inspection (GVI) level has been selected for a particular structure inspection task in the Structure section of the MRBR, the inspection requirement is considered adequately covered by the equivalent Zonal (ZIP) tasks which are referenced in the ZIP reference column. The MRB Report Structure section GVI tasks which have a ZIP reference are therefore not listed as individual tasks in the MPD as well as in this AMS. GVI maintenance tasks which are not compatible with the Zonal section are stated in the MPD as individual tasks. GVI SSI's which also require the addition of Temporary Protection Systems (TPS) will still be indicated as individual tasks in the Structure section. The TPS application remains a Structure requirement but the inspection part of the maintenance task may be covered by the Zonal Inspection CORROSION PREVENTION AND CONTROL PROGRAM (CPCP) A. INTRODUCTION The Structure section includes requirements to control corrosion to Level 1 or better on all structural details, elements or assemblies whose failure could affect the structural integrity necessary for the safety of the aircraft All Corrosion Prevention and Control Program (CPCP) requirements are indicated by the note 'CPCP' in the “task description”. B. CORROSION LEVEL DEFINITIONS The severity of the corrosion damage is categorized into three 'Levels' as follows: Level 1 Corrosion Corrosion damage that does not require structural reinforcement or replacement. or Corrosion occurring between successive inspections exceeds allowable limit but is local and can be attributed to an event not typical of operator usage of other aircraft in the same fleet (e.g. Mercury spill). Level 2 Corrosion Corrosion occurring between successive inspections that requires a single rework/blend out which exceeds allowable limits as defined by the manufacturer (SRM, SB, etc.), requiring a repair/reinforcement or complete or partial replacement of applicable structure Level 3 Corrosion Corrosion found during first or subsequent inspection(s), which is determined (normally by the operator) to be an urgent airworthiness concern requiring expeditious action. C. CPCP RULES The effectiveness of the CPCP is determined by following the General Rules applicable to the Structure section and by following the rules listed below:


Level 1 Corrosion Findings Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat inspections on particular aircraft operated in similar conditions, then the existing program is considered effective for the concerned area, and no change to the program is necessary. Level 2 Corrosion Findings Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections, then the existing program is not effective for the concerned area of the particular fleet. In order to control corrosion to Level 1 or better, consideration should be given to one or more of the following corrective actions: -

Decreasing the inspection threshold/interval Considering a higher inspection level Re considering the Program Concept Application/More frequent application of Temporary Protection System Embodiment of preventive modifications, where applicable Installation of parts with improved protection standard, where applicable

In this way, the program is self regulating and will adjust itself to the optimum program Level 3 Corrosion Findings Should inspections reveal that corrosion is Level 3 in a given area, then the existing program is not effective for the concerned area In addition to the considerations given for Level 2 corrosion, an action plan calling for a one time inspection of the concerned area should be expeditiously agreed with the local Aviation Authority and carried out on all aircraft of a similar age or older. Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all details of findings are to be promptly reported for detailed evaluation and the assistance required clearly expressed. GENERAL RULES APPLICABLE TO THE STRUCTURE SECTION 1. The Maintenance tasks are to be carried out 'at or before' the limits stated for Sample Threshold/Interval and 100% Threshold/Interval. Where a task has more than one limit, e.g. one in FC and another in calendar time, the limit expiring first shall apply. 2. The Threshold is the time at which the maintenance requirement is first due. - For FC or FH tasks without MOD applicability, the sample thresholds and 100% thresholds are counted from first flight. - For FC or FH tasks with MOD applicability, the sample thresholds and 100% thresholds are counted from point of MOD embodiment, unless otherwise stated. In a very small number of retrofit mod cases, the fatigue threshold in FC and FH is also applicable from 1st flight. This is indicated by a note in the tasks concerned - For tasks in Years, the sample thresholds and 100% thresholds are counted from the date of initial delivery from the manufacturer, unless otherwise stated (NOTE 8 in MPD).


3. For repeat maintenance tasks, the interval starts at the time of the last maintenance tasks performed 4. Thresholds and intervals quoted in calendar time in this section include aircraft time in and out of service. In other words, operators will not, in general, be allowed to take credit for time out of service or storage periods to extend corrosion inspection intervals. 5. It is assumed that the structure to be inspected is in a state of cleanliness which allows a satisfactory inspection to be carried out at the required inspection level. Where existing Temporary Protection System (TPS) permits unobscured assessment of the condition of the structure, TPS may remain in place for the inspection. 6. If damage is found or suspected (such as bulging skin) then the full extent of any damage must be clearly identified using appropriate inspection techniques and/or disassembly when necessary. This may require additional access to that stated for the maintenance task All damage is to be evaluated and repaired in accordance with documentation acceptable to the relevant Airworthiness Authority. 7. If inspections indicate evidence of deterioration, appropriate further actions must be taken to prevent similar deterioration occurring in the operators fleet. For corrosion findings refer to Corrosion Prevention and Control Program. 8. The following applies to Temporary Protection System (TPS) application: Prior to any application of TPS, perform an inspection of the area at the inspection level for the task quoted in calendar time. Prior to re fitting/re connecting/re installing parts removed to gain access to the inspection area, TPS is to be applied to each SSI, as quoted in the TPS column of this Structure section, at least as frequently as the calendar time thresholds and intervals of the respective SSI. For SSI's where the FC or FH limit is reached before the calendar time limit, consideration should be given to application of TPS at the FC or FH limit The Type of TPS to be applied is provided in the TPS column of the Structure section. When TPS is only applied to a selected area, details are provided as a note in the Description column. Sampling Program tasks do not have TPS selected in the Structure section. If an operator chooses to apply TPS to a particular SSI for aircraft inspected in accordance with the Sampling Program, these aircraft are no longer representative of the non-sampled aircraft. In this case, TPS must be applied to all aircraft in this SSI area, including the aircraft not selected for sampling. This task then effectively becomes 100% for those specific aircraft. CAUTION: Do not apply TPS on oxygen systems, control cables, pulleys, Teflon bearings and lubricated surfaces. Drain valves and all open orifices are to be protected from ingress prior to temporary protection being applied. 9. The access column may contain one of the following instructions concerning insulation blankets: Insulation = Insulation to be removed from the inspection area. Note 1 = Insulation to be displaced as required to complete the required maintenance task 10. Ensure wet insulation blankets are dried prior to reinstallation, or replaced with new. 11. Ensure that all drain holes and drainage paths are clear from obstruction


12. The condition of the paint system should be verified during the inspections. Re protection should be applied where necessary. 13. The requirements stated in years were determined for an aircraft operated in a moderate humidity environment and not subjected to corrosive products Any operators who routinely operate in humid or marine environments and/or carry corrosive cargo such as seafood, may find that the calendar time maintenance tasks stated in this MPD are not sufficient to control corrosion to Level 1 or better. Operators in this category should take appropriate further actions. 14. Operators shall report inspection results related to SSI's to the manufacturer in accordance with the Maintenance Task Reporting System. Refer to the General Introduction paragraph 15. 15. “Touch and Go" Cycles can be neglected if they are less than 5% of the total number of Flight Cycles up to threshold inspection or between two consecutive inspections. Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold inspection or between two consecutive inspections. ZONAL INTRODUCTION GENERAL This section provides the General Visual Inspection (GVI) requirements for each aircraft zone to inspect system, power plant installations and structure for security and general condition. Inspections are to be accomplished at or before the stated intervals. The inspections are specified by quoting the relevant zone number, zone description, access requirements and intervals. The extent of the inspection is defined by the preparation and access requirements. The zone is to be inspected as visible with the relevant access open. There are zones which will require more than one inspection at different intervals, because the depth at which the zone is to be examined may necessitate differing levels of accessibility. The inspection tasks in this Zonal section (ZIP) do not provide a complete summary of all structure and systems items to be inspected in the affected zone. It is therefore considered that the person performing the inspection has an adequate knowledge of the aircraft construction and of its system installation. Any evolution of Zonal Inspection tasks involving an escalation to the inspection task interval should consider that credit has been taken for many of these tasks providing the most appropriate opportunity to detect degradation of wiring installations, electrical bonding and structural corrosion. As a result, operators should consider the need to identify dedicated tasks if findings suggest that interval escalation might lead to an unacceptable level of deterioration of these particular features prior to the repeat inspection. This action would allow any ZIP task interval escalation to proceed while at the same time ensuring that operators do not overlook the potential impact on EWIS, L/HIRF and structural corrosion issues. In view of the fact that all zonal tasks contribute to the identification of degradation that, if ignored, could ultimately lead to a reduction in certification margins, zonal tasks must not be deleted from an operator’s maintenance program


Operators shall consider that all Zonal tasks identified with “(EWIS)” after the task description are required to support compliance with Electrical Wiring Interconnection System (EWIS) requirements GVI tasks arising from EZAP Analysis considered notfully covered by the Zonal section and any nonGVI task arising from the EZAP analysis are included within ATA 20 of the Systems and Powerplant Section and are identified by “(EWIS)” after the task description. These dedicated tasks remain under the responsibility of the Zonal MWG. All ATA 20 tasks are uniquely identified in the Systems and Powerplant Section with (EWIS) after the task description to prevent the inadvertent deletion or escalation of dedicated EZAP derived tasks without proper consideration of associated risk basis for task and interval. GUIDANCE FOR ACCOMPLISHMENT OF A ZONAL GVI A Zonal GVI requires a visual examination to detect obvious unsatisfactory conditions and discrepancies. It shall be performed from within touching distance unless otherwise noted, that being the distance from the examiner’s eye to the area/item being inspected. The tasks inspect: -

-

Structure by looking for signs of accidental damage, corrosion, cracks and for general condition of fasteners. System installations for proper attachment ,security and general condition (components, wiring, ducting, tubing, pulleys, bearings, electrical bonding, leaks, chafing marks etc...). The general condition of any fairings, panels, or other items which are removed/opened to gain access to a particular zone. Condition of L/HIRF (Lightning & High Intensity Radiated Field) protection For accumulation of any kind of contamination (including potential combustible material) for EZAP (Enhanced Zonal Analysis Procedure) concerns.

The items in the zone are to be visually inspected from within touching distance where physically possible unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. The inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Access to zones should be easily accomplished and should not require the use of special tools. Stands, ladders or platforms may be required to gain proximity to the area being checked. There is no requirement for equipment removal or displacement unless this is specifically called for in the access instructions. However, should unsatisfactory conditions be suspected, additional items may need to be removed or displaced in order to permit proper assessment. Paint and/or sealant removal is not necessary and should be avoided unless condition is suspect. It is expected that the area to be inspected is clean enough to minimise the possibility that accumulated dirt or grease might hide unsatisfactory conditions. Any cleaning that is considered necessary should be performed before the Zonal inspection. In general, the person performing the inspection is expected to identify degradation due to wear, vibration, moisture, contamination, excessive heat, aging, etc. and make an assessment as to what actions are appropriate to address the noted discrepancy. In making this assessment, the


person performing the inspection shall take into account potential influence on adjacent system installations, particularly if these include wiring.


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Page: 4


08

LEVELING / WEIGHING

Task Number

Zone

081000-01-1-D

100

Task Title

Task code

FUC

AIRCRAFT WEIGHING

Threshold Interval

I

4 YE

References

Ctrl

N

AMM 081000-200-801

CARRY OUT AIRCRAFT WEIGHING Skills :

12.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 08 [1 / 1] ATA

: 08

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200001-01-1

522 622

Task Title

LIGHTNING/HIRF PROTECTION-WING

Task code

Threshold Interval

CHK

Check : 4C

N

AMM 249200-210-801

ALL

CHK

I

N

AMM 249200-210-816

ALL

References

Ctrl

Eff

SECURITY CHECK OF THE FOLLOWING HARNESSES END FITTINGS, FROM RIB 9 TO RIB 10A : - 7021VP, 7001VC-A, 7021VC-A, 7025VC-A, 10HA1, LH SIDE - 7024VP, 7022VC-A, 7026VC-A, 10HA2, RH SIDE Access panels :

454BL

464BL

Total access time :

522AB 522BB 1.60 Hrs

622AB

622BB

Skills :

0.20 MHrs

1 EL 633

200001-03-1


36 MO

SECURITY CHECK OF THE FOUR B3 TYPE CONNECTORS LOCATED ON THE RAT. Access panels :


0.00 Hrs

Skills :

0.25 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [1 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200001-04-1

523 623

Task Title


Task code

Threshold Interval

GVI

Check : 1C

References

Ctrl

N

AMM 249200-210-804

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE FOLLOWING HARNESS END FITTINGS FROM WING TIP TO RIB 39 : - 7621VB, 7623VB, 7625VB, 7627VB, LH SIDE 7622VB, 7622VB, 7626VB, 7628VB, RH SIDE Access panels :

523NB

535AB

Total access time :

575DB 623NB 3.80 Hrs

635AB

675DB

Skills :

0.80 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [2 / 34] ATA

: 20

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200001-05-1

533 574 633 674

Task code

Task Title


Threshold Interval

References

Ctrl

Eff

GVI

I

36 MO

N

AMM 249200-210-805

ALL

GVI

I

36 MO

N

AMM 249200-210-808

ALL

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE FOLLOWING HARNESSES END FITTINGS, FROM RIB 19 TO RIB 14: - 7633VB LH SIDE - 7634VB RH SIDE PREP. : FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z633; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z633; Access panels :

533AB 633CB

533CB 674CB

Total access time :

574CB 674DB

574DB 674EB

574EB 674FB

574FB

633AB

0.00 Hrs

Skills :

0.20 MHrs

1 EL R

571 671

200001-08-1

LIGHTNING/HIRF PROTECTION-WING GENERAL VISUAL INSPECTION OF THE FOLLOWING BRAIDED CONDUIT END FITTINGS, FROM RIB 6 TO FUSELAGE : - 112QA1-A, 121QA1-A, 122QA1-A, LH SIDE - 112QA2-A, 121QA2-A, 122QA2-A, RH SIDE PREP. : FUEL PUMP FAIRINGS Z500; FUEL PUMP FAIRINGS Z600; Skills :

0.50 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [3 / 34] ATA

: 20


R

20

STANDARD PRACTICE

Task Number

Zone

200001-09-1

531 631

Task code

Task Title


Threshold Interval

GVI

I

GVI

Check : 4C

36 MO

References

Ctrl

Eff

N

AMM 249200-210-821

ALL

N

AMM 249200-210-819

275

DETAILED INSPECTION OF ELEMENTS FITTED ON THE FOLLOWING HARNESSES END FITTINGS, FROM RIB 6 TO FUSELAGE : - 7633VB, 7645VB, 7651VB, LH SIDE - 7634VB, 7646VB, 7652VB, RH SIDE PREP. : FLAPS EXTENDED Access panels :

531CB 673DB

573BB

Total access time :

573CB

573DB

631CB

673BB

673CB

0.00 Hrs

Skills :

0.50 MHrs

1 EL 147 148 191 192

200001-14-1


294

FUNCTIONAL CHECK OF THE FOLLOWING WING PRESSURE SEA BONDINGS: 3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503VP, 3505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3744VP, 3721VP, 3735VP, 3737VP, 3743VP PREP. : WING FILLET FAIRINGS Z191; WING FILLET FAIRINGS Z192;

299 366

Access panels :

521AB

621AB

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [4 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200002-01-1

310 312

Task Title

LIGHTNING/HIRF PROTECTION-SECTION 19

Task code

Threshold Interval

CHK

Check : 2C

N

AMM 249200-210809

ALL

FUC

I

72 MO

N

AMM 249200-210-866

ALL

FUC

I

72 MO

N

AMM 249200-210-867

ALL

References

Ctrl

Eff

SECURITY CHECK OF THE FOLLOWING HARNESSES END FITTINGS AT FR.87 : - 1CS-G, 1CS-H Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 EL 200002-02-1

200002-03-1

Issue No

:

Date

:

315 316

LIGHTNING/HIRF PROTECTION-SECTION 19

311 312 313 314

LIGHTNING/HIRF PROTECTION-TAIL CONE

10 01/12/2013

FUNCTIONAL CHECK OF THE BONDING OF THE FOLLOWING BRAIDED CONDUITS: 4500VB, 4501VB, 4504VB, 4505VB, 4508VB, 4509VB - LH 4502VB, 4503VB, 4506VB, 4507VB, 4510VB - RH

FUNCTIONAL CHECK OF THE BONDING OF THE FOLLOWING BRAIDED CONDUITS: 5865VB, 5867VB, 5869VB

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [5 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200003-01-1

193

Task Title

LIGHTNING/HIRF PROT.-BELLY FAIRING

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 249200-210-810

ALL

GVI

Check : 4C

N

AMM 249200-210-820

275

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE FOLLOWING HARNESSES END FITTINGS, FROM FR.39 TO FR.40.2 : - 1541VB, 1543VB Access panels :

193AB Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 EL 191 192 198

200003-03-1

LIGHTNING/HIRF PROT.-BELLY FAIRING

294

FUNCTIONAL CHECK OF THE FOLLOWING BELLY FAIRING PRESSURE SEAL BONDING: 3586VP,3594VP,3686VP,3688VP,3583VP,3591VP

299 366

Access panels :

191CB

192CB

Total access time :

198CB 0.00 Hrs

Skills :

1.20 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [6 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200004-01-1

454 464

Task Title

LIGHTNING/HIRF PROTECTION-ENGINE PYLON

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 249200-210-811

ALL

CHK

Check : 2C

N

AMM 249200-210-817

ALL

DI

Check : 2C

N

AMM 249200-210-813

ALL

I

N

AMM 249200-210-864

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE HARNESS END FITTINGS, FROM RIB 10 TO TEE. Access panels :

454BR

454NR

Total access time :

464BR 464NR 0.00 Hrs

Skills :

0.50 MHrs

1 EL 731 741

200005-01-1

LIGHTNING/HIRF PROTECTION-MLG SECURITY CHECK OF THE END FITTINGS AT MLG BRAIDED CONDUIT. Skills :

0.30 MHrs

1 EL 731 741

200005-02-1

LIGHTNING/HIRF PROTECTION-MLG DETAILED INSPECTION OF ELEMENTS FITTED ON THE ROUTE 2M FROM UNION PLATE TO INTERFACE BRACKET ON STRUT AT MLG BRAIDED CONDUIT. Skills :

0.20 MHrs

1 EL 731 741

200005-04-1

Issue No

:

Date

:

10 01/12/2013

LIGHTNING/HIRF PROTECTION-MLG

FUC

72 MO

FUNCTIONAL CHECK OF THE BONDING OF BRAIDED CONDUITS LINKED TO PROXIMITY SENSORS 30GA1, 30GA2, 31GA1, 31GA2.

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [7 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200006-01-1

123 711

Task Title

LIGHTNING/HIRF PROTECTION-NLG

Task code

Threshold Interval

CHK

Check : 2C

N

AMM 249200-210-814

ALL

GVI

Check : 2C

N

AMM 249200-210-815

275

References

Ctrl

Eff

SECURITY CHECK OF THE FOLLOWING HARNESSES END FITTINGS AT NLG BRAIDED CONDUIT : - 1605VC-A, 1607VC-A, 2GH, 1GH Skills :

0.20 MHrs

1 EL 323

200007-01-1

LIGHTNING/HIRF PROTECTION-VERTICAL FIN

294

GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION INSTALLATION AT VERTICAL FIN. 5994VB, 5995VB, 5996VB, 5997VB

299 366

Access panels :

312AR

325ML

Total access time :

325NL 2.91 Hrs

Skills :

1.00 MHrs

1 EL R

323

200007-02-2

LIGHTNING/HIRF PROTECTION-VERTICAL FIN

GVI

Check : 2C

N

AMM 249200-210-815

943 946

GENERAL VISUAL INSPECTION OF FLY BY WIRE PROTECTION INSTALLATION AT VERTICAL FIN: - 5989VB, 5994VB, 5995VB, 5996VB, 5997VB, 6989VB, 6994VB, 6996VB

962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [8 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200121-01-1

121 122

Task Title

AVIONICS COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

72 MO

N

AMM 249200-100-801

ALL

GVI

I

144 MO

N

AMM 249200-210-829

ALL

RS

I

72 MO

N

AMM 249200-100-802 MRB 20.0.131/01

ALL

CLEANING OF EWIS INSTALLED IN THE AVIONICS COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : FLOOR PANELS Z120; INSULATION Z120; Access panels :

131AW

131BW

Total access time :

132AZ 132CW 1.51 Hrs

821

Skills :

2.00 MHrs

1 AF 121 122

200121-02-1

AVIONICS COMPARTMENT GENERAL VISUAL INSPECTION OF 710VU AND 740VU IN THE AVIONICS COMPARTMENT, (EWIS). Access panels :

132AZ

821

Total access time :

0.03 Hrs

Skills :

0.30 MHrs

1 AF 131 132

200131-01-1

FORWARD CARGO COMPARTMENT CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : SIDEWALL PANELS Z130 Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [9 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200131-03-1

131 132

Task Title

FORWARD CARGO COMPARTMENT

Task code

Threshold Interval

RS

I

RS

Check : 4C

144 MO

References

Ctrl

Eff

N

AMM 249200-210-830 MRB 20.0.131/02

ALL

N

AMM 249200-100-803 MRB 20.0.137/01

ALL

GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS). PREP. : CEILING PANELS Z130; SIDEWALL PANELS Z130; Access panels :


0.02 Hrs

Skills :

0.30 MHrs

1 AF 137 138

200137-01-1

BAY BEHIND FWD CARGO COMPARTMENT CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). Access panels :


0.02 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [10 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200141-01-1

141 142

Task Title

CENTER WING BOX

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-823 MRB 20.0.141/01

ALL

RS

I

144 MO

N

AMM 249200-100-804 MRB 20.0.145/01

ALL

GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE THE FUEL TANK (AS FAR AS VISIBLE), (EWIS). PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

147AZ

148AZ

Total access time :

734 744 0.00 Hrs

Skills :

0.50 MHrs

1 AF 145 146

200145-01-1

ZONE UNDER CABIN FLOOR CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN FLOOR (ONLY IF CONTAMINATED), (EWIS). PREP. : FLOOR PANELS Z250; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [11 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200151-03-1

151 152

Task Title

AFT CARGO COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

72 MO

N

AMM 249200-100-805 MRB 20.0.151/03

ALL

GVI

I

144 MO

N

AMM 249200-210-834 MRB 20.0.151/05

ALL

CLEANING OF EWIS INSTALLED IN THE AFT CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : SIDEWALL PANELS Z150; Access panels :


0.02 Hrs

Skills :

0.70 MHrs

1 AF 151 152

200151-05-1

AFT CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS). PREP. : CEILING PANELS Z150; LDL (IF INSTALLED); LDMCR (IF INSTALLED); SIDEWALL PANELS Z150; Access panels :


0.02 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [12 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200161-01-1

161 162

Task Title

BULK CARGO COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

RS

Check : 4C

N

AMM 249200-100-816 MRB 20.0.161/01

ALL

GVI

I

N

AMM 249200-210-835 MRB 20.0.161/02

ALL

CLEANING OF EWIS INSTALLED IN THE BULK CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : SIDEWALL PANELS Z160; Access panels :


0.02 Hrs

Skills :

0.40 MHrs

1 AF 161 162

200161-03-1

BULK CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS). PREP. : CEILING PANELS Z160; SIDEWALL PANELS Z160;

144 MO

Access panels :


0.02 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [13 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200211-01-1

211 212

Task Title

COCKPIT

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-806 MRB 20.0.211/01

ALL

GVI

I

144 MO

N

AMM 249200-210-836 MRB 20.0.211/02

ALL

CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z210; FLOOR PANELS Z210; SIDEWALL PANELS Z210; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.40 MHrs

1 AF 211 212

200211-02-1

COCKPIT GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE COCKPIT AT LEVEL OF LATERAL FLOOR STRUCTURE BETWEEN FR.1 TO FR.11, (EWIS). PREP. : FLOOR PANELS Z210; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [14 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200221-01-1

221 222

Task Title

Task code

Threshold Interval

FWD CABIN UTILITY AREA/COURIER COMPART

GVI

Check : 4C

N

AMM 249200-210-825 MRB 20.0.221/01

ALL

RS

I

N

AMM 249200-100-807 MRB 20.0.221/02

ALL

References

Ctrl

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEATS AND A/C AND SEAT TO SEAT CONNECTION INSTALLED IN THE FWD CABIN UTILITY AREA, (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY;

Eff

Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.02 MHrs

1 AF 221 222

200221-02-1

FWD CABIN UTILITY AREA CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN UTILITY AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : DOOR FRAME LININGS Z220; FCRC (IF INSTALLED); GALLEYS Z220; INSULATION Z220; LAVATORIES Z220;

144 MO

Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.60 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [15 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200221-03-1

221 222

Task code

Task Title

FWD CABIN UTILITY AREA

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-826 MRB 20.0.221/03

ALL

RS

I

144 MO

N

AMM 249200-100-808 MRB 20.0.223/01

ALL

GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED IN THE FWD CABIN UTILITY AREA. (EWIS) PREP. : DOOR FRAME LININGS Z220; GALLEYS Z220; INSULATION Z220; LAVATORIES Z220; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.20 MHrs

1 AF 223 224

200223-01-1

FWD CABIN UTILITY AREA OVERHEAD COPMPART CLEANING OF ALL EWIS AND CIRCUIT BREAKERS "5001 VE" INSTALLED IN THE FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z220; FCRC (IF INSTALLED); GALLEYS Z220; INSULATION Z220; LAVATORIES Z220; Access panels :

221AZ

221BZ

Total access time :

222AZ 222BZ 0.30 Hrs

831

841

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [16 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200223-02-1

223 224

Task Title

FWD CABIN UTILITY AREA OVERHEAD COPMPART

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-827 MRB 20.0.223/02

ALL

GVI

I

72 MO

N

AMM 249200-210-828 MRB 20.0.231/01

ALL

GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001 VE" AND "G", AND "P"´ ROUTES INSTALLED IN THE FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT, (EWIS). PREP. : CEILING PANELS Z220; GALLEYS Z220; LAVATORIES Z220; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.10 MHrs

1 AF 231 232

200231-01-1

FWD CABIN GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED IN THE FWD CABIN AREA, (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [17 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200231-02-1

231 232

Task Title

FWD CABIN

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-809

ALL

RS

I

144 MO

N

AMM 249200-100-810 MRB 20.0.233/01

ALL

CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : FLOOR PANELS Z230; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); SEATS AND FURNISHINGS Z230; SIDEWALL LININGS Z230; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

1.60 MHrs

1 AF 233 234

200233-01-1

FWD CABIN OVERHEAD COMPARTMENT CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z230; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z230; Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [18 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200233-03-1

233 234

Task Title

FWD CABIN OVERHEAD COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-857

ALL

GVI

I

72 MO

N

AMM 249200-210-831 MRB 20.0.241/01

ALL

GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE FORWARD CABIN OVERHEAD COMPARTMENT, (EWIS). PREP. : CEILING PANELS Z230; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z230; Skills :

0.20 MHrs 10.00 MHrs

1 AF 1 PRE 241 242

200241-01-1

MID CABIN UTILITY AREA GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED IN THE MID CABIN UTILITY AREA, (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY; Access panels :

832

842

Total access time :

0.04 Hrs

Skills :

0.02 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [19 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200241-02-1

241 242

Task Title

MID CABIN UTILITY AREA

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-811

ALL

RS

I

144 MO

N

AMM 249200-100-812

ALL

CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : FLOOR PANELS Z240; GALLEYS Z240; INSULATION Z240; LAVATORIES Z240; Access panels :

832

842

Total access time :

0.04 Hrs

Skills :

0.50 MHrs

1 AF 243 244

200243-01-1

MID CABIN UTILITY AREA OVERHEAD COMPARTM CLEANING OF ALL WIRING INSTALLED IN THE MID CABIN UTILITY AREA OVERHEAD COMPARTMENT AREA (ONLY CONTAMINATED WIRING), (EZAP). PREP. : CEILING PANELS AND OVERHEAD STOWAGE BINS FROM FR 31 TO FR 36; GALLEYS AND TOILETS IF INSTALLED; INSULATION TO BE DISPLACED AS REQUIRED; NOTE: THRESHOLD'S NEXT 4C CHECK FROM APPROVED DATE FOR A/C OVER 144 MO. Access panels :

832

842

Total access time :

0.04 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [20 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200243-03-1

243 244

Task Title

MID CABIN UTILITY AREA OVERHEAD COMPARTM

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-859

ALL

GVI

I

72 MO

N

AMM 249200-210-832

ALL

GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE MID CABIN UTILITY OVERHEAD COMPARTMENT AREA, (EWIS). PREP. : CEILING PANELS Z240; GALLEYS Z240; LAVATORIES Z240; Skills :

0.10 MHrs

1 AF 251 252

200251-01-1

MID CABIN GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION, INSTALLED IN THE MID CABIN AREA. (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND AND/OR SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [21 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200251-02-1

251 252

Task Title

MID CABIN

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-813

ALL

GVI

I

144 MO

N

AMM 249200-210-833

ALL

CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : FLOOR PANELS Z250; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); SEATS AND FURNISHINGS Z250; SIDEWALL LININGS Z250; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

2.80 MHrs

1 AF 251 252

200251-03-1

MID CABIN GENERAL VISUAL INSPECTION OF ALL "G" AND "P" ROUTE INSTALLED IN THE MID CABIN AREA, (EWIS). PREP. : GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); SEATS AND FURNISHINGS Z250; SIDEWALL LININGS Z250; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [22 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200253-01-1

253 254

Task Title

MID CABIN OVERHEAD COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-814

ALL

GVI

I

144 MO

N

AMM 249200-210-856

ALL

CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z250; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z250; STAIRHOUSE (IF INSTALLED); Access panels :

832

842

Total access time :

0.04 Hrs

Skills :

1.40 MHrs

1 AF 253 254

200253-04-1

Issue No

:

Date

:

10 01/12/2013

MID CABIN OVERHEAD COMPARTMENT GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA, (EWIS). PREP. : CEILING PANELS Z250; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z250; STAIRHOUSE (IF INSTALLED);

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [23 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200261-01-1

261 262

Task Title

Task code

GVI

AFT CABIN

Threshold Interval

I

72 MO

References

Ctrl

N

AMM 249200-210-838

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED IN THE AFT CABIN AREA, (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAT AND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [24 / 34] ATA

: 20

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200261-02-1

261 262

Task Title

Task code

RS

AFT CABIN

Threshold Interval

I

144 MO

References

Ctrl

N

AMM 249200-100-817

CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : DOOR FRAME LININGS Z260; FLOOR PANELS Z260; GALLEYS (IF INSTALLED); INSULATION Z260; LAVATORIES (IF INSTALLED); SEATS AND FURNISHINGS Z260; SIDEWALL LININGS Z260; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

2.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [25 / 34] ATA

: 20

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200263-01-1

263 264

Task Title

AFT CABIN OVERHEAD COMPARTMENT

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-818

ALL

GVI

I

144 MO

N

AMM 249200-210-858

ALL

CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z260; GALLEYS (IF INSTALLED); INSULATION Z260; LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z260; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

1.20 MHrs

1 AF 263 264

200263-04-1

AFT CABIN OVERHEAD COMPARTMENT GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS). PREP. : CEILING PANELS Z260; GALLEYS (IF INSTALLED); LAVATORIES (IF INSTALLED); OVERHEAD STOWAGE BINS Z260; Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [26 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200271-01-1

271 272

Task Title

Task code

GVI

AFT CABIN UTILITY AREA

Threshold Interval

I

72 MO

References

Ctrl

N

AMM 249200-210-839

GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLED IN THE AFT CABIN UTILITY AREA, (EWIS). NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY. PREP. : SEAT COVERS IF NECESSARY; Access panels :

834

844

Total access time :

0.04 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [27 / 34] ATA

: 20

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200271-02-1

271 272

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-819

ALL

GVI

I

144 MO

N

AMM 249200-210-840

ALL

CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY AREA (ONLY IF CONTAMINATED), (EWIS). PREP. : DOOR FRAME LININGS Z270; FLOOR PANELS Z270; GALLEYS Z270; LAVATORIES Z270; SEATS AND FURNISHINGS Z270; SIDEWALL LININGS Z270; Access panels :

833

843

Total access time :

0.04 Hrs

Skills :

0.60 MHrs

1 AF 271 272

200271-03-1

AFT CABIN UTILITY AREA GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED IN THE AFT CABIN UTILITY AREA, (EWIS). PREP. : GALLEYS Z270; INSULATION Z270; LAVATORIES Z270; NOTE: THRESHOLD'S NEXT 4C CHECK FOR A/C OVER 144 MO. Access panels :

833

843

Total access time :

0.04 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [28 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200273-01-1

273 274

Task Title

AFT CABIN UTILITY AREA OVERHEAD

Task code

Threshold Interval

References

Ctrl

Eff

RS

I

144 MO

N

AMM 249200-100-820

ALL

GVI

I

144 MO

N

AMM 249200-210-841

ALL

CLEANING OF EWIS AND CIRCUIT BREAKERS "5005 VE" INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED), (EWIS). PREP. : CEILING PANELS Z270; GALLEYS Z270; INSULATION Z270; LAVATORIES Z270; NOTE: THRESHOLD IS NEXT 4C FOR A/C OVER 144 MO. Access panels :

833

843

Total access time :

0.04 Hrs

Skills :

0.40 MHrs

1 AF 273 274

200273-02-1

AFT CABIN UTILITY AREA OVERHEAD COMPARTM GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5005 VE" AND "P" ROUTE INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT, (EWIS). Access panels :

833

843

Total access time :

0.04 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [29 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200315-01-1

315 316

Task code

Task Title

TAIL CONE APU AND ACCESSORY COMPARTMENT

Threshold Interval

References

Ctrl

Eff

GVI

I

54 MO

N

AMM 249200-210-842

ALL

GVI

I

144 MO

N

AMM 249200-210-843

ALL

GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES INSTALLED IN THE TAIL CONE FIREWALL AND APU AREA, (EWIS). Access panels :

315AL

316AR

Total access time :

0.08 Hrs

Skills :

0.20 MHrs

1 AF 319

200319-02-1

HORIZONTAL STABILIZER CENTER BOX GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS). PREP. : DISCONNECT SCAVENGE WATER SYSTEM PIPE; Access panels :

312AR

313AL

Total access time :

319AL 319AR 0.00 Hrs

319BL

319DR

319ER

Skills :

0.40 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [30 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200333-01-1

333 343

Task code

Task Title

HORIZONTAL STABILIZER LATERAL BOX

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-844

ALL

SDI

I

144 MO

N

AMM 249200-220-803

ALL

GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 3 TO RIB 4 LH/RH, (EWIS). PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

331AT 343AB

331BT 343AR

Total access time :

333AB 343AT

333AL

333AT

341AT

341BT

0.00 Hrs

Skills :

0.20 MHrs

2 AF 333 343

200333-05-1

HORIZONTAL STABILIZER LATERAL BOX SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO RIB 20 LH/RH, (EWIS). PREP. : FUEL TANK DRAINED AND VENTED; PEELABLE HOLE COVERS; Access panels :

333BB 334GB 344GB

333CB 343BB 346AB

Total access time :

333DB 343CB

333EB 343DB

333FB 343EB

333GB 343FB

334AZ 343GB

0.20 Hrs

Skills :

1.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [31 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200541-01-1

541 641

Task code

Task Title

GVI

INNER FUEL TANK

Threshold Interval

I

144 MO

References

Ctrl

N

AMM 249200-210-848

GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER FUEL TANK (AS FAR AS VISIBLE), (EWIS). PREP. : FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FUEL TANK DRAINED AND VENTED; Access panels :

541AB 541DZ 541HB 541QB 641CB 641FZ 641MB

541AZ 541EB 541JB 541RB 641CZ 641GB 641NB

Total access time :

541BB 541EZ 541KB 541SB 641DB 641GZ 641PB 23.44 Hrs

541BZ 541FB 541LB 641AB 641DZ 641HB 641QB

541CB 541FZ 541MB 641AZ 641EB 641JB 641RB

541CZ 541GB 541NB 641BB 641EZ 641KB 641SB

541DB 541GZ 541PB 641BZ 641FB 641LB

Skills :

2.20 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [32 / 34] ATA

: 20

Eff ALL


20

STANDARD PRACTICE

Task Number

Zone

200542-01-1

542 642

Task code

Task Title

OUTER FUEL TANK

Threshold Interval

References

Ctrl

Eff

GVI

I

144 MO

N

AMM 249200-210-849

ALL

GVI

I

144 MO

N

AMM 249200-210-851

ALL

GENERAL VISUAL INSPECTION OF EWIS IN THE OUTER FUEL TANK (RIB 23 TO RIB 33)(AS FAR AS VISIBLE), (EWIS). PREP. : FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED; Access panels :

542AB 542HB 642DB 660DB

542BB 542JB 642EB

Total access time :

542CB 542KB 642FB

542DB 560DB 642GB

542EB 642AB 642HB

542FB 642BB 642JB

542GB 642CB 642KB

17.40 Hrs

Skills :

0.60 MHrs

2 AF 550 650

200550-01-1

VENT SURGE TANK GENERAL VISUAL INSPECTION OF EWIS WITHIN THE VENT SURGE TANK (AS FAR AS VISIBLE), (EWIS). PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

550AB

550BB

Total access time :

550CB

650AB

650BB

650CB

6.00 Hrs

Skills :

0.50 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [33 / 34] ATA

: 20


20

STANDARD PRACTICE

Task Number

Zone

200571-01-1

571 671

Task Title

Task code

GVI

MAIN LANDING GEAR WELL

Threshold Interval

I

144 MO

References

Ctrl

Eff

N

AMM 249200-210-852

ALL

N

AMM 249200-210-853 SIL 24-077

ALL

GENERAL VISUAL INSPECTION OF FUEL PUMP EWIS (AS FAR AS VISIBLE), (EWIS). PREP. : FUEL PUMP FAIRINGS Z500; FUEL PUMP FAIRINGS Z600; Skills :

0.30 MHrs

1 AF 300 500 600 700 800

202800-01-1

DI

ELECTRICAL BONDING DETAILED INSPECTION OF BONDING LEADS LOCATED ON THE FOLLOWING MOVABLE SURFACES: FLAPS, FLAP TRACK FAIRINGS, SLATS, SPOILERS, AILERONS, NOSE LANDING GEAR DOORS, MAIN LANDING GEAR DOORS, PASSENGER DOORS, ELEVATORS AND RUDDER HINGE ARMS.

Check : 1C

Skills :

1.25 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 20 [34 / 34] ATA

: 20


21


Task Number

Zone

212100-03-1

137 138 145 146

Task Title

Task code

Threshold Interval

CABIN AIR DISTRIBUTION AND RECIRCULATION

DIS

I

GVI

Check : 4C

4 000 FH

References

Ctrl

Eff

N

AMM 212141-960-801

ALL

N

AMM 212143-200-801

ALL

DISCARD RECIRCULATION FILTER ELEMENTS. NOTE : - 5600 FH, IF PALL STANDARD RECIRCULATION FILTER INSTALLED (P/N QB0408-01 AND PREVIOUS) - 5600 FH, IF LE BOZEC-DONALDSON RECIRCULATION FILTER INSTALLED (P/N 430B100-2 AMT A, P/N /430B100-3) - 4000 FH, IF LE BOZEC-DONALDSON RECIRCULATION FILTER INSTALLED (P/N 430B100-2 AND PREVIOUS) NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

131CX

132CX

Total access time :

151BW 152BW 2.00 Hrs

Skills :

1.20 MHrs

1 CA 137 138

212100-04-1

CABIN AIR DISTRIBUTION AND RECIRCULATION VISUAL CHECK OF MIXER UNIT NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [1 / 15] ATA

: 21


21


Task Number

Zone

212100-06-1

200

Task Title

Task code


DIS

Threshold Interval

I

800 FH

References

Ctrl

N

AMM 233653-920-801

275 294

Check : 1A

CABIN AIR DISTRIBUTION AND RECIRCULATION DISCARD VIDEO CONTROL CENTER AIR FILTER ELEMENTS NOTE: ETOPS SIGNIFICATION SYSTEMS

Eff

299 366 946

Skills :

0.30 MHrs

1 AF 200

212100-07-1


OP

I

20 000 FH

N

AMM 261800-710-805

294

OPERATIONAL CHECK OF STAND ALONE SMOKE DETECTION SYSTEM SMOKE TEST BUTTON NOTE: IF VCC WITH SMOKE TEST BUTTON INSTALLED NOTE: ETOPS SIGNIFICATION SYSTEMS 137

212100-11-1


275 299 366 946

VCK

Check : 1C

N

AMM 212143-200-802

ALL

DIS

I

N

AMT 212300-600-801 SIL 21-105

ALL

CABIN AIR DISTRIBUTION AND RECIRCULATION VISUAL INSPECTION OF ICE PROTECTION GRIDS ACCESS: 131CX 132CX NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.60 MHrs

1 AF 200

212300-01-1

LAVATORY/GALLEY VENTILATION DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT

1 200 FH

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [2 / 15] ATA

: 21


21


Task Number

Zone

212500-01-1

210

Task Title

AIR CONDITIONING COMPARTMENT VENTILATION

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 212500-710-801

ALL

DI

Check : 4C

N

AMM 212500-200-801

ALL

I

N

AMM 212500-200-804

ALL

N

AMM 212600-710-805

ALL

OPERATIONAL CHECK OF ABNORMAL VENTILATION WARNING Skills :

0.20 MHrs

1 AF 192

212500-02-1

AIR CONDITIONING COMPARTMENT VENTILATION DETAILED INSPECTION OF TURBOFAN SUPPLY DUCT Skills :

0.50 MHrs

1 AF 190

212500-03-1

AIR CONDITIONING COMPARTMENT VENTILATION

GVI

36 MO See note

GENERAL VISUAL INSPECTION OF PICCOLO TUBES. Access panels :

192GB

192JB

Total access time :

192PB

193AB

2.30 Hrs

Skills :

0.30 MHrs

1 AF 210

212600-01-1


OP

Check : 2C

OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [3 / 15] ATA

: 21


21


Task Number

Zone

212600-02-2

210

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 212600-710-806 CMP 21-2-0000-004

ALL

OP

Check : 2C

N

AMM 212600-710-802

ALL

OP

I

N

AMM 212600-710-808

ALL

OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION NOTE : CMP TASK NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.20 MHrs

1 AF 210

212600-03-1

AVIONICS EQUIPMENT VENTILATION OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.20 MHrs

1 AF 210

212600-04-1


10 000 FH

OPERATIONAL CHECK OF COOLING EFFECT DETECTOR (AEVC SYSTEM TEST) NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [4 / 15] ATA

: 21


21


Task Number

Zone

212600-06-1

121

Task Title


Task code

DI

Threshold Interval

References

Ctrl

Eff

Check : 2C

N

AMM 212600-200-803

ALL

CLN

I

N

AMM 122113-100-802

ALL

OP

Check : 4C

N

AMM 212800-710-807 SB 21-3128

275

DETAILED INSPECTION OF: - INSIDE OF ADIRU VENTILATION HOSES FOR ACCUMULATION OF DEBRIS - DRAIN HOLE IN EACH ADIRU TRAY - WATER DRAIN LOCATED ON LOWER SIDE OF EACH VENTILATION DUCT NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

121HF

121KF

Total access time :

122JF 0.00 Hrs

Skills :

0.16 MHrs

1 AF 120

212600-07-1


42 MO

CLEANING OF RELAY BOX VU PANELS GRIDS NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.25 MHrs

1 AF 150 210

212800-04-2

LOWER DECK CARGO COMPARTMENT HEATING, VE OPERATIONAL CHECK OF HARD WIRED BACKUP TO VERIFY CLOSING OF LOWER DECK MOBILE CREW REST ISOLATION VALVES

299 366

Skills :

0.30 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : SYS - 21 [5 / 15] ATA

: 21


21


Task Number

Zone

212800-05-1

210

Task Title

LOWER DECK CARGO COMPARTMENT HEATING, VE

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 4C

N

AMM 212800-710-803

ALL

OP

I

20 000 FH

N

AMM 213100-710-802

ALL

OP

I

20 000 FH

N

AMM 213100-710-803

ALL

OP

I

20 000 FH

N

AMM 213100-710-804

ALL

OPERATIONAL CHECK OF HARD WIRED BACKUP OF VENTILATION CONTROLLER (TO VERIFY CLOSING OF ISOLATION VALVES AND COLD AIR VALVE) Skills :

0.50 MHrs

1 AF 210

213100-01-1

PRESSURE CONTROL AND MONITORING OPERATIONAL CHECK OF MANUAL MODE NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 EL 210

213100-02-1

PRESSURE CONTROL AND MONITORING OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN DITCHING CONFIGURATION NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.05 MHrs

1 AF 210

213100-03-1

PRESSURE CONTROL AND MONITORING OPERATIONAL CHECK OF OUTFLOW VALVE OPENING (50%) BY EMERGENCY RAM AIR SWITCH NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.05 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [6 / 15] ATA

: 21


21


Task Number

Zone

213100-04-1

210

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

I

20 000 FH

N

AMM 213100-710-807

ALL

FUC

I

24 000 FH

N

AMM 213100-720-801

943

I

6 YE

OPERATIONAL CHECK OF LANDING FIELD ELEVATION SELECTOR BY MEANS OF INITIATED TEST (VIA MCDU) NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.15 MHrs

1 AF R

210 270 310

213100-05-2

210

213100-06-1

PRESSURE CONTROL AND MONITORING FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P PROTECTION OF SAFETY VALVES NOTE: THIS TASK MAY BE ALTERNATIVELY ACCOMPLISHED AS AN OFF AIRCRAFT TASK. REFER TO AMM PROCEDURE FOR REMOVAL AND INSTALLATION 213152-000-801 AND 213152-400-801 PREP. : ACCESS THROUGH PANEL OF REAR GALLEY; NOTE: ETOPS SIGNIFICATION SYSTEMS PRESSURE CONTROL AND MONITORING

946 962 1019 1256 1266

OP

Check : 4C

N

AMM 213100-710-806

OPERATIONAL CHECK OF NEGATIVE PRESSURE RELIEF VALVE NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [7 / 15] ATA

: 21

ALL


21


Task Number

Zone

213100-07-1

210 270

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

I

20 000 FH

N

AMM 213100-710-805

ALL

DIS

I

18 MO

N

AMM 214300-200-801

ALL

GVI

I

24 000 FH

N

AMM 215200-200-801

ALL

DI

I

24 000 FH

N

AMM 215200-220-801

ALL

OPERATIONAL CHECK OF POSITION INDICATION OF SAFETY VALVES NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.20 MHrs

2 AF 160

214300-01-1

FAN HEATER-BULK CARGO COMPARTMENT DETAILED INSPECTION AND CLEANING OF THE FAN HEATER NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH AIRLINE EXPERIENCE AND OPERATING ENVIRONMENT Skills :

1.00 MHrs

1 AF 190

215000-05-1

AIR COOLING TEMPERATURE CONTROL GENERAL VISUAL INSPECTION OF PACK AIR SUPPLY DUCTS, CLAMPS AND BELLOWS (BETWEEN PACK OUTLET AND MIXER UNIT). NOTE: ETOPS PARALLEL SYSTEM Skills :

0.10 MHrs

1 AF 190

215000-06-1

AIR COOLING TEMPERATURE CONTROL DETAILED INSPECTION OF PACK DOWNSTREAM CHECK VALVES FLAPPERS FOR CONDITION AND OPERATION NOTE: ETOPS PARALLEL SYSTEM Skills :

1.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [8 / 15] ATA

: 21


21


Task Number

Zone

215000-11-2

190 210

Task code

Task Title

FUC

AIR COOLING FUNCTIONAL CHECK OF RAM AIR INLET DOORS FOR BACKLASH. NOTE: ETOPS SIGNIFICATION SYSTEMS

Threshold Interval

I

8 500 FH

I

18 MO

I

36 MO

References

Ctrl

Eff

N

AMM 215300-220-802 ISB 21-3048

ALL

N

AMM 215200-920-801 SIL 21-143

275

Access panels :

191FB

193BB

Total access time :

193CB 3.14 Hrs

Skills :

0.50 MHrs

1 AF 190

215000-12-1

REM

AIR COOLING REMOVE AND REPLACE THE COMBO SEALS AND PERISEALS ON THE HOT AIR INLET CIRCUIT, TRIM AIR DUCTING AND PACK DUCTING NOTE: - TASK MAY BE COMBINED WITH TASK 361242-02-1 - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR´S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED NOTE: ETOPS PARALLEL SYSTEMS

299 366

Access panels :

131BX 192PB

131CX 193AB

Total access time :

132CX 191DB 193BB 193DB 0.00 Hrs

191FB

192GB

192JB

Skills :

15.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : SYS - 21 [9 / 15] ATA

: 21


21


Task Number

Zone

215100-01-1

190

Task Title

AIR CONDITIONING

Task code

Threshold Interval

DIS

I

DVI

Check : 1C

2 400 CY

References

Ctrl

Eff

N

AMM 215100-920-801

ALL

N

AMM 215300-220-808 ISB 21-3075

275

DISCARD FLOW CONTROL VALVE FILTERS NOTE: ETOPS SIGNIFICATION SYSTEMS NOTE: TASK APPLICABLE FOR A/C FITTED WITH P/N: 964F0000-01 Skills :

1.00 MHrs

1 AF 190

215300-02-1

PACK OUTLET DUCT DETAILED INSPECTION OF THE PACK OUTLET DUCTS NOTE: ETOPS SIGNIFICATION SYSTEMS

294 299 366

Skills :

6.00 MHrs

1 AF 190

215354-01-1

CLN

WATER INJECTOR CLEANING AND DETAILED INSPECTION FOR EROSION OF PACK WATER INJECTOR NOZZELS AND INSPECTION AND REPLACEMENT OF COMPRESSOR TO TURBINE FLEXIBLE HOSE. NOTE: ETOPS SIGNIFICATION SYSTEMS

I

18 000 FH

I

42 MO

N

AMM 215300-100-802

Access panels :

191BB

191FB

Total access time :

6.06 Hrs

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [10 / 15] ATA

: 21

ALL


21


Task Number

Zone

215500-01-1

190 210

Task Title

AIR COOLING TEMPERATURE CONTROL OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM OPENING

Task code

Threshold Interval

DI OP

I

DI

Check : 4C

20 000 FH

References

Ctrl

Eff

N

AMM 215500-200-801 AMM 215500-710-801

ALL

N

AMM 215500-200-801 SIL 21-124

ALL

Access panels :

131CG

132AZ

Total access time :

191EB 193CB 0.00 Hrs

Skills :

0.15 MHrs

1 AF 190

215500-02-1

EMERGENCY RAM AIR INLET EMERGENCY RAM AIR INLETEMERGENCY RAM AIR CHECK VALVE, DETAILED INSPECTION OF SKIN VALVE FLAPPERS FORERS FOR CONDITION AND OPERATION Access panels :

131CG

132AZ

Total access time :

191EB 193CB 0.01 Hrs

Skills :

0.05 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [11 / 15] ATA

: 21


21


Task Number

Zone

215500-03-1

190

Task Title

EMERGENCY RAM AIR INLET

Task code

Threshold Interval

DI

I

DI

Check : 4C

24 000 FH

References

Ctrl

Eff

N

AMM 215500-220-803

ALL

N

AMM 215500-220-804

ALL

DETAILED INSPECTION OF LP GROUND AIR CHECK VALVE FLAPPERS FOR CONDITION AND OPERATION PREP. : SKIN CHECK VALVE; Access panels :

191EB

193CB

Total access time :

0.00 Hrs

Skills :

0.05 MHrs

1 AF 190

215500-04-1

EMERGENCY RAM AIR INLET DETAILED INSPECTION OF EMERGENCY RAM AIR CHECK VALVE FLAPPERS FOR CONDITION AND OPERATION Access panels :

131CG

191EB

Total access time :

193CB 0.00 Hrs

Skills :

0.05 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [12 / 15] ATA

: 21


21


Task Number

Zone

216000-02-1

130

Task Title

Task code

DI


Threshold Interval

References

Ctrl

Eff

Check : 4C

N

AMM 216300-200-801

ALL

CLN

I

10 000 FH

N

AMM 216317-100-802

ALL

CLN

I

800 FH

N

AMM 216317/7 AMT 216317-100-803

ALL

DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS FOR CONDITION AND OPERATION NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

131BX

131CX

Total access time :

132CX 191EB 2.72 Hrs

193BB

Skills :

0.80 MHrs

1 AF 210

216000-03-1

AIR COOLING TEMPERATURE CONTROL CLEAN FLIGHT DECK TEMPERATURE SENSORS NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 AF 200

216000-04-1

AIR COOLING TEMPERATURE CONTROL CLEAN INLET GRID OF CABIN TEMPERATURE SENSORS (IN ZONE 230, 240, 250) NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE NOTE: ETOPS SIGNIFICATION SYSTEMS

Check : 1A

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [13 / 15] ATA

: 21


21


Task Number

Zone

216000-05-1

200

Task Title


Task code

DIS

Threshold Interval

I

800 FH

Eff

N

AMM 216317/3 AMT 216317-920-801

ALL

N

AMM 216317-100-804

ALL

N

AMM 215300-210-801

ALL

Check : 1A

DISCARD CABIN TEMPERATURE SENSOR FILTERS NOTE: ETOPS SIGNIFICATION SYSTEMS

References

Ctrl

Skills :

0.50 MHrs

1 AF 200

216000-06-1


CLN

See note Check : 1C

CLEAN CABIN TEMPERATURE SENSOR AND NOZZLE NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.50 MHrs

1 AF 191 192

216000-08-1

PACK CONTROL AND INDICATING

GVI

I

20 000 FH

GENERAL VISUAL INSPECTION OF HEATSHIELDS FOR CONDITION AND VISIBLE DAMAGE NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

191KB

192JB

Total access time :

192MB

193BB

0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [14 / 15] ATA

: 21


21


Task Number

Zone

216000-09-1

190

Task Title

AIR COOLING TEMPERATURE CONTROL DISCARD TRIM AIR PRESSURE REGULATING VALVE FILTER NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE NOTE: ETOPS SIGNIFICATION SYSTEMS

Task code

GVI

Threshold Interval

Ctrl

See note

N

Check : 2C

References

AMM 216300-920-801 SIL 21-134

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 21 [15 / 15] ATA

: 21

Eff ALL


22

AUTO FLIGHT

Task Number

Zone

221000-01-2

210

Task Title

AUTOPILOT/FLIGHT DIRECTOR

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 2C

N

AMM 221000-710-801 CMP 22-2-0000-001

ALL

OP

Check : 4C

N

AMM 221000-710-803

ALL

OP

Check : 4C

N

AMM 223000-710-801

ALL

OP

I

N

AMM 227000-710-803

ALL

OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION NOTE : CMP TASK NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 AV 210

221100-01-1

AUTOPILOT/FLIGHT DIRECTOR OPERATIONAL CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING DEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.30 MHrs

1 AV 210

223100-01-1

AUTOTHRUST OPERATIONAL CHECK OF A/THR ISOLATION FROM ENGINE CONTROL NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.30 MHrs

1 AV 210

227100-01-1

FLIGHT MANAGEMENT DATA BASE

48 MO

OPERATIONAL CHECK OF FM SOURCE SWITCHING NOTE: ETOPS PARALLEL SYSTEM Skills :

0.30 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 22 [1 / 2] ATA

: 22


22

AUTO FLIGHT

Task Number

Zone

227200-01-1

210

Task Title

FLIGHT MANAGEMENT NAVIGATION

Task code

Threshold Interval

OP

I

OP

OP

References

Ctrl

Eff

N

AMM 227000-710-804

ALL

Check : 1C

N

AMM 227000-710-802

ALL

Check : 1C

N

AMM 227000-710-801

ALL

48 MO

OPERATIONAL CHECK OF BACK-UP NAVIGATION FUNCTION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.30 MHrs

1 AV 210

227500-01-1

FLIGHT MANAGEMENT DISPLAYS OPERATIONAL CHECK OF MCDU 3 TRANSFER NOTE: ETOPS PARALLEL SYSTEM Skills :

0.10 MHrs

1 AV 210

227500-02-1

FLIGHT MANAGEMENT DISPLAYS OPERATIONAL CHECK OF MCDU ANNUNCIATORS NOTE: ETOPS PARALLEL SYSTEM Skills :

0.05 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 22 [2 / 2] ATA

: 22


23

COMMUNICATI0NS

Task Number

Zone

233300-01-1

200

Task Title

AUDIO MANAGEMENT (INTEGRATING/FLIGHT INT

Task code

Threshold Interval

120

233300-02-1

IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)

Eff

OP

I

22 600 FH

N

AMM 233300-710-817 SIL 23-049

ALL

DIS

I

2 400 FH

N

AMM 233300-920-801

943

OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION INSTALLED FROM FLIGHT DECK (IF INSTALLED) AND CABIN. R

References

Ctrl

946

DISCARD IFE-RACK FILTERS

962 1019 1256 1266

Skills :

0.00 MHrs

1 EL 200

233300-03-1

IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)

RS

I

10 000 FH

N

AMM 233653-100-801

ALL

OP

I

800 FH

N

AMM 233300-200-801

ALL

OP

Check : 1C

N

AMM 235100-710-804

ALL

CLEANING OF VENTILATION GRIDS AND VENTILATOR HOUSING FROM IFE COMPONENTS INSTALLED IN THE CABIN (VCC/RCC). Skills :

1.00 MHrs

1 EL 200

233300-04-1

IN-FLIGHT ENTERTAINMENT SYSTEM (IFES) GENERAL VISUAL INSPECTION OF SEAT ELECTRONIC BOX(SEB)

210

235100-01-1

AUDIO MANAGEMENT (INTEGRATING/FLIGHT INT OPERATIONAL CHECK OF OXYGEN MASK MICROPHONE Skills :

1.20 MHrs

2 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 23 [1 / 4] ATA

: 23


23

COMMUNICATI0NS

Task Number

Zone

235100-02-1

210

Task Title

AUDIO MANAGEMENT (INTEGRATING/FLIGHT INT

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 2C

N

AMM 235100-710-803

ALL

FUC

Check : 1C

N

AMM 236100-200-801

ALL

GVI

Check : 1C

N

AMM 236100-210-801

ALL

OP

Check : 1C

N

AMM 237100-710-801

ALL

OPERATIONAL CHECK OF CAPTAIN AND F/O ACP SWITCHING TO THIRD ACP Skills :

0.60 MHrs

1 AF 300 500 600

236100-01-1

STATIC DISCHARGER CHECK RESISTANCE FROM THE DISCHARGER TO THE BASE (RETAINER) AND FROM THE BASE (RETAINER) TO THE AIRCRAFT STRUCTURE Skills :

0.75 MHrs

1 RA 300 500 600

236100-02-1

STATIC DISCHARGER GENERAL VISUAL INSPECTION OF STATIC DISCHARGER. Skills :

0.60 MHrs

1 AF 210

237100-01-1

COCKPIT VOICE RECORDER OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING Skills :

0.30 MHrs

1 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 23 [2 / 4] ATA

: 23


23

COMMUNICATI0NS

Task Number

Zone

237100-02-1

210

Task Title

COCKPIT VOICE RECORDER

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 237100-710-802

ALL

OP

I

22 600 FH

N

AMM 237300-710-808

ALL

OP

I

11 300 FH

N

AMM 237300-710-810

ALL

OP

I

20 000 FH

N

AMM 237300-710-804

ALL

OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING TIME DELAY RELAY Skills :

0.60 MHrs

2 RA 200 210

237300-01-1

CABIN INTERCOMMUNICATION DATA SYSTEM (CI OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, DEUS-A CUT OFF FUNCTION Skills :

0.30 MHrs

1 RA 200 210

237300-03-1

CABIN INTERCOMMUNICATION DATA SYSTEM (CI OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU Skills :

0.20 MHrs

2 RA 200 210

237300-04-1

CABIN INTERCOMMUNICATION DATA SYSTEM (CI OPERATIONAL CHECK OF EVAC FUNCTION Skills :

0.10 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 23 [3 / 4] ATA

: 23


R

23

COMMUNICATI0NS

Task Number

Zone

237300-10-1

200 210

Task Title

CABIN INTERCOMMUNICATION DATA SYSTEM (CI

Task code

OP

Threshold Interval

I

20 000 FH

References

Ctrl

N

AMM 237300-710-839

Eff 943 946

OPERATIONAL CHECK OF BATTERY POWERED CIDS PA OPERATION.

962 1019 1256 1266

210

238100-01-1

OP

RADIO MANAGEMENT

I

36 MO

N

AMM 238100-710-802

OPERATIONAL CHECK OF RADIO NAVIGATION BACK-UP MODE Skills :

0.20 MHrs

1 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 23 [4 / 4] ATA

: 23

ALL


24

ELECTRICAL POWER

Task Number

Zone

240000-01-1

100 200

Task Title

ELECTRICAL POWER - GENERAL

Task code

Threshold Interval

References

Ctrl

Eff

CHK

I

42 MO

N

AMM 240000-200-803 SIL 20-017

ALL

FUC

I

2 100 FH

N

AMM 242100/6 AMT 242100-210-815

ALL

OPENING AND CLOSING OF ALL CIRCUIT BREAKERS (EXCEPT RCCB) Skills :

2.00 MHrs

1 EL 412 422

242100-12-1

INTEGRATED DRIVE GENERATOR CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT NOTE: ETOPS PARALLEL SYSTEM Skills :

1 ENG

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

0.50 MHrs

Page : SYS - 24 [1 / 6] ATA

: 24


24

ELECTRICAL POWER

Task Number

Zone

242100-13-1

412

Task Title

INTEGRATED DRIVE GENERATOR DISCARD SCAVENGE FILTER AND DRAIN AND REPLENISH INTEGRATED DRIVE GENERATOR OIL SYSTEM NOTE : - REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL. - DO NOT PERFORM THE SERVICING ON BOTH IDG AT THE SAME TIME BUT ON ONE UNIT ONLY. SERVICING ON THE OTHER IDG TO BE PERFORMED AFTER 400FH. - IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE OTHER IDG. NOTE: ETOPS PARALLEL SYSTEM NOTE : CMP TASK

Task code

DIS

Threshold Interval

T

150 FH

I

800 FH See note

References

Ctrl

B1 AMM CMP SIL SIL SIL SIL

121324-612-807 24-2-0000-001 SUN236 SUN279 SUN346 24-049

Access panels :

415BL

416BR

Total access time :

417AL 418AR 0.04 Hrs

Skills :

0.50 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 24 [2 / 6] ATA

: 24

Eff ALL


24

ELECTRICAL POWER

Task Number

Zone

242100-13-2

422

Task Title

INTEGRATED DRIVE GENERATOR DISCARD SCAVENGE FILTER AND DRAIN AND REPLENISH INTEGRATED DRIVE GENERATOR OIL SYSTEM NOTE : - REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH AT 150FH AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL. - DO NOT PERFORM THE SERVICING ON BOTH IDG AT THE SAME TIME BUT ON ONE UNIT ONLY. SERVICING ON THE OTHER IDG TO BE PERFORMED AFTER 400FH. - IN ORDER TO AVOID RISK OF MULTIPLE IDG LOSSES, DO NOT PERFORM THIS SERVICING ON BOTH IDG AT THE SAME TIME. IT IS RECOMMENDED TO WAIT AT LEAST TWO FLIGHTS BEFORE PERFORMING THIS SERVICING ON THE OTHER IDG. NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

Task code

DIS

Threshold Interval

T

150 FH

I

800 FH See note

References

Ctrl

N

AMT CMP SIL SIL SIL

121324-612-807 24-2-0000-001 SUN236 SUN279 SUN346

Access panels :

425BL

426BR

Total access time :

427AL 428AR 0.04 Hrs

Skills :

0.50 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 24 [3 / 6] ATA

: 24

Eff ALL


24

ELECTRICAL POWER

Task Number

Zone

242100-15-1

412 422

Task Title

INTEGRATED DRIVE GENERATOR

Task code

OPC

Threshold Interval

Ctrl

See note

N

AMM 242100-710-806

ALL

References

Eff

Check : 4C

OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR DISCONNECT FUNCTION NOTE : TASK SHOULD BE ACCOMPLISHED AT OPPORTUNITY OF ENGINE OR IDG CHANGE. NOTE: ETOPS PARALLEL SYSTEM Skills :

0.40 MHrs

1 EN 210

242200-01-1

AC GENERATION

OP

I

42 MO

N

AMM 242200-710-801

ALL

OP

I

42 MO

N

AMM 242400-710-803 CMP 24-2-0000-005

ALL

OPERATIONAL CHECK OF AC GENERATION SIDE 1 AND SIDE 2 ISOLATION Skills :

0.15 MHrs

1 EL R

210

242400-03-2

AC EMERGENCY GENERATION OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM Skills :

0.02 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 24 [4 / 6] ATA

: 24


R

24

ELECTRICAL POWER

Task Number

Zone

242400-05-2

210

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

I

18 MO

N

AMM 242400-710-807

ALL

OP

I

800 FH

N

AMM 243400/5 AMT 243400-710-802

ALL

VCK

I

24 MO

N

AMM 243200-210-803 SIL 24-086

ALL

VCK

I

24 MO

N

AMM 243400-210-802 SIL 24-086

ALL

VCK

I

24 MO

N

AMM 243200-210-804 SIL 24-086

ALL

OPERATIONAL CHECK OF CSM/G DISCONNECTION WITH SIMULATED ENGINES FLAMED OUT CONDITION AND SLATS EXTENDED NOTE: ETOPS PARALLEL SYSTEM Skills :

0.40 MHrs

2 EL 210

243500-03-1

DC GENERATION OPERATIONAL CHECK OF DC BAT BUS AND DC ESS BUS ISOLATION Skills :

0.02 MHrs

1 EL 243500-04-1

243500-05-1

120 162

DC MAIN GENERATION

120

DC EMERGENCY GENERATION

VISUAL INSPECTION OF TRU 1,2, THE INSIDE OF HOT AIR EXTRACTION DUCT AND THE ADJACENT AREA.

VISUAL INSPECTION OF THE ESSENTIAL TRU AND THE ADJACENT AREA. 162

243500-06-1

DC MAIN GENERATION VISUAL INSPECTION OF THE TRU APU AND THE ADJACENT AREA.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 24 [5 / 6] ATA

: 24


24

ELECTRICAL POWER

Task Number

Zone

245000-01-1

200 210

Task Title

AC ELECTRICAL LOAD DISTRIBUTION

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 245100-710-801

ALL

OP

I

N

AMM 245200-710-802

ALL

OPERATIONAL CHECK OF COMMERCIAL LOAD SHEDDING Skills :

0.30 MHrs

1 EL 210

245000-02-1


24 MO

Check : C1

OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION Skills :

0.10 MHrs

1 EL 210

245000-03-1


OP

Check : 2C

N

AMM 245200-710-801

ALL

OP

I

N

AMM 282200-710-807

ALL

OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN EMERGENCY CONFIGURATION Skills :

0.02 MHrs

1 EL 210

245000-05-1


24 MO

OPERATIONAL CHECK AFT APU PUMP SHEDDING IN LAND RECOVERY CONFIGURATION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.10 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 24 [6 / 6] ATA

: 24


25


Task Number

Zone

251100-01-1

210

Task Title

COCKPIT SEATS

Task code

Threshold Interval

GVI

I

FUC

References

Ctrl

Eff

N

AMM 251100-200-801

ALL

Check : 1C

N

AMM 251100-200-804 SIL 25-108

ALL

GVI

I

42 MO

N

AMM 252100-210-801

ALL

OP

I

42 MO

N

AMM 252100-210-802

ALL

GVI

I

42 MO

N

AMM 252100-210-803

ALL

6 YE

VISUAL CHECK OF SEAT STRUCTURE AND SEAT ATTACHMENT Skills :

0.20 MHrs

1 AF 210

251100-02-1

COCKPIT SEATS FUNCTIONAL CHECK OF HORIZONTAL / VERTICAL MECHANICAL CONTROL CABLE ADJUSTMENT OF COCKPIT SEATS Skills :

0.10 MHrs

1 AF 200

252100-01-1

PASSENGER COMPARTMENT SEATS VISUAL CHECK OF SEAT TO FLOOR ATTACHMENT Skills :

17.00 MHrs

1 AF 200

252100-02-1

PASSENGER COMPARTMENT SEATS OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND BELT ATTACHMENTS Skills :

6.80 MHrs

1 AF 200

252100-03-1

PASSENGER COMPARTMENT SEATS VISUAL CHECK OF LOWER SEAT STRUCTURE, BAGGAGE RESTRAINT BAR, BACKREST AND BACKREST SUPPORT Skills :

34.00 MHrs

1 CA Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [1 / 12] ATA

: 25


25


Task Number

Zone

252200-01-1

200

Task Title

CABIN ATTENDANT SEATS

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

42 MO

N

AMM 252200-210-801

ALL

OP

I

42 MO

N

AMM 252200-210-802

ALL

OP

I

42 MO

N

AMM 252200-210-803

ALL

DI

I

24 MO

N

AMM 252344-210-802

ALL

VISUAL CHECK OF SEAT STRUCTURE Skills :

1.00 MHrs

1 AF 200

252200-02-1

CABIN ATTENDANT SEATS VISUAL CHECK OF SEAT ATTACHMENT POINTS Skills :

0.50 MHrs

1 AF 200

252200-03-1

CABIN ATTENDANT SEATS OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND BELT ATTACHMENTS Skills :

0.20 MHrs

1 AF 200

252331-01-1

LININGS AND FURNISHINGS (DADO PANELS) \ETAILED INSPECTION OF LOWER SIDE WALL PANEL AND OF AREA BEHIND LOWER SIDE WALL PANEL FOR FOREIGN MATERIAL ACCUMULATION. NOTE : -ON LOWER SIDE WALL PANEL IN FWD MID AND AFT PASSENGER CAB SHOULD BE REMOVED IN ORDER TO ASSESS THE NEED FOR MORE EXTENSIVE PANEL REMOVAL -ALTERNATE SIDEWALL IS RECOMENDED AT NEXT INSPECTION Skills :

0.30 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [2 / 12] ATA

: 25


25


Task Number

Zone

252344-01-1

200

Task Title

LININGS AND FURNISHINGS (DADO PANELS)

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 4C

N

AMM 256800-710-803

ALL

GVI

I

24 MO

N

AMM 256800-210-802

ALL

DIS

I

1 400 FH

N

AMM 253000-920-802

ALL

CLN

I

1 400 FH

N

AMM 253400/7 AMT 253400-160-801

ALL

OPERATIONAL CHECK OF CABIN DECOMPRESSION PANELS OPENING Skills :

0.80 MHrs

1 AF 200

252344-02-1

LININGS AND FURNISHINGS (DADO PANELS) VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS IN CABIN ARE CLOSED Skills :

0.15 MHrs

1 AF 200

253000-01-1

BUFFET AND GALLEY DISCARD GALLEY AIR EXTRACTION FILTER ELEMENT Skills :

0.80 MHrs

1 AF 100

253400-01-1

GALLEY COOLING CLEAN CONDENSER AIR FILTER OF AIR CHILLER UNIT (IF GALLEY COOLING INSTALLED) NOTE: IF AIR CHILLER SYSTEM INSTALLED Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [3 / 12] ATA

: 25


25


Task Number

Zone

253400-04-1

100

Task code

Task Title

GALLEY COOLING CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" FILTERS/ RILLES IN THE GALLEY CABINET. NOTE: IF AIR CHILLER SYSTEM AND GALLEY WITH GRILLES

Threshold Interval

References

Ctrl

Eff

SER

I

1 400 FH

N

AMM 253400-160-806

ALL

OP

I

1 000 FH See note

N

AMM 254000/5 AMT 254000-710-802 FAD 74-08-09

ALL

GVI

I

1 000 FH See note

N

AMM 254000-220-801 FAD 74-08-09

ALL

INSTALLED

Skills :

0.00 MHrs

1 CA 200

254000-01-1

LAVATORIES OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP NOTE: 1000 FH INTERVAL FOR OPERATORS FLYING UNDER FAA REGULATIONS AS PER FAA AD 74-08-09 Skills :

0.10 MHrs

1 AF 200

254000-02-1

LAVATORIES VISUAL CHECK OF WASTE COMPARTMENT FOR FIRE CONTAINMENT CAPABILITY NOTE: 1000 FH INTERVAL FOR OPERATORS FLYING UNDER FAA REGULATIONS AS PER FAA AD 74-08-09 Skills :

0.20 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [4 / 12] ATA

: 25


R

25


Task Number

Zone

255100-01-1

130 150

Task Title

LOWER DECK CARGO LOADING SYSTEM

Task code

OP

Threshold Interval

Check : 1C

References

Ctrl

N

AMM 255100-710-803

Eff 275 294

OPERATIONAL CHECK OF POWER DRIVE UNITS

299 366 943 946 962 1019

Access panels :

821

822

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF R

130 150

255100-02-1


DI

I

34 000 FH

N

AMM 255100-210-801

275 294

REMOVE XZ-LATCHES FOR DETAILED INSPECTION

299 366 943 946 962 1019

Access panels :

821

822

Total access time :

0.04 Hrs

Skills :

0.60 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [5 / 12] ATA

: 25


25


Task Number

Zone

255100-03-2

150

Task Title


Task code

VCK

Threshold Interval

I

34 000 FH

References

Ctrl

N

AMM 255100-210-802

Eff 275 294

REMOVE CREW REST ROOM CONTAINER LATCHES AT FR 53.7 FOR DETAILED INSPECTION PREP. : LDMCR;

299 366

Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AF R

130 150

255100-08-1

LOWER DECK CARGO LOADING SYSTEM DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR WEAR AND DAMAGE (NOTE 11).

GVI

I

300 CY

N

AMM 255100/6 AMT 255100-210-809

275 294 299 366 943 946 962 1019

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [6 / 12] ATA

: 25


R

25


Task Number

Zone

255100-10-1

130 150

Task Title


Task code

GVI

Threshold Interval

I

3 200 FH

References

Ctrl

N

AMM 255100-210-816

Eff 275 294

GENERAL VISUAL INSPECTION OF POWER DRIVE UNITS NOTE 11

299 366 943 946 962 1019

Skills :

0.40 MHrs

1 AF R

130 150

255100-19-1


OP

I

36 MO

N

AMM 255100-200-802

275 294

OPERATIONAL CHECK OF BRAKING ROLLER.

299 366 943 946 962 1019

Skills :

0.20 MHrs

1 AF 130 150

255101-01-1

Issue No

:

Date

:

10 01/12/2013

ADVANCED LOWER DECK CARGO LOADING SYSTEM

OP

Check : 4C

N

AMM 255100-200-804

1266

OPERATIONAL CHECK OF SWIVEL NOSE AT XZ-LATCHES EG (ENTRANCE GUIDE) AND SWIVEL NOSES AT OVERRIDEABLE CENTER LATCHES. (NOTE 11)

Amendment No Date

: 01 : 06/09/2014

1256

Page : SYS - 25 [7 / 12] ATA

: 25


25


Task Number

Zone

255101-02-1

130 150


130 150


130 150


130 150


130

LOWER DECK FORWARD CARGO COMPARTMENT

255101-04-1

255101-08-1

255101-10-1

255200-01-1

Task Title

Task code

RAI

Threshold Interval

I

34 000 FH

References

Ctrl

N

AMM 255100-210-813

OP

I

36 MO

N

AMM 255100-200-805

OP

DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR WEAR AND DAMAGE. (NOTE 11) GVI

I

1 500 CY

I

18 MO

I

3 200 FH

N

AMM 255100-210-811

:

Date

:

10 01/12/2013

N

AMM 255100-210-810

Date

GVI

I

7 DY

Check : WY

N

AMM 255200-210-801 CMP 25-2-0000-002

0.35 MHrs

: 01 : 06/09/2014

1256 1266

GENERAL VISUAL INSPECTION OF XZ LATCHES (NOTE 11)

Amendment No

1256 1266

Skills :

Issue No

1256 1266

OPERATIONAL CHECK OF BRAKING ROLLER AND SWIVEL CASTER. (NOTE 11)

1 AF

1256 1266

REMOVE XZ-LATCHES FOR DETAILED INSPECTION.

VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS, PROTECTION PLATES, DECOMPRESSION PANELS, CENTER LINE COVER PLATES AND ACCESS DOORS

Eff

Page : SYS - 25 [8 / 12] ATA

: 25

ALL


25


Task Number

Zone

255200-03-1

130

Task Title


Task code

GVI

Threshold Interval

I

800 FH

References

Ctrl

Eff

N

AMM 255200-210-802

ALL

N

AMM 255200-210-803

1256

Check : 1A

VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE ROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY. (NOTE 11) Access panels :

132UC Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 130

255200-06-1


VCK

150

LOWER DECK AFT CARGO COMPARTMENT VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS, PROTECTION PLATES, DECOMPRESSION PANELS, CENTER LINE COVER PLATES AND ACCESS DOORS NOTE: CREW REST ROOM (UNDERFLOOR) AND/OR ACTS NOT TO BE REMOVED IF INSTALLED

800 FH

1266

Check : 1A

VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY. 255300-01-1

I

GVI

I

8 DY

Check : WY

N

AMM 255300-210-801 CMP 25-2-0000-002

Skills :

0.75 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [9 / 12] ATA

: 25

ALL


25


Task Number

Zone

255300-03-1

150

Task Title


Task code

GVI

Threshold Interval

I

800 FH

References

Ctrl

Eff

N

AMM 255300-210-804

ALL

N

AMM 255300-210-805

1256

Check : 1A

VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE ROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY. (NOTE 11) Access panels :

152UC Total access time :

0.00 Hrs

Skills :

0.80 MHrs

1 AF 150

255300-06-1

LOWER DECK AFT CARGO COMPARTMENT

VCK

160

LOWER DECK BULK CARGO COMPARTMENT

800 FH

1266

Check : 1A

VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY. 255400-01-1

I

VCK

I

8 DY

N

AMM 255400-210-801

ALL

N

AMM 255400-210-804

ALL

Check : WY

VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS AND ACCESS DOOR AT C73 Skills :

0.75 MHrs

1 AF 160

255400-04-1


DI

Check : 1C

DETAILED INSPECTION OF DIVIDER NETS, NET ATTACHMENT POINTS, NET CONNECTING DEVICES AND TENSION BUCKLES. Skills :

0.50 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [10 / 12] ATA

: 25


25


Task Number

Zone

255400-05-1

160

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

DI

Check : 1C

N

AMM 255400-210-805

ALL

DI

Check : 1C

N

AMM 255400-210-806

ALL

DI

I

6 YE

N

AMM 256141-200-801

ALL

OP

I

24 MO

N

AMM 256500-710-803

ALL

DETAILED INSPECTION OF NET SCREENS, NET SCREEN ATTACHMENT POINTS AND TENSION BUCKLES. 160

255400-06-1

LOWER DECK BULK CARGO COMPARTMENT DETAILED INSPECTION OF SCREEN DECOMPRESSION TARPAULINS. Skills :

0.20 MHrs

1 AF 211 212

256141-01-1

COCKPIT ESCAPE FACILITIES DETAILED INSPECTION OF EMERGENCY ESCAPE ROPE AND ROPE ATTACHMENT. Access panels :

211HC

212HC

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF 200

256535-01-1

EMERGENCY LOCATOR TRANSMITTER OPERATIONAL CHECK OF AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) SYSTEM BY MANUAL ACTIVATION. NOTE: IF ELT INSTALLED Skills :

0.04 MHrs

2 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [11 / 12] ATA

: 25


25


Task Number

Zone

256551-02-1

100

Task Title

Task code

OP

MEGAPHONE

Threshold Interval

Check : 1C

References

Ctrl

N

AMM 256551-710-801

OPERATIONAL CHECK OF MEGAPHONE Skills :

0.06 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 25 [12 / 12] ATA

: 25

Eff ALL


26

FIRE PROTECTION

Task Number

Zone

261500-02-1

130

Task Title

Task code

Threshold Interval

AVIONICS COMPARTMENT SMOKE DETECTION

REM

I

OP

I

OP

References

Ctrl

Eff

42 MO

N

AMM 261500-100-801

ALL

3 200 FH See note Check : 4A

N

AMM 261600/5 AMT 261600-710-803

ALL

I

N

AMM 261800-710-810

943

REMOVE AVIONICS SMOKE DETECTION PICCOLO TUBES FOR CLEANING NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

131EF

132EF

Total access time :

0.52 Hrs

Skills :

1.50 MHrs

1 AV 210

261600-01-1

LOWER DECK CARGO COMPT AND AVIONIC COMPT OPERATIONAL CHECK OF LOWER DECK CARGO COMPARTMENT AND AVIONICS COMPARTMENT SMOKE DETECTION BY PTT NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.20 MHrs

1 AV R

210

261800-12-1

AUXILIARY AREAS SMOKE DETECTION OPERATIONAL CHECK OF IFEC SMOKE DETECTION BY MCDU.

24 MO

946

Check : C1

962 1019 1256 1266

Skills :

3.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [1 / 8] ATA

: 26


R

26

FIRE PROTECTION

Task Number

Zone

261800-13-1

134

Task Title

AUXILIARY AREAS SMOKE DETECTION

Task code

OP

Threshold Interval

I

20 000 FH

References

Ctrl

N

AMM 261800-100-807

Eff 943 946

REMOVE IFEC PICCOLO TUBES FOR CLEANING

962 1019 1256 1266

Access panels :

132EG Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AV 210

262100-04-1

OP


I

800 FH

N

AMM 261200/6 AMT 261200-710-812

ALL

N

AMM 262100-710-809

ALL

Check : 1A

OPERATIONAL CHECK OF FIRE EXTINGUISHING SYSTEM NOTE: ETOPS PARALLEL SYSTEM Skills :

1.00 MHrs

1 AV 210 450 460

262100-11-1

OP


Check : 1C

OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER BOTTLE LOW PRESSURE INDICATING CIRCUIT Access panels :

453CL

453CR

Total access time :

463CL

463CR

0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [2 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262100-12-1

410 420

Task code

Task Title


Threshold Interval

References

Ctrl

Eff

FUC

I

12 000 FH

N

AMM 262100-720-819

ALL

FUC

I

48 MO

N

AMM 262100-710-810

ALL

FUNCTIONAL CHECK OF DISTRIBUTION PIPING FOR LEAKAGE AND OBSTRUCTION Access panels :

415AL 428AR

416AR 453CL

Total access time :

417AL 453CR

418AR 463CL

425AL 463CR

426AR

427AL

0.00 Hrs

Skills :

4.00 MHrs

1 AF 210 450 460

262100-13-1

ENGINE FIRE EXTINGUISHING FUNCTIONAL CHECK OF FIRING CIRCUIT CONTINUITY Access panels :

453CL

453CR

Total access time :

463CL

463CR

0.00 Hrs

Skills :

0.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [3 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262100-14-1

210 450 460

Task code

Task Title


Threshold Interval

References

Ctrl

Eff

OP

I

24 MO

N

AMM 262100-710-811 CMP 24-2-0000-006 CMP 36-2-0000-001

ALL

OP

I

800 FH

N

AMM 262200/5 AMT 262200-710-801 CMP 26-2-0000-001

ALL

N

AMM 262200-710-802

ALL

OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW FUNCTION NOTE : CMP TASK Access panels :

452CL

453CL

Total access time :

453CR 462CL 0.00 Hrs

463CL

463CR

Skills :

0.30 MHrs

1 AV 210

262200-01-3


Check : 1A

OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM NOTE : CMP TASK Skills :

0.10 MHrs

1 AV 310

262200-02-1

OP


I

42 MO

OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY Access panels :


0.00 Hrs

Skills :

0.40 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [4 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262200-03-2

310

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 2C

N

AMM 262200-710-806 CMP 26-2-0000-002

ALL

DI

I

N

AMM 262200-200-801

ALL

OP

Check : 1C

N

AMM 262200-710-804

ALL

OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT NOTE : CMP TASK Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AV 310

262200-04-1


14 000 FH

DETAILED INSPECTION OF DISTRIBUTION PIPING FOR CRACKS Access panels :

313AL

315AL

Total access time :

316AR 0.00 Hrs

Skills :

0.20 MHrs

1 AV 310

262200-05-1

APU FIRE EXTINGUISHING OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING TRIGGER CIRCUIT Skills :

0.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [5 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262200-06-1

210

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

I

42 MO

N

AMM 262200-710-805 CMP 28-2-0000-005

ALL

OP

I

4 800 FH

N

ALL

I

36 MO

AMM 262200-710-803 CMP 28-2-0000-004

I

12 000 FH

N

AMM 262300-710-801

ALL

OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION NOTE : CMP TASK Skills :

0.50 MHrs

1 AV 210 310

262200-07-3

APU FIRE EXTINGUISHING OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA MCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF, 6WF) NOTE : CMP TASK Skills :

0.40 MHrs

1 AV R

130

262300-01-1


OP

OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

132SW

821

Total access time :

0.02 Hrs

Skills :

0.50 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [6 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262300-02-1

130

Task Title


Task code

Threshold Interval

DIS

I

OP

DI

References

Ctrl

Eff

N

AMM 262300-920-802

ALL

Check : 1C

N

AMM 262300-710-802

ALL

I

N

AMM 262300-200-803

275

15 MO

DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

132SW

132WW

Total access time :

821 0.02 Hrs

Skills :

0.20 MHrs

1 AF 210

262300-03-1

LOWER DECK CARGO COMPARTMENT FIRE EXTING OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW PRESSURE INDICATION CIRCUIT BY PTT NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.05 MHrs

1 AV 130

262300-04-1


14 000 FH

294

DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND CHECK VALVE PREP. : CHECK VALVES; FILTERS;

299 366

Access panels :

132SW

821

Total access time :

831 0.02 Hrs

Skills :

0.10 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [7 / 8] ATA

: 26


26

FIRE PROTECTION

Task Number

Zone

262300-06-1

130

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

FUC

I

14 000 FH

N

AMM 262300-200-804

ALL

OP

I

1 000 FH

N

AMM 262400-210-801 AMM 262400/6

ALL

VCK

I

1 000 FH

N

AMM 262400-220-802

ALL

N

AMM 262500-280-803

ALL

CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

132SW

821

Total access time :

831 0.02 Hrs

Skills :

0.30 MHrs

1 AV 120 200

262400-04-1

PORTABLE FIRE EXTINGUISHER OPERATIONAL CHECK AND VISUAL CHECK OF PORTABLE FIRE EXTINGUISHER ATTACHMENT. Skills :

1.00 MHrs

1 AF 262400-09-1

262500-01-1

100 200


200


Check : 1A

VISUAL CHECK OF THE PORTABLE FIRE EXTINGUISHER PRESSURE GAUGE READING. OP

Check : 1C

CHECK PRESSURE OF EXTINGUISHING AGENT Skills :

0.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 26 [8 / 8] ATA

: 26


27


Task Number

Zone

271400-01-1

210

Task code

Task Title

OP

AILERON AND HYDRAULIC ACTUATION

Threshold Interval

I

12 000 FH

References

Ctrl

N

AMM 271400-740-802

Eff 275 294

OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY BITE

299 366

Skills :

0.20 MHrs

1 AF 575 675

271400-02-1


OP

I

34 000 FH

N

AMM 271400-210-801

ALL

FUC

I

30 000 FH

N

AMM 271400-200-801

ALL

OPERATIONAL CHECK OF AILERON SERVO CONTROL ACCUMULATOR PISTON POSITION. Access panels :

575AB

575CB

Total access time :

675AB 675CB 0.00 Hrs

Skills :

15.00 MHrs

1 AF 210 575 675

271400-03-1

AILERON AND HYDRAULIC ACTUATION CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND GENERAL CONDITION Access panels :

575AB 591DB 675CB 692BB

575BB 592AB 675DB 692CB

Total access time :

575CB 592BB 691AB 692DB

575DB 592CB 691BB

591AB 592DB 691CB

591BB 675AB 691DB

591CB 675BB 692AB

0.00 Hrs

Skills :

8.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [1 / 29] ATA

: 27


27


Task Number

Zone

271400-04-1

575 675

Task code

Task Title

LUB

AILERON AND HYDRAULIC ACTUATION LUBRICATION OF AILERON HINGE BEARINGS

Threshold Interval

I

7 500 FH

I

18 MO

I

7 500 FH

I

18 MO

References

Ctrl

Eff

N

AMM 122227-640-807

ALL

N

AMM 122227-640-811

ALL

Access panels :

575AB 591BB 675AB 691BB

575AT 591CB 675AT 691CB

Total access time :

575BB 591DB 675BB 691DB

575BT 592AB 675BT 692AB

575CB 592BB 675CB 692BB

575DB 592CB 675DB 692CB

591AB 592DB 691AB 692DB

0.00 Hrs

Skills :

0.40 MHrs

1 AF 575 675

271400-05-1

AILERON AND HYDRAULIC ACTUATION LUBRICATION OF AILERON SERVO CONTROL ROLLER BEARINGS

LUB

Access panels :

575AB

575CB

Total access time :

675AB

675CB

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [2 / 29] ATA

: 27


27


Task Number

Zone

272100-01-1

100 310

Task Title


Task code

Threshold Interval

LUB

Check : 4C

References

Ctrl

N

AMM 272100-210-801

Eff 275 294

DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL (EXCLUDING FIN) PREP. : CEILING PANELS Z130; CEILING PANELS Z150; CEILING PANELS Z160; FLOOR PANELS Z250;

299 366

Access panels :

132AZ

162ZW

Total access time :

311AZ 312AR 0.16 Hrs

Skills :

4.00 MHrs

1 AF R

325

272100-02-2

RUDDER MECHANICAL CONTROL DETAILED INSPECTION OF DUPLICATED CONTROL RODS OF RUDDER MECHANICAL CONTROL. NOTE: TASK APPLICABLE BEFORE: 272100-02-1

DI

I

20 000 FH

I

72 MO

N

AMM 272100-210-802

294 299 366

Access panels :

325DL

325ER

Total access time :

0.68 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : SYS - 27 [3 / 29] ATA

: 27


R

27


Task Number

Zone

272100-03-1

121

Task Title


Task code

Threshold Interval

LUB

Check : 2C

References

Ctrl

N

AMM 272100-200-801

Eff 275 294

CHECK POINTER OF CABLE TENSION REGULATOR WITHIN LIMITS

299 366

Skills :

0.30 MHrs

1 AF 325

272100-04-1


LUB

I

34 000 FH

N

AMM 272100-710-801

275 294

OPERATIONAL CHECK OF CENTERING MECHANISM

299 366

Access panels :

325AL

325BL

Total access time :

325CL 0.00 Hrs

Skills :

1.00 MHrs

1 AF 210

272100-05-1


LUB

I

20 MO

N

AMM 272143-600-801

LUBRICATION OF THE RUDDER PEDALS ADJUSTMENT MECHANISM Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [4 / 29] ATA

: 27

ALL


R

27


Task Number

Zone

272100-18-1

120 210

Task Title


Task code

DI

Threshold Interval

Check : 4C

References

Ctrl

N

AMM 272100-210-805

Eff 943 946

DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT

962 1019 1256 1266

Skills :

2.00 MHrs

1 AF R

210

272100-19-1


OP

I

24 000 FH

N

AMM 272200-710-806

943 946

OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY CHANNEL

962 1019 1256 1266

Skills :

0.20 MHrs

1 EL 210

272200-01-1


OP

Check : 4C

N

AMM 272200-710-801

294

OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL SPRING ROD

299 366

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : SYS - 27 [5 / 29] ATA

: 27


R

27


Task Number

Zone

272200-01-2

122

Task Title


Task code

OP

Threshold Interval

Check : 4C

References

Ctrl

N

AMM 272200-710-801

Eff 943 946

OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL SPRING ROD

962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF 210

272200-02-1


OP

I

20 000 FH

N

AMM 272200-710-803

275 294

OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL

299 366

Skills :

0.10 MHrs

1 AF 210

272300-01-1


OP

I

20 000 FH

N

AMM 272300-710-801

294

OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL LIMITATION UNITS STANDBY CHANNEL

299 366

Skills :

0.15 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : SYS - 27 [6 / 29] ATA

: 27


27


Task Number

Zone

272400-01-1

210

Task Title

Task code

FUC

RUDDER HYDRAULIC ACTUATION

325


I

800 FH

References

Ctrl

N

AMM 272400-710-801

Eff 275 294

Check : 1A

OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH INDIVIDUAL HYDRAULIC SYSTEMS

272400-03-1

Threshold Interval

299 366

FUC

I

FUC

Check : 2C

34 000 FH

N

AMM 272400-200-801

ALL

N

AMM 272400-710-803

275

CHECK RUDDER SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND GENERAL CONDITION Access panels :

325CR

325DR

Total access time :

325EL 325GR 0.00 Hrs

325JR

Skills :

2.00 MHrs

1 AF 210

272400-04-1


294

OPERATIONAL CHECK OF RUDDER SERVO CONTROL JAMMING DEVICE

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299 366

Page : SYS - 27 [7 / 29] ATA

: 27


27


Task Number

Zone

272400-06-1

325

Task Title


Task code

LUB

LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER BEARING (RUDDER SIDE)

Threshold Interval

I

7 500 FH

I

18 MO

I

7 500 FH

I

18 MO

References

Ctrl

Eff

N

AMM 122227-640-810

ALL

N

AMM 122255-600-802

ALL

Access panels :

325DL Total access time :

0.68 Hrs

Skills :

0.10 MHrs

1 AF 325

272400-07-1

RUDDER HYDRAULIC ACTUATION LUBRICATION OF RUDDER HINGE BEARING NO 6

LU

Access panels :

325PL Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 LU

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [8 / 29] ATA

: 27


27


Task Number

Zone

272651-01-1

310

Task code

Task Title

OPC

YAW DAMPER ACTUATION INSPECTION OF RUDDER YAW DAMPER SERVO-ACTUATOR (ACTIVE POSITION) FOR LEAKAGE (FIN 19CS1 AND 19CS2) NOTE: - THRESHOLD: TASK TO BE PERFORMED PRIOR TO ACCUMULATION OF 10000 AIRCRAFT FH OR, IF UNIT FH ARE RECORDED, PRIOR TO ACCUMULATION OF 10000 YAW DAMPER SERVO-ACTUATOR FH SINCE NEW - INTERVAL: REPEAT THE TASK EVERY 800FH OR, AS RECOMMENDED IN ISB 27-3124

Threshold Interval

T

10 000 FH

I

800 FH

References

Ctrl

N

AMM 272651-200-802

Eff 275 294 299 366

Skills :

1.50 MHrs

1 AF 210

273400-01-2

OP

ELEVATOR AND HYDRAULIC ACTUATION

I

12 000 FH

N

AMM 273400-740-802

275 294

OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY BITE

299 366

Skills :

0.10 MHrs

1 AF 210 330 340

273400-02-1

FUC


I

30 000 FH

N

AMM 273400-200-801

CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND GENERAL CONDITION Access panels :

334AB

334BB

Total access time :

334CB

344AB

344BB

344CB

0.00 Hrs

Skills :

4.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [9 / 29] ATA

: 27

ALL


27


Task Number

Zone

273400-03-1

330 340

Task code

Task Title


Threshold Interval

References

Ctrl

Eff

VCK

I

34 000 FH

N

AMM 273400-210-801

ALL

LUB

I

7 500 FH

N

AMM 122227-640-814

ALL

I

18 MO

OPERATIONAL CHECK OF ELEVATOR SERVO CONTROL ACCUMULATOR PISTON POSITION. Access panels :

334BB

334CB

Total access time :

344BB 344CB 0.00 Hrs

Skills :

11.00 MHrs

1 AF 330 340

273400-06-1

ELEVATOR AND HYDRAULIC ACTUATION LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING Access panels :

334AB

334BB

Total access time :

334CB 344AB 0.00 Hrs

344BB

344CB

Skills :

2.00 MHrs

1 LU

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [10 / 29] ATA

: 27


27


Task Number

Zone

274000-01-1

310

Task Title

TRIMMABLE HORIZONTAL STABILIZER (THS)

Task code

Threshold Interval

References

Ctrl

Eff

DI

I

12 000 FH

N

AMM 274400-210-801

ALL

LUB

I

36 MO

N

AMM 122227-640-802

ALL

DETAILED INSPECTION OF FOLLOWING ITEMS OF TRIMMABLE HORIZONTAL STABILIZER ACTUATOR: - FAIL SAFE NUT - UPPER AND LOWER ATTACHMENTS ( PRIMARY AND SECONDARY) - NO-BACK HOUSING Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AF 120 310

274100-01-1

TRIMMABLE HORIZONTAL STABILIZER (THS) LUBRICATION OF THS MECHANICAL CONTROL CHAINS Access panels :

312AR

811

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [11 / 29] ATA

: 27


27


Task Number

Zone

274100-02-1

100 210 310

Task code

Task Title

DI


Threshold Interval

References

Ctrl

Eff

Check : 4C

N

AMM 274100-210-801

ALL

I

N

AMM 274100-220-802

ALL

DETAILED INSPECTION OF THS MECHANICAL CONTROL LOOP PREP. : FLOOR PANELS Z250; SEATS AND FURNISHINGS Z250; Access panels :

131BC 131VC 151PC 251QG

131FC 132AZ 161BC 251YF

Total access time :

131KC 151BC 161EC 312AR

131MC 151DC 251DG

131PC 151FC 251JG

131RC 151HC 251KG

131TC 151KC 251NF

0.00 Hrs

Skills :

0.40 MHrs

1 AF 310

274100-04-1


FUC

42 MO

FUNCTIONAL CHECK OF MOVABLE INDEX ON THS CABLE TENSION COMPENSATOR SCALE WITHIN LIMITS. Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [12 / 29] ATA

: 27


27


Task Number

Zone

274400-03-1

310

Task Title


Task code

Threshold Interval

SER

I

FUC

References

Ctrl

Eff

N

AMM 274451-210-801

ALL

Check : 4C

N

AMM 274454-720-801

ALL

I

N

AMM 274451-210-802

ALL

4 800 FH

CHECK OIL LEVEL OF THS ACTUATOR GEARBOX Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF 310

274400-04-1

TRIMMABLE HORIZONTAL STABILIZER (THS) FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE-OFF BRAKE (CHECK OF STATIC TORQUE) Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AF 310

274400-05-1


DI

12 000 FH

CHECK MAGNETIC CHIP DETECTOR OF THS ACTUATOR GEARBOX Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [13 / 29] ATA

: 27


27


Task Number

Zone

274400-06-1

310

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

VCK

I

15 000 FH

N

AMM 274451-220-802

ALL

OP

I

34 000 FH

N

AMM 274400-710-803

ALL

FUC

I

16 000 FH

N

AMM 274451-220-801

ALL

DETAILED INSPECTION OF WEAR INDICATOR OF THS ACTUATOR NO-BACK SYSTEM. Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF R

310

274400-07-1

TRIMMABLE HORIZONTAL STABILIZER (THS) OPERATIONAL CHECK OF THS ACTUATOR NO-BACK SYSTEM Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AF 310

274400-08-1

TRIMMABLE HORIZONTAL STABILIZER (THS) CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT (PRIMARY AND SECONDARY LOAD PATH). Access panels :


0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [14 / 29] ATA

: 27


27


Task Number

Zone

274400-10-1

310

Task Title


Task code

VCK

Threshold Interval

I

1 600 FH

Eff

N

AMM 274400/6 AMT 274400-210-803

ALL

N

AMM 121327-612-802

ALL

Check : 2A

VISUAL CHECK OF THS ACTUATOR DRAIN COLLECTING CONTAINER ASSEMBLY INCLUDING HOSES AND OIL LEVEL.

References

Ctrl

Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF R

148

275100-01-1

SER

FLAPS

I

18 MO

TOP UP PCU TO CONFIRM FLUID LEVEL Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [15 / 29] ATA

: 27


27


Task Number

Zone

275400-01-1

500 600

Task code

Task Title

SER

FLAPS

Threshold Interval

I

60 MO

References

Ctrl

N

AMM 121327-612-804

DRAIN AND REFILL ROTARY ACTUATOR WITH SEMI-FLUID PREP. : MOVABLE FLAP TRACK FAIRING Z531; MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; MOVABLE FLAP TRACK FAIRING Z631; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634; Access panels :

531AB 531FL 532DB 533CL 534AT 534FR 631EB 632CR 633EB 634AB 634FL

531AT 531FR 532EB 533CR 534CB 631AB 631FL 632DB 633EL 634AT 634FR

Total access time :

531CB 532AB 532FL 533DB 534CL 631AT 631FR 632EB 633ER 634CB 734 0.00 Hrs

531CL 532AT 532FR 533EB 534CR 631CB 632AB 632FL 633GB 634CL 744

531CR 532CB 533AB 533FL 534DB 631CL 632AT 632FR 633HB 634CR

531DB 532CL 533AT 533FR 534EB 631CR 632CB 633AB 633HL 634DB

531EB 532CR 533CB 534AB 534FL 631DB 632CL 633AT 633HR 634EB

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [16 / 29] ATA

: 27

Eff ALL


27


Task Number

Zone

275400-02-1

140 500 600

Task code

Task Title

FLAPS

Threshold Interval

References

Ctrl

Eff

DI

I

60 MO

N

AMM 275400-200-801

ALL

DI

I

60 MO

N

AMM 275400-200-802

ALL

DETAILED INSPECTION OF TRANSMISSION ASSY Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 140 500 600

275400-03-1

FLAPS DETAILED INSPECTION OF CRUISE ROLLERS, FLAP TRACKS AND CARRIAGES, ROTARY ACTUATORS AND ATTACHMENTS PREP. : FLAPS EXTENDED; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z531; MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z631; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634; Access panels :

147AB 198AT

147BB 573BB

Total access time :

147BT 734

148AB 744

148BB

148BT

197AT

0.20 Hrs

Skills :

3.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [17 / 29] ATA

: 27


R

27


Task Number

Zone

275400-04-1

500 600

Task Title

Task code

LUB

FLAPS

Threshold Interval

I

3 200 FH

References

Ctrl

N

AMM 122227-640-803

275 294

Check : 4A

LUBRICATION OF FLAP TRACK/ CARRIAGE ROLLER BEARINGS

Eff

299 366 943 962 1019 1256 1266

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 580 680

275400-05-1

DI

FLAPS

I

60 MO

N

AMM 275100-200-801

DETAILED INSPECTION OF INTERCONNECTION STRUT AND ATTACHMENTS Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [18 / 29] ATA

: 27

ALL


27


Task Number

Zone

275400-06-1

500 600

Task Title

FLAPS

Task code

Threshold Interval

References

Ctrl

Eff

SER

I

36 MO

N

AMM 275400-210-802

ALL

LUB

I

18 MO

N

AMM 122227-640-806

ALL

CHK

I

18 MO

N

AMM 275400-280-801 SIL 27-142

ALL

TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF 570 670

275400-08-1

FLAPS LUBRICATION OF STEADY BEARINGS PREP. : FLAPS EXTENDED; Skills :

0.60 MHrs

1 AF 140 530 630

275400-09-1

FLAPS ACTUATION CHECK THE TORQUE OF FLAP TRACK CARRIAGES Z- ROLLERS Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

4.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [19 / 29] ATA

: 27


R

27


Task Number

Zone

275400-10-1

530 630

Task code

Task Title

CHK

FLAPS DETAILED INSPECTION OF FLAP TRACK AFT LINK BEARING BALL AT FLAP TRACK 2, 3 AND 4 PREP. : MOVABLE FLAP TRACK FAIRING Z531; MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z631; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; REAR LINKS Z500; REAR LINKS Z600;

Threshold Interval

References

Ctrl

N

AMM 275400-200-804

531AT 531FR 532EB 533CR 534CB 631AB 631FL 632DB 633EL 634AT 634FR

Total access time :

531CB 532AB 532FL 533DB 534CL 631AT 631FR 632EB 633ER 634CB 734 0.00 Hrs

531CL 532AT 532FR 533EB 534CR 631CB 632AB 632FL 633GB 634CL 744

531CR 532CB 533AB 533FL 534DB 631CL 632AT 632FR 633HB 634CR

531DB 532CL 533AT 533FR 534EB 631CR 632CB 633AB 633HL 634DB

3 400 FC

T

36 MO

294

I

18 MO

299 366 943 946 962 1019

531EB 532CR 533CB 534AB 534FL 631DB 632CL 633AT 633HR 634EB

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Access panels :

531AB 531FL 532DB 533CL 534AT 534FR 631EB 632CR 633EB 634AB 634FL

Eff

Page : SYS - 27 [20 / 29] ATA

: 27


27


Task Number

Zone

275400-14-1

210 574 674

Task Title

FLAPS

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

6 400 FH

N

AMM 275100-710-801

ALL

DI

T

48 MO

N

ALL

I

24 MO

AMM 275400-220-803 SIL 57-112

T

48 MO

N

24 MO

AMM 275400-720-801 SIL 57-112

ALL

I

OPERATIONAL CHECK OF FLAP WTB/POB PERFOMANCE TEST. Skills :

2.00 MHrs

2 AF 275400-15-1

275400-16-1

Issue No

:

Date

:

147 148 531 532 533 534 631 632 633 634

FLAPS

147 148 531 532 533 534 631 632 633 634

FLAPS

10 01/12/2013

DETAILED INSPECTION OF FLAP TRACKS (1-5) AND CARRIAGE ROLLERS.

FUC

FUNCTIONAL CHECK OF FLAP TRACK (1-5) CARRIAGES ROLLERS FOR PLAY.

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [21 / 29] ATA

: 27


27


Task Number

Zone

275500-01-1

533 633

Task Title

FLAPS

Task code

Threshold Interval

References

Ctrl

Eff

DI

I

60 MO

N

AMM 275100-200-802

ALL

LUB

I

18 MO

N

AMM 122227-640-805

ALL

DETAILED INSPECTION OF TRACK 4 SENSORS Skills :

0.20 MHrs

1 AF 580 680

276400-01-1

SPOILER HYDRAULIC ACTUTION LUBRICATION OF ALL SPOILER LINKAGE BEARINGS PROVIDED WITH GREASE NIPPLES Skills :

2.00 MHrs

1 AF 210 580 680

276400-02-1

SPOILER HYDRAULIC ACTUATION

DI

Check : 4C

N

AMM 276400-200-801

ALL

OP

I

N

AMM 276400-710-803 ISB 27-3195

ALL

DETAILED INSPECTION OF LINKAGE AND ATTACHMENT OF SPOILERS 1 TO 6 PREP. : FLAPS EXTENDED; SLATS EXTENDED; SPOILERS EXTENDED; Skills :

2.40 MHrs

1 AF 210 580 680

276400-03-1

Issue No

:

Date

:

10 01/12/2013

SPOILER HYDRAULIC ACTUATION OPERATIONAL CHECK OF SPOILER SERVOCONTROL HYDRAULIC LOCKING FUNCTION. PREP. : FLAPS EXTENDED;

Amendment No Date

: 01 : 06/09/2014

48 MO

Page : SYS - 27 [22 / 29] ATA

: 27


27


Task Number

Zone

278000-01-1

510 610

Task code

Task Title

LUB

LIFT AUGMENTING (SLATS)

Threshold Interval

I

2 800 FH

References

Ctrl

N

AMM 122227-640-804

LUBRICATION OF ALL SLAT TRACK ROLLER BEARINGS, PINION BEARINGS, PINION AND RACK TEETH AND SLAT TRACK 2 AND 3 LEVER BEARINGS Access panels :

521BB 522LB 523JB 622CB 623CB

521DB 522NB 523LB 622FB 623EB

Total access time :

521GB 522RB 523NB 622JB 623GB 0.00 Hrs

521JB 522TB 621BB 622LB 623JB

522CB 523CB 621DB 622NB 623LB

522FB 523EB 621GB 622RB 623NB

522JB 523GB 621JB 622TB

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [23 / 29] ATA

: 27

Eff ALL


27


Task Number

Zone

278000-02-1

500 600

Task code

Task Title

DI


Threshold Interval

References

Ctrl

Eff

Check : 4C

N

AMM 278400-210-801

ALL

I

N

AMM 121327-612-803

ALL

DETAILED INSPECTION OF SLAT TRANSMISSION ASSY, SLAT TRACKS AND ROLLERS, PINIONS AND CURVED RACK GEARS Access panels :

193DB 521GB 522JB 523EB 621CB 622CB 622TB 623NB

195AB 521JB 522LB 523GB 621DB 622FB 622UB

Total access time :

521AB 522AB 522NB 523JB 621FB 622HB 623CB

521BB 522BB 522RB 523LB 621GB 622JB 623EB

521CB 522CB 522TB 523NB 621JB 622LB 623GB

521DB 522FB 522UB 621AB 622AB 622NB 623JB

521FB 522HB 523CB 621BB 622BB 622RB 623LB

0.00 Hrs

Skills :

3.00 MHrs

1 AF R

190

278000-03-1

SER

LIFT AUGMENTING (SLATS

18 MO

TOP UP PCU GEARBOX TO CONFIRM FLUID LEVEL Access panels :

195AB Total access time :

0.00 Hrs

Skills :

0.25 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [24 / 29] ATA

: 27


27


Task Number

Zone

278000-04-2

190

Task code

Task Title


Threshold Interval

SER

I

LUB

LUB

References

Ctrl

Eff

N

AMM 278400-210-802

ALL

Check : 4C

N

AMM 122227-640-808

ALL

I

N

AMM 122227-640-813

ALL

36 MO

TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL ACCESS: 193FB 278000-05-1

278000-06-1

500 600


190 500 600


LUBRICATION OF SLAT ROTARY ACTUATORS TYPE A (TRACK 2-3) PREP. : SLATS EXTENDED; 18 MO

LUBRICATION OF STEADY BEARINGS PREP. : SLATS EXTENDED; Access panels :

193DB 622AB

521BB 622BB

Total access time :

522AB 622HB

522BB 623CB

522HB

523CB

621BB

0.20 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [25 / 29] ATA

: 27


27


Task Number

Zone

278000-07-1

520 620

Task Title


Task code

Threshold Interval

LUB

Check : 4C

N

AMM 122227-640-815

ALL

OP

I

6 400 FH

N

AMM 278100-710-801

ALL

OP

I

12 000 FH

N

AMM 279600-710-801

ALL

References

Ctrl

Eff

LUBRICATION OF SLAT ROTARY ACTUATOR TYPE B TRACK 5-16) PREP. : FLAPS EXTENDED SLATS EXTENDED Access panels :

522CB 523EB 622LB 623JB

522JB 523GB 622NB 623LB

Total access time :

522LB 523JB 622RB 623NB

522NB 523LB 622TB

522RB 523NB 623CB

522TB 622CB 623EB

523CB 622JB 623GB

0.20 Hrs

Skills :

2.00 MHrs

1 AF 210 523 623

278000-10-1

LIFT AUGMENTING (SLATS) OPERATIONAL CHECK OF SLAT WTB/POB PERFOMANCE TEST. PREP. : SLATS EXTENDED; Skills :

3.00 MHrs

2 AF 210

279000-01-1

ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) OPERATIONAL CHECK OF FCPCS AND FCSCS AILERON SERVO LOOPS Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [26 / 29] ATA

: 27


27


Task Number

Zone

279000-02-1

210

Task Title

ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)

Task code

OP

Threshold Interval

I

12 000 FH

References

Ctrl

N

AMM 279600-710-802

Eff 275 294

OPERATIONAL CHECK OF FCPCS AND FCSCS AILERON SERVO LOC

299 366

Skills :

0.20 MHrs

1 AF 210

279000-04-1

ELECTRICAL FLIGHT CONTROL SYSTEM

OP

I

N

AMM 279600-710-804

ALL

OP

Check : 1C

N

AMM 279600-710-805

ALL

OP

Check : 4C

N

AMM 279600-710-808

275

12 000 FH

OPERATIONAL CHECK OF TAKEOVER AND PRIORITY FUNCTION Skills :

0.40 MHrs

1 AF 210

279000-06-1

ELECTRICAL FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF FCPC1 AND FCSC1 POWER SUPPLY Skills :

0.40 MHrs

1 AF 210

279000-08-1


294

OPERATIONAL CHECK OF RETURN TO LOW SPEED CONFIGURATION OF RUDDER AND PEDAL TRAVEL LIMITATION UNITS

299 366

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [27 / 29] ATA

: 27


27


Task Number

Zone

279000-09-1

210

Task Title


Task code

OP

Threshold Interval

Check : 1C

References

Ctrl

N

AMM 279600-710-819

Eff 275 294

OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2

299 366

Skills :

0.10 MHrs

1 EL 120 210

279000-11-1


OP

Check : 1C

N

AMM 279600-710-814

ALL

OP

I

N

AMM 279900-740-801

943

OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY Skills :

0.65 MHrs

1 EL R

210

279000-14-2


5 000 FH

946

OPERATIONAL CHECK OF THE BACK UP CONTROL MODULE AND BACK UP POWER SUPPLY (BCM/BPS)

962 1019 1256 1266

R

210

279000-15-1


OP

I

12 000 FH

N

AMM 279600-710-817

943 946

OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP

962 1019 1256 1266

Skills :

0.40 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [28 / 29] ATA

: 27


R

27


Task Number

Zone

279000-16-1

210

Task Title


Task code

OP

Threshold Interval

I

5 000 FH

References

Ctrl

N

AMM 279900-710-801

Eff 943 946

OPERATIONAL CHECK RUDDER ELECTRICAL BACK UP

962 1019 1256 1266

210

279000-19-1


OP

Check : 1C

N

AMM 279600-710-813

275 294

OPERATIONAL CHECK OF POWER SUPPLY OF THE RTA2, RTLU AND PTLU MOTOR 2

299 366

Skills :

0.30 MHrs

1 EL R

210

279000-20-1


OP

Check : 1C

N

AMM 279600-710-820

943 946

OPERATIONAL CHECK OF PFTU-TRIM 2 NORMAL/BACK-UP POWER SUPPLY

962 1019 1256 1266

Skills :

0.30 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 27 [29 / 29] ATA

: 27


28

FUEL

Task Number

Zone

281100-02-1

330 340

Task Title

Task code

OP

TANKS

Threshold Interval

I

2 MO

Eff

N

AMM 123228/3 AMT 123228-281-803 CMP 28-2-0000-010

ALL

See note

OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER FROM TRIM TANK AND TRIM VENT SURGE TANK NOTE: CMP TASK

References

Ctrl

Skills :

0.30 MHrs

1 AF 210

281100-05-1

TANKS

OP

I

18 MO

N

AMM 281100-710-801

ALL

OP

I

6 YE

N

AMM 281100-710-802

ALL

OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, USING INDIVIDUAL MOTORS, TO PROVE CORRECT ACTUATOR OPERATION AND COCKPIT INDICATION Skills :

0.05 MHrs

1 AF 210

281100-06-1

TANKS OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE TO PROVE THAT NEITHER VALVE HAS JAMMED IN THE OPEN POSITION AND TO VERIFY CORRECT OPERATION OF THE P/BSW Skills :

0.05 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [1 / 17] ATA

: 28


28

FUEL

Task Number

Zone

281100-07-1

540 640

Task Title

TANKS

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 8C

N

AMM 281100-710-805

ALL

OP

Check : 8C

N

AMM 281100-710-806

ALL

OPERATIONAL CHECK OF STANDBY FUEL CELL CLACK VALVES TO ENSURE FULL AND FREE MOVEMENT PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

541BB

641BB

Total access time :

0.00 Hrs

Skills :

0.66 MHrs

1 AF 540 640

281100-09-1

TANKS OPERATIONAL CHECK OF ALL COLLECTOR CELL CLACK VALVES TO ENSURE FULL AND FREE MOVEMENT PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

541BB

641BB

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [2 / 17] ATA

: 28


28

FUEL

Task Number

Zone

281100-10-1

190 500 600

Task Title

Task code

OP

TANKS

Threshold Interval

I

7 DY

Eff

N

AMM 123228-281-810 CMP 28-2-0000-013

ALL

N

AMM 123228/3 AMT 123228-281-812 SIL 28-079

ALL

N

AMM 281200-210-803

ALL

See note

OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS NOTE : CMP TASK

References

Ctrl

Check : WY

Access panels :

191RB

192RB

Total access time :

0.08 Hrs

Skills :

1.80 MHrs

1 AF 190 300 500 600

281100-15-1

TANKS

SER

I

VCK

Check : 2C

SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION ANALYSIS NOTE : INTERVAL DEPENDING ON EACH INDIVIDUAL OPERATOR´S ENVIRONMENT

1 600 FH See note

Access panels :

191RB

192RB

Total access time :

0.08 Hrs

Skills :

1.60 MHrs

1 AF 346 550 650

281200-01-1

TANK VENTING SYSTEM VISUAL CHECK OF THE APERTURE LEADING TO WING AND TRIM SURGE TANK FLAME ARRESTORS (INSIDE THE NACA INTAKES) FOR BLOCKAGE Skills :

0.12 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [3 / 17] ATA

: 28


28

FUEL

Task Number

Zone

281200-02-1

346 550 650

Task Title

Task code

VCK

TANK VENTING SYSTEM VISUAL CHECK OF THE WING AND TRIM VENT SURGE TANK OVERPRESSURE PROTECTORS (BURST DISCS) FOR INTEGRITY

Threshold Interval

Ctrl

See note

N

References

AMM 281200-210-802

Check : 1C

Skills :

0.06 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [4 / 17] ATA

: 28

Eff ALL


28

FUEL

Task Number

Zone

281800-01-1

140 300 500 600

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

DVI

Check : 8C

References

Ctrl

N

AMM 281800-200-801

DETAILED INSPECTION OF THE WING AND TRIM TANK BONDING LEADS. (SFAR88) PREP. : FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634; Access panels :

147AZ 333BB 343BB 541AZ 541EB 541JB 541RB 542FB 550CB 641BZ 641FB 641LB 642AB 642HB 650EB

148AZ 333CB 343CB 541BB 541EZ 541KB 541SB 542GB 550DB 641CB 641FZ 641MB 642BB 642JB 650FB

Total access time :

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

319AL 333DB 343DB 541BZ 541FB 541LB 542AB 542HB 550EB 641CZ 641GB 641NB 642CB 642KB

319AR 333EB 343EB 541CB 541FZ 541MB 542BB 542JB 550FB 641DB 641GZ 641PB 642DB 650AB

319BL 333FB 343FB 541CZ 541GB 541NB 542CB 542KB 641AB 641DZ 641HB 641QB 642EB 650BB

319DR 333GB 343GB 541DB 541GZ 541PB 542DB 550AB 641AZ 641EB 641JB 641RB 642FB 650CB

333AL 343AR 541AB 541DZ 541HB 541QB 542EB 550BB 641BB 641EZ 641KB 641SB 642GB 650DB

0.00 Hrs

: 01 : 06/09/2014

Page : SYS - 28 [5 / 17] ATA

: 28

Eff ALL

A330 AIRCRAFT MAINTENANCE PROGRAM CHAPTER : Task Number

28

FUEL Task Title

Zone

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

Eff

Skills :

10.00 MHrs

1 AV 140 300 500 600

281800-03-1

IGNITION PREVENTION

N

AMM 281851-210-801

GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS. (SFAR88)ANK. (SFAR88) PREP. : FUEL TANK DRAINED AND VENTED; Access panels :

147AZ 641AB

148AZ 641BB

Total access time :

312AR

319DR

319ER

541AB

541BB

0.00 Hrs

Skills :

2.00 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [6 / 17] ATA

: 28

ALL


28

FUEL

Task Number

Zone

281800-04-1

140 300 500 600

Issue No

:

Date

:

10 01/12/2013

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 281844-210-801

GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND PROBE ATTACHMENTS. (SFAR88) PREP. : FUEL TANK DRAINED AND VENTED; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED;

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [7 / 17] ATA

: 28

Eff ALL

A330 AIRCRAFT MAINTENANCE PROGRAM CHAPTER : Task Number

28

FUEL Task Title

Zone

Task code

Threshold Interval

GVI

Check : 4C

References

Ctrl

Eff

Access panels :

147AZ 333BB 343BB 541AZ 541EB 541JB 541RB 542FB 550CB 641BZ 641FB 641LB 642AB 642HB 650EB

148AZ 333CB 343CB 541BB 541EZ 541KB 541SB 542GB 550DB 641CB 641FZ 641MB 642BB 642JB 650FB

319AL 333DB 343DB 541BZ 541FB 541LB 542AB 542HB 550EB 641CZ 641GB 641NB 642CB 642KB

Total access time :

319AR 333EB 343EB 541CB 541FZ 541MB 542BB 542JB 550FB 641DB 641GZ 641PB 642DB 650AB

319BL 333FB 343FB 541CZ 541GB 541NB 542CB 542KB 641AB 641DZ 641HB 641QB 642EB 650BB

319DR 333GB 343GB 541DB 541GZ 541PB 542DB 550AB 641AZ 641EB 641JB 641RB 642FB 650CB

333AL 343AR 541AB 541DZ 541HB 541QB 542EB 550BB 641BB 641EZ 641KB 641SB 642GB 650DB

0.50 Hrs

Skills :

10.00 MHrs

1 AV 130

281800-06-1

IGNITION PREVENTION

N

AMM 281852-210-802

GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD CARGO BAY INSULATION MATS. (SFAR88) Access panels :

131BX

131CX

Total access time :

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

131DX 132CX 0.00 Hrs

: 01 : 06/09/2014

132DX

Page : SYS - 28 [8 / 17] ATA

: 28

ALL


28

FUEL

Task Number

Zone

281800-07-1

250

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 281842-210-801

GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE CENTER TANK. (SFAR88) PREP. : FLOOR COVERING Z250; FLOOR PANELS Z250; SEATS IN Z250; Skills :

0.50 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [9 / 17] ATA

: 28

Eff ALL


28

FUEL

Task Number

Zone

281800-08-1

500 600

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 281841-210-801

IGNITION PREVENTION GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS. (SFAR88) PREP. : FLAPS EXTENDED; SLATS EXTENDED; Access panels :

521AB 522AB 522HB 523EB 573FB 575CB 621GB 622CT 622UB 673CB 675BB

521BB 522AT 522JB 523GB 573GB 575DB 621JB 622EB 623CB 673DB 675BT

Total access time :

521CB 522BB 522LB 523JB 574AT 621AB 622AB 622HB 623EB 673FB 675CB 0.50 Hrs

521DB 522BT 522NB 523LB 575AB 621BB 622AT 622JB 623GB 673GB 675DB

521FB 522CB 522TB 523NB 575AT 621CB 622BB 622LB 623JB 674AT

521GB 522CT 522UB 573CB 575BB 621DB 622BT 622NB 623LB 675AB

521JB 522EB 523CB 573DB 575BT 621FB 622CB 622TB 623NB 675AT

Skills :

2.00 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [10 / 17] ATA

: 28

Eff ALL


28

FUEL

Task Number

Zone

281800-09-1

300

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 281841-210-802

ALL

GVI

Check : 8C

N

AMM 281843-210-801

ALL

References

Ctrl

Eff

IGNITION PREVENTION AV GENERAL VISUAL INSPECTION OF TRIM TANK EXTERNAL ELECTRICAL WIRING AND CONNECTIONS. (SFAR88) Access panels :

331BT 334CT 335CB 341ET 344DB 345BB

331CT 334DB 335DB 344AB 344DT 345CB

Total access time :

500 600

281800-10-1

331DT 334EB 335EB 344AT 344EB 345DB 0.00 Hrs

331ET 334FB 335FB 344BB 344ET 345EB

334AB 334GB 341BT 344BT 344FB 345FB

334BB 335AB 341CT 344CB 344GB

IGNITION PREVENTION

334CB 335BB 341DT 344CT 345AB

GENERAL VISUAL INSPECTION OF WING FUEL PUMP ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL SUPPLY CABLE. (SFAR88) PREP. : FUEL PUMP FAIRINGS Z500; FUEL PUMP FAIRINGS Z600; Skills :

0.20 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [11 / 17] ATA

: 28


28

FUEL

Task Number

Zone

282100-02-1

210

Task Title

MAIN FUEL PUMP SYSTEM

Task code

Threshold Interval

OP

I

OP

OP

References

Ctrl

Eff

N

AMM 282100-710-804

ALL

Check : 1C

N

AMM 282100-710-812

ALL

I

N

AMM 282100-710-814

ALL

20 000 FH

OPERATIONAL CHECK TO VERIFY THAT RELAY 27QA HAS NOT FAILED IN THE ENERGISED POSITION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.10 MHrs

1 AF 210

282100-06-1

MAIN FUEL PUMP SYSTEM OPERATIONAL CHECK OF STANDBY PUMP AUTOMATIC CONTROL. NOTE: ETOPS PARALLEL SYSTEM Skills :

0.50 MHrs

1 AF 210

282100-10-1


24 MO

OPERATIONAL CHECK TO ENSURE THAT THE RIGHT NO.2 MAIN FUEL PUMP OPERATES WHEN THE LEFT NO.2 MAIN FUEL PUMP IS SWITCHED OFF IN ELECTRICAL EMERGENCY CONFIGURATION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [12 / 17] ATA

: 28


28

FUEL

Task Number

Zone

282100-11-1

450 460 520 620

Task Title


Task code

Threshold Interval

DIS

Check : 4C

N

AMM 282100-960-801 SB 28-3076

ALL

DIS

I

N

AMM 123228-281-807 CMP 28-2-0000-008

ALL

References

Ctrl

DISCARD "O" OR "D" RINGS ON PYLON ENGINE FUEL FEED PIPE CONNECTORS AND REPLACE BY NEW "O" OR "D" RINGS NOTE: ETOPS PARALLEL SYSTEM

Eff

Access panels :

452CR

462CR

Total access time :

522AB 622AB 0.00 Hrs

Skills :

8.00 MHrs

1 AF 311

282200-07-4

APU FUEL PUMP SYSTEM OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO DRAIN ANY ACCUMULATED WATER. ACCESS: 311AL NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

800 FH

Check : 1A

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [13 / 17] ATA

: 28


28

FUEL

Task Number

Zone

282200-08-1

147 210 312

Task Title

APU FUEL PUMP SYSTEM

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

4 600 FH

N

AMM 282200-710-808 CMP 28-2-0000-012

ALL

OP

I

36 MO

N

AMM 282200-710-810

ALL

OP

Check : 1C

N

AMM 282200-710-812

ALL

OPERATIONAL CHECK OF RELAYS 12QC AND 14QC NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM Access panels :

312AR

734

Total access time :

744 0.00 Hrs

Skills :

0.30 MHrs

1 AF 210 310

282200-11-1

APU FUEL PUMP SYSTEM OPERATIONAL CHECK TO VERIFY THAT RELAY 15QC HAS NOT FAILED IN ENERGIZED POSITION NOTE: ETOPS PARALLEL SYSTEM Access panels :


0.00 Hrs

Skills :

0.60 MHrs

1 AV 210

282200-12-1

APU FUEL PUMP SYSTEM OPERATIONAL CHECK OF AFT APU FUEL PUMP FIRE STOP CIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS (5WF AND 6WF) NOTE: ETOPS PARALLEL SYSTEM Skills :

0.20 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [14 / 17] ATA

: 28


28

FUEL

Task Number

Zone

282300-02-1

210

Task Title

CROSSFEED SYSTEM

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

36 MO

N

AMM 282300-710-803 CMP 28-2-0000-001

ALL

OP

I

34 000 FH

N

AMM 282300-710-804

ALL

I

12 YE

I

36 MO

N

AMM 282400-710-803

ALL

N

AMM 28-25-00-869-802-A

ALL

OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL MOTORS NOTE : CMP TASK NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.10 MHrs

1 EL 210

282300-03-1

CROSSFEED SYSTEM OPERATIONAL CHECK OF CROSSFEED VALVE TO VERIFY THAT INDIVIDUAL ENGINE FUEL FEED SYSTEMS CAN BE INTERCONNECTED NOTE: ETOPS SIGNIFICATION SYSTEMS Skills :

0.02 MHrs

1 EL 520 620

282400-04-1

OP

ENGINE LP FUEL SHUT-OFF OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL MOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT AND CORRECT COCKPIT INDICATION Skills :

0.40 MHrs

1 EL N

282500-01-VNA

200

REFUEL/DEFUEL SYSTEM

OPC

Check : NT

Ground Fuel Transfer To The Trim Tank to check leak of TRIM TANK NOTE: BEFORE A/C FINISH THE C CHECK OR WHENEVER A/C BEEN DEFUEL MORE THAN 8 DAYS

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [15 / 17] ATA

: 28


28

FUEL

Task Number

Zone

282500-01-3

520 620

Task Title

Task code

DI

REFUEL/DEFUEL SYSTEM DETAILED INSPECTION OF REFUEL COUPLING(S) FOR DAMAGE OR EVIDENCE OF WEAR

Threshold Interval

I

4 400 CY

I

48 MO

I

34 000 FH

I

12 YE

References

Ctrl

Eff

N

AMM 282500-220-801

ALL

N

AMM 282500-710-802

ALL

N

AMM 282700-710-801

275

Access panels :

522HB

622HB

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF 210

282500-02-1

OP

REFUEL/DEFUEL SYSTEM OPERATIONAL CHECK TO PROVE THAT THERE IS NO FUEL TRANSFER FROM AFT TO FWD INNER TANK WHEN EMERGENCY ISOLATION VALVE IS SELECTED CLOSED Skills :

0.10 MHrs

1 EL 210

282700-02-1

OP

TRIM TRANSFER SYSTEM

Check : 2C

294

OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES FOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH

299 366

Skills :

0.25 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [16 / 17] ATA

: 28


28

FUEL

Task Number

Zone

284600-02-1

210

Task Title

Task code

OP

TANK LEVEL SENSING

Threshold Interval

I

11 300 FH

References

Ctrl

N

AMM 284600-710-802

OPERATIONAL CHECK OF INNER TANK LOW LEVEL SENSORS AND ASSOCIATED WARNINGS Skills :

0.15 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 28 [17 / 17] ATA

: 28

Eff ALL


R

29

HYDRAULIC POWER

Task Number

Zone

290000-01-1

120 140 190 320 330 340 570 670

Task code

Task Title

DI

HYDRAULIK POWER GENERAL DETAILED INSPECTION OF UNION P/N ASNA3760-XX FOR CRACKS. NOTE: IF P/N ASNA3760-XX INSTALLED NOTE: ACCORDING SB 29-3105 REPEAT INSPECTION EVERY: -24 MO IF MORE THAN 2 CRACKED UNION WERE FOUND -48 MO IF NO OR 1 OR 2 CRACKED UNION WAS FOUND

Threshold Interval

T

24 MO

I

24 MO

References

Ctrl

N

See note Check : C1

AMM 290000-200-806 AMM 290000/6 ISB 29-3105

Eff 275 294 299 366 943 946 962 1019

Access panels :

191BB 196EB 344BB 574CB 672AB

191HB 196HB 344CB 574EB 673BB

Total access time :

191KB 311AZ 572AB 574GB 673DB

191QB 325ML 573BB 574HB 673FB

192HB 325NL 573DB 574LB 674BB

192QB 334BB 573FB 575CB 674CB

195DB 334CB 574BB 575DB 674EB

40.11 Hrs

Skills :

8.00 MHrs

1 AF 147 210

291000-01-1

FUC


Check : 4C

N

AMM 291900-720-801

FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE IN YELLOW AND BLUE SYSTEMS Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [1 / 10] ATA

: 29

ALL


29

HYDRAULIC POWER

Task Number

Zone

291000-02-1

147 190

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

FUC

I

36 MO

N

AMM 123229-281-801 SIL 29-081

ALL

OP

I

18 MO

N

AMM 291000-710-802

ALL

OP

I

18 MO

N

AMM 291000-710-804

ALL

DI

Check : 1C

N

AMM 291400-200-802

ALL

HYDRAULIC FLUID ANALYSIS Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.40 MHrs

1 AF R

210

291000-03-1

MAIN HYDRAULIC POWER OPERATIONAL CHECK OF EDP DEPRESSURIZATION Skills :

0.30 MHrs

1 AF R

120 210

291000-04-1

MAIN HYDRAULIC POWER OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT-OFF VALVES Skills :

1.20 MHrs

1 AV 190

291000-05-1

MAIN HYDRAULIC POWER CHECK FOR CORRECT AIR PRESSURE BY READING GAUGES ON EACH RESERVOIR Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [2 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

291000-06-1

147 190

Task Title

MAIN HYDRAULIC POWER CHECK NITROGEN CHARGING PRESSURE ON HYDRAULIC POWER ACCUMULATORS

Task code

Threshold Interval

References

Ctrl

Eff

FNT FUC

I

400 FH

N

AMM 291000-200-802 AMM 291000/6 AMT 291000-200-802

ALL

VCK

I

800 FH

N

AMT 291000-200-803

ALL

Access panels :

195BB

196BB

Total access time :

197CB 0.06 Hrs

Skills :

0.10 MHrs

1 AF 147 197 400

291000-07-1

MAIN HYDRAULIC POWER VISUAL CHECK OF CLOGGING INDICATORS OF HIGH PRESSURE (HP), RETURN, ENGINE DRIVEN PUMPS (EDP) CASE DRAIN, RESERVOIR FILL AND AIR PRESSURIZATION UNIT (PUA) FILTERS

Check : 1A

Access panels :

415AL

734

Total access time :

744 0.18 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [3 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

291000-08-1

195

Task Title

Task code

SRV

MAIN HYDRAULIC POWER DRAINING OF WATER SEPARATORS NOTE: TASK APPLICABLE FOR ALL A/C PUA P/N 4020Q8-3 INSTALLED

Threshold Interval

I

800 FH

References

Ctrl

Eff

N

AMM 291400-600-801

ALL

Check : 1A

IF PUA P/N 4020Q8-2 INSTALLED OR

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.10 MHrs

1 AF 195

291000-10-1


VCK

I

36 MO

N

AMM 291444-600-803 SIL 29-076

ALL

VCK

I

3 200 FH

N

AMM 291400-200-803

ALL

REPLACE WATER SEPARATOR AIR FILTER AND FLUID SEPARATOR ELEMENTS Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF 140

291000-11-1

MAIN HYDRAULIC POWER VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN VALVE POSITION Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [4 / 10] ATA

: 29


R

29

HYDRAULIC POWER

Task Number

Zone

291000-17-1

410 420

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

VCK

I

18 MO

N

AMM 291149-200-804 SIL 29-066

ALL

VCK

I

900 FH

N

AMM EAD FAD ISB

291000-200-809 2011-0139 2009-24-09 29-3111

946

VCK

I

900 FH

N

AMM AOT EAD ISB

291000-200-809 A29L001-12 2012-0244 29-3111

275

VISUAL INSPECTION OF THE HYDRAULIC TUBES AND CLAMPS OF THE GREEN, BLUE AND YELLOW HYDRAULIC SYSTEM NOTE: ETOPS PARALLEL SYSTEM Access panels :

415AL

416AR

Total access time :

425AL 426AR 0.00 Hrs

Skills :

0.10 MHrs

1 AF R

147 195 196

291000-19-1

MAIN HYDRAULIC POWER VISUAL CHECK OF CHECK VALVES ON GREEN, YELLOW AND BLUE HP MANIFOLD. TASK TO BE PEFORMED IF AT LEAST ONE CHECK VALVE P/N CAR401 IS INSTALLED ON EACH HP MANIFOLD (FIN 5102JM,6103JM, 7103JM) Skills :

0.00 MHrs

1 AF R

147 195 196

291000-19-2

MAIN HYDRAULIC POWER VISUAL CHECK OF CHECK VALVES ON GREEN, YELLOW AND BLUE HP MANIFOLD.

294 299 366 943 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [5 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

291000-21-1

571 671


210


291100-01-1

Task Title

Task code

DIS

Threshold Interval

I

8 YE

FUC

Check : 4C

AMM 291000-960-801 SIL 29-098

ALL

N

AMM 291100-720-801

ALL

FUNCTIONAL CHECK OF PRIORITY VALVE NOTE: ETOPS PARALLEL SYSTEM Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff

N

See note

DISCARD OF FLEXIBLE HOSES INSTALLED IN THE OVERWING PANEL AREA LH/RH (5274GG, 5275GG, 5020GM, 5021GM, 5264GG, 5265GG). NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.

References

Ctrl

Page : SYS - 29 [6 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

291100-03-1

210

Task Title


Task code

Threshold Interval

References

Ctrl

Eff

OP

I

24 MO

N

AMM 291100-710-804

ALL

SER

I

1 600 FH

N

AMM 122429-600-801

ALL

N

AMM 291900-710-801

ALL

OPERATIONAL CHECK OF AUTOMATIC CONTROL OF FIRE SHUT-OFF VALVE IN CASE OF LOW LEVEL ON GREEN HYDRAULIC SYSTEM NOTE: ETOPS PARALLEL SYSTEM Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF 147 148 195 196

291700-01-1


Check : 2A

DRAIN RECOVERY TANK Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.20 MHrs

1 AF 210

291900-01-1

HYD GROUND INTERNAL LEAK TEST SYSTEM

OP

Check : 4C

OPERATIONAL CHECK OF INHIBITION OF MANUAL CONTROL OF LEAK MEASUREMENT SOLENOID VALVE Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [7 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

292000-01-1

210

Task Title

AUXILIARY HYDRAULIC POWER

Task code

OP

Threshold Interval

I

3 200 FH

References

Ctrl

Eff

N

AMM 292000-710-802

ALL

N

AMM 292000-710-801

ALL

Check : 4A

OPERATIONAL CHECK OF AUTOMATIC AND MANUAL START OF GREEN AND YELLOW ELECTRICAL PUMPS AND MANUAL START OF BLUE ELECTRICAL PUMP Skills :

2.00 MHrs

1 AF 120 210

292000-02-1


OP

I

3 200 FH

Check : 4A

OPERATIONAL CHECK OF AUTOMATIC START OF GREEN AND YELLOW ELECTRIC PUMPS Skills :

2.00 MHrs

1 AF 147 210

292000-04-1


FUC

I

12 000 FH

N

AMM 291900-720-802

ALL

FUC

I

12 000 FH

N

AMM 293100-720-804

ALL

FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE IN GREEN SYSTEM Skills :

1.00 MHrs

1 AF 210

292000-05-1

AUXILIARY HYDRAULIC POWER FUNCTIONAL CHECK OF GREEN, BLUE AND YELLOW LOW LEVEL WARNING SYSTEM Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [8 / 10] ATA

: 29


R

29

HYDRAULIC POWER

Task Number

Zone

292000-06-1

210

Task Title


Task code

OP

Threshold Interval

Check : 1C

References

Ctrl

N

AMM 292000-710-804

Eff 943 946

OPERATIONAL CHECK OF THE AUTOMATIC START OF THE BLUE ELECTRIC PUMP

962 1019 1256 1266

120 140 210 633

292400-01-1


OP

I

24 MO

N

AMM 292400-710-804

ALL

N

AMM 293100/6 AMT 293100-200-801

ALL

Check : 1C

OPERATIONAL CHECK OF RAM AIR TURBINE AUTOMATIC DEPLOYMENT DETAILED INSPECTION OF THE RAM AIR TURBINE ONCE EXTENDED. Access panels :

633HB Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 190 210

293000-01-1

HYDRAULIC SYSTEM DATA ACQUISITION / INTE CROSS CHECK FLUID LEVEL ON EACH RESERVOIR, ON ECAM HYDRAULIC PAGE AND GROUND SERVICE PANEL INDICATOR

OP

I

1 600 FH

Check : 2A

Access panels :

197CB Total access time :

0.02 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [9 / 10] ATA

: 29


29

HYDRAULIC POWER

Task Number

Zone

293000-02-1

147 190 210

Task Title

HYDRAULIC SYSTEM DATA ACQUISITION / INTE

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 293100-710-802

ALL

OP

Check : 1C

N

AMM 293100-740-802

ALL

OPERATIONAL CHECK OF RESERVOIRS LOW AIR PRESSURE WARNING Access panels :

195BB

196BB

Total access time :

197CB 734 0.22 Hrs

744

Skills :

0.40 MHrs

1 AF 210

293000-03-1

HYDRAULIC SYSTEM DATA ACQUISITION / INTE OPERATIONAL CHECK OF OVERHEAT DETECTION SYSTEM Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 29 [10 / 10] ATA

: 29


30

ICE AND RAIN PROTECTION

Task Number

Zone

301100-01-1

500 600

Task code

Task Title

DI

WING ICE PROTECTION

Threshold Interval

References

Ctrl

Eff

Check : 2C

N

AMM 301100-200-801

ALL

FUC

I

24 MO

N

AMM 303100-720-802 SIL 34-084

ALL

OP

I

12 000 FH

N

AMM 304600-710-801

275

DETAILED INSPECTION OF TELESCOPIC DUCTS, FLEXIBLE SLAT INTERCONNECTION SLEEVES AND, IN WING LEADING EDGE, ANTI-ICING DUCT COUPLINGS, CLAMPS AND ATTACHMENT POINTS NOTE: ETOPS SIGNIFICATION SYSTEMS Access panels :

522JB 622LB

522LB 622NB

Total access time :

522NB 622RB

522RB 623CB

523CB 623EB

523EB

622JB

0.00 Hrs

Skills :

1.00 MHrs

1 EL 120

303100-01-1

PROBE ICE PROTECTION FUNCTIONAL CHECK OF HEATER INSULATION RESISTANCE OF THE PITOT PROBES. GOODRICH PITOT PROBE PN 0851 HL INSTALLED NOTE: ETOPS PARALLEL SYSTEM

120 130 150 170

304600-01-1

Issue No

:

Date

:

10 01/12/2013

ESCAPE SLIDE LOCKING MECHANISM ICE PROTE

294

OPERATIONAL CHECK OF ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION

Amendment No Date

: 01 : 06/09/2014

299 366

Page : SYS - 30 [1 / 1] ATA

: 30


31


Task Number

Zone

313300-02-1

210

Task Title


Task code

OP

Threshold Interval

Ctrl

See note

N

AMM 313300-710-803

ALL

2 YE

N

AMM 313300-720-802

ALL

AMM 313300-710-815

ALL

References

Eff

Check : 1C

OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU Skills :

0.10 MHrs

1 AV 312

313300-03-1

DGTL FLIGHT DATA RCDG SYSTEM (DFDRS)

OP

I Check : C

OPERATIONAL CHECK OF THE ULB NOTE : DUKANE P/N : DK100-DK120 HONEYWELL P/N : 980-4700-042 NOTE:NATIONAL/VENDOR REQUIREMENT TASK Access panels :


0.00 Hrs

Skills :

0.25 MHrs

1 AV 310

313300-04-1


OP

I

12 MO

N

FUC

I

12 MO

N

DOWNLOAD DFDR DATA 313300-04-1A

310


ALL

READ OUT OF DFDR DATA TO ENSURE RECORDED PARAMETERS MEET THE RANGE AND ACCURACIES REQUIRED IN "BO QUY CHE AN TOAN HANG KHONG DAN DUNG LINH VUC TAU BAY VA KHAI THAC TAU BAY"

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 31 [1 / 4] ATA

: 31


31


Task Number

Zone

313300-05-1

120 210


210

CENTRAL WARNING SYSTEM

315000-01-1

Task Title

Task code

OP

Threshold Interval

I

24 000 FH

References

Ctrl

N

AMM 313300-710-820

Eff 1256 1266

OPERATIONAL CHECK OF WGL-QAR INTERLOCK AND TRANSMISSION LOGIC. OP

I

34 000 FH

N

AMM 315000-740-803

ALL

OP

I

34 000 FH

N

AMM 315000-740-804

ALL

OP

Check : 1C

N

AMM 316000-710-804

275

OPERATIONAL CHECK OF SLAT AND FLAP SENSOR CIRCUIT VIA MCDU Skills :

0.10 MHrs

1 AV 210

315000-02-1

CENTRAL WARNING SYSTEM OPERATIONAL CHECK OF DMC OUTPUT CIRCUITS TO FWC„S Skills :

0.10 MHrs

1 AV 210

316000-01-1

ELECTRONIC INSTRUMENT SYSTEM 2 (LCD TECH

294

OPERATIONAL CHECK OF PFD/ ND AND ECAM/ ND MANUAL TRANSFER

299 366

Skills :

0.20 MHrs

1 AV 210

316000-02-1


OP

Check : 1C

N

AMM 316000-710-805

275 294

OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER

299 366

Skills :

0.25 MHrs

1 AV Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 31 [2 / 4] ATA

: 31


31


Task Number

Zone

316000-03-1

210

Task Title


Task code

OP

Threshold Interval

Check : 2C

References

Ctrl

N

AMM 316000-710-806

210


299 366

OP

I

34 000 FH

N

AMM 316000-720-801

210

316001-01-1


275 294

OPERATIONAL CHECK OF EFIS OFFSIDE AND ECAM NON ACTIVE MONITORING CIRCUITS

R

275 294

OPERATIONAL CHECK OF CORRECT EFIS AND ECAM TRANSFER WHEN BUSBAR 105XP IS LOST

316000-04-2

Eff

299 366

OP

I

24 MO

N

AMM 316000-710-809

946

Check : 1C

OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL TRANSFER

943 962 1019 1256 1266

Skills :

0.20 MHrs

1 AV R

121 210 211 212

316001-03-1


OP

Check : 2C

N

AMM 316000-710-807

943 946

OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN BUSBAR 105XP IS LOST

962 1019 1256 1266

Skills :

0.80 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 31 [3 / 4] ATA

: 31


R

31


Task Number

Zone

316001-04-1

210 211 212

Task Title


Task code

OP

Threshold Interval

I

24 MO

References

Ctrl

N

AMM 316000-710-810

Eff 943 946

OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER

962 1019 1256 1266

Skills :

1.20 MHrs

1 AV 210

316322-01-1

REM

DISPLAY UNIT

I

2 400 FH

N

REPOSITION ALL CATHODE RAY TUBES BY SWAPPING ALL DISPLAY UNITS FROM ONE POSITION (PFD, ND, UPPER ECAM, LOWER ECAM) TO ANOTHER NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE

AMM 316322-400-802 SIL 31-025

275 294 299 366

Skills :

0.25 MHrs

1 AV 210

316322-02-1

REM

DISPLAY UNIT FUNCTIONAL CHECK OF DISPLAY UNIT BRIGHTNESS. NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE

I

1 600 FH

Check : 2A

N

AMM 316322-200-801 SIL 31-030

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

366

0.50 MHrs

: 01 : 06/09/2014

294 299

Skills :

1 AV

275

Page : SYS - 31 [4 / 4] ATA

: 31


R

32

LANDING GEAR

Task Number

Zone

VN320000-01

700

Task Title

Task code

GVI

MAIN LDG BRAKES

731 741

LUB

MAIN GEAR AND DOORS

I

800 FH

References

Ctrl

Eff

N

AMM 324000-210-802

ALL

N

AMM 122232-600-817

ALL

Check : 1A

INSPECTION/CHECK MAIN LANDING GEAR BRAKES. CARRY OUT THE WEAR INDICATOR PIN MEASUREMENT AND RECORD. 321000-03-1

Threshold Interval

LUBRICATION OF MLG AND DOORS

I

500 CY

I

4 MO

Skills :

2.40 MHrs

1 AF 731 741

321000-04-1

MAIN GEAR AND DOORS

LUB

Check : WY

N

AMM 122232-640-801

ALL

LUB

I

250 CY

N

4 MO

AMM 122232-600-820 AMM 122232/3

ALL

I

I

1 600 FH

N

AMM 121432-614-802

ALL

LUBRICATION OF MLG BOGIE PIVOT PIN Skills :

0.30 MHrs

1 AF D

731 741

321000-05-1

MAIN GEAR AND DOORS LUBRICATION OF SHORTENING MECHANISM SM8 AND SM9 HINGE JOINTS. Skills :

0.00 MHrs

1 AF 321100-VNA-1

Issue No

:

Date

:

731 741

10 01/12/2013

MAIN LANDING GEAR SHOCK ABSORBER GAS REPLENISHMENT OF THE MLG SHOCK ABSORBER

Amendment No Date

: 01 : 06/09/2014

SER

Check : 2A

Page : SYS - 32 [1 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

321100-03-1

731 741

Task Title

MAIN GEAR

Task code

Threshold Interval

FUC

Check : 1C

N

AMM 321100-220-819

ALL

SER

I

N

AMM 321100-220-803

ALL

N

AMM 321127-200-801

ALL

N

AMM 321100-210-831

ALL

N

AMM 321100-210-820

ALL

References

Ctrl

Eff

FUNCTIONAL CHECK OF MLG SHOCK ABSORBER NITROGEN CHARGE PRESSURE. Skills :

1.00 MHrs

1 AF 731 741

321100-04-1

MAIN GEAR

42 MO

Check : 2C

SERVICE MLG SHOCK ABSORBER Skills :

3.32 MHrs

1 AF 731 741

321100-05-1

DVI

MAIN GEAR

I

42 MO

Check : 2C

FUNCTIONAL CHECK MLG TORQUE LINKS FOR EXCESSIVE PLAY Skills :

0.40 MHrs

1 AF 321100-14-1

321100-23-1

731 741

MAIN GEAR

731 741

MAIN GEAR

GVI

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF MLG BOGIE PITCH TRIMMER CONTROL MANIFOLD. GVI

GENERAL VISUAL INSPECTION OF MLG SHOCK ABSORBER.

I

I

800 FH

Check : 1A

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [2 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

321100-24-1

731 741

MAIN LANDING GEAR

731 741

MAIN LANDING GEAR

711

NOSE GEAR AND DOORS

321100-27-1

322000-01-1

Task Title

Task code

SDI

SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN MLG AIRFRAME ATTACHMENT FITTINGS. GVI

Threshold Interval

I

17 000 CY

I

10 YE

I

800 FH

References

Ctrl

Eff

N

AMM 321100-280-801

ALL

N

AMM 32-11-00-210-832

ALL

N

AMM 122232-600-819

ALL

N

AMM 121432-614-804

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF MLG STOP PAD. LUB

LUBRICATION OF NLG AND DOORS.

I

500 CY

I

4 MO

I

1 600 FH

Skills :

0.60 MHrs

1 AF 322100-VNA-1

711

SER

NOSE GEAR

Check : 2A

GAS REPLENISHMENT OF THE NLG SHOCK ABSORBER 711

322100-03-1

NOSE GEAR SHOCK ABSORBER

SER

Check : 2C

N

AMM 322100-220-802

ALL

FUC

I

N

AMM 322100-720-801

ALL

SERVICE NLG SHOCK ABSORBER Skills :

1.16 MHrs

1 AF R

711

322100-04-1

NOSE GEAR FUNCTIONAL CHECK NLG SHOCK ABSORBER NITROGEN CHARGE PRESSURE.

24 MO

Check : 1C

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [3 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

322100-05-1

711

Task Title

NOSE GEAR TORQUE LINKS

Task code

Threshold Interval

FUC

Check : 2C

N

AMM 322127-200-801

ALL

GVI

I

800 FH See note Check : 1A

N

AMM 322100-210-806

ALL

SDI

I

17 000 CY

N

AMM 322100-280-801

ALL

I

10 YE

I

2 200 CY

N

AMM 323100-220-801

ALL

I

24 MO

I

12 YE

N

AMM 323100-220-802

ALL

References

Ctrl

Eff

FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE PLAY PREP. : AIRCRAFT JACKING (NLG ONLY); Skills :

0.60 MHrs

1 AF 710

322100-06-1

NOSE GEAR GENERAL VISUAL INSPECTION OF NLG SHOCK ABSORBER. Skills :

0.10 MHrs

1 AF 711

322100-11-1

NOSE GEAR SPECIAL DETAILED INSPECTION OF BUSHES AND BEARINGS IN NLG AIRFRAME ATTACHMENT FITTINGS.

323000-20-1

323000-21-1

Issue No

:

Date

:

123 147 148 700

NORMAL EXTENSION AND RETRACTION

123 147 148


10 01/12/2013

DI

DETAILED INSPECTION OF LANDING GEAR UPLOCK UNITS, DOOR UPLOCK UNITS AND ROLLERS. DI

DETAILED INSPECTION OF LANDING GEAR DOOR HINGE BEARINGS, ATTACHMENT LUG BUSHES AND PINS.

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [4 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

323000-22-1

123 147 148


711


323000-25-1

Task Title

Task code

323100-01-1

References

Ctrl

Eff

DI

I

12 YE

N

AMM 323100-220-803

ALL

FUC

I

17 000 CY

N

AMM 323100-720-806

ALL

I

10 YE

I

17 000 CY

N

AMM 323100-720-807

ALL

I

10 YE

I

1 600 FH

N

AMM 323100/6 AMT 323100-210-801

ALL

N

AMM 323100-710-803

ALL

DETAILED INSPECTION OF LANDING GEAR DOOR ACTUATING CYLINDER BEARINGS, ATTACHMENT LUG BUSHES AND PINS.

FUNCTIONAL CHECK OF NLG RETRACTION ACTUATOR. 323000-26-1

Threshold Interval

731 741


700


FUC

FUNCTIONAL CHECK OF MLG RETRACTION ACTUATOR. VCK

Check : 2A

VISUAL CHECK OF DOWN LOCK SPRINGS ON ALL LANDING GEARS Skills :

0.20 MHrs

1 AF 210

323100-02-1


OP

Check : 4C

OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK. Skills :

0.06 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [5 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

323100-03-1

210

Task Title


Task code

Threshold Interval

FUC

Check : 4C

N

AMM 323100-720-802

ALL

VCK

I

25 000 FH

N

5 YE

AMM 321100-210-830 ISB 32-3178

275

I

OP

I

8 000 FH

N

AMM 323300-710-809

ALL

FUC

I

6 YE

N

AMM 323300-720-804

ALL

References

Ctrl

Eff

FUNCTIONAL CHECK OF LANDING GEAR ISOLATION SAFETY VALVE. PREP. : APU RUNNING; Skills :

1.16 MHrs

1 AF R

731 741

323100-12-1

NORMAL EXTENSION AND RETRACTION VISUAL CHECK OF MLG UPLOCK ROLLER FOR EVIDENCE AND CORROSION.

366

Skills :

0.00 MHrs

1 AF 700

323300-03-1

FREE FALL EXTENSION OPERATIONAL CHECK OF LANDING GEAR FREE-FALL SYSTEM. Skills :

1.20 MHrs

1 AF 700

323300-04-1

FREE FALL EXTENSION FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION Skills :

0.76 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [6 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

324000-02-1

195

Task Title

Task code

FUC

BRAKE ACCUMULATORS

Threshold Interval

I

800 FH

Eff

N

AMM 324000/6 AMT 324000-210-805

ALL

N

AMM 324000/6 AMT 324000-210-804

ALL

N

AMM 324400-710-802 CMP 32-2-0000-001

ALL

N

AMM 324000-220-803

ALL

Check : 1A

FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON ALTERNATE PARKING BRAKE ACCUMULATORS.

References

Ctrl

Access panels :

195BB Total access time :

0.00 Hrs

Skills :

0.03 MHrs

1 AF 731 741

324000-03-1

FUC

BRAKE ACCUMULATORS

I

1 600 FH

Check : 2A

CHECK NORMAL AND ALTERNATE BRAKE RETURN ACCUMULATORS NITROGEN PRESSURES BY READING GAUGES Access panels :

731

741

Total access time :

0.00 Hrs

Skills :

0.06 MHrs

1 AF 210

324000-04-1

OP

BRAKES AND WHEELS

I

3 200 FH

Check : 4A

OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE NOTE : CMP TASK Skills :

1.00 MHrs

1 AF 731 741

324000-19-1

Issue No

:

Date

:

10 01/12/2013

BRAKES AND WHEELS DETAILED INSPECTION OF MLG AXLE SLEEVES.

Amendment No Date

: 01 : 06/09/2014

DI

I

24 MO

Check : 1C

Page : SYS - 32 [7 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

324100-03-1

700

Task Title

TYRES

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

36 HR

N

AMM 324100-210-803

ALL

FUC

I

3 DY

N

AMM 324100-220-802

ALL

DVI

I

18 MO

N

AMM 324100-210-804

ALL

VCK

I

7 DY

N

AMM 324000-210-802

ALL

GENERAL VISUAL INSPECTION OF TYRES, WHEELS AND BRAKES. Skills :

0.30 MHrs

1 AF 700

324100-04-1

TYRES FUNCTIONAL CHECK OF TYRE PRESSURES Skills :

0.20 MHrs

1 AF 731 741

324100-05-1

WHEELS DETAILED INSPECTION OF AXLE OUTER DIAMETER AND AXLE SLEEVE INNER DIAMETER NOTE: TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF AN ADJACENT BRAKE CHANGE ON EACH BRAKED AXLE. PREP. : AIRCRAFT JACKING; MLG BRAKES; MLG SLEEVES; MLG WHEELS; Skills :

0.40 MHrs

1 AF 730 740

324200-01-1

BRAKE UNITS VISUAL CHECK OF HEAT PACK WEAR INDICATOR. Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [8 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

324300-01-1

122

Task Title

ALTERNATE BRAKE HYDRAULIC RESERVOIR

Task code

Threshold Interval

FUC

Check : 1C

N

AMM 324300-210-802

ALL

SER

I

N

AMM 324314-200-801

ALL

N

AMM 324500-710-803 SIL 32-091

ALL

N

AMM 324900-220-802

ALL

References

Ctrl

Eff

FUNCTIONAL CHECK OF BRAKE LOW PRESSURE RESERVOIR FLUID LEVEL. Access panels :

132AZ

811

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 147

324314-01-1

ALTERNATE BRAKE DUAL VALVE

3 200 FH

Check : 4A

VISUAL CHECK OF BRAKE DUAL DISTRIBUTION VALVE (BDDV) DRAIN TUBE FOR THE ACCUMULATION OF WATER. Skills :

0.20 MHrs

1 AF 210

324500-01-1

OP

PARKING BRAKING OPERATIONAL CHECK OF THE PARKING BRAKE CONTROL VALVE MOTORS 1 AND 2

I

2 000 CY

I

24 MO

I

800 FH

Skills :

0.20 MHrs

1 AF 210 700

324900-02-1

CHK

TYRE PRESSURE SYSTEM FUNCTIONAL CHECK OF TPIS AND CROSS CHECK WITH TYRE PRESSURE GAUGE READING.

Check : 1A

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [9 / 11] ATA

: 32


R

32

LANDING GEAR

Task Number

Zone

325100-02-1

710

Task Title

NOSE WHEEL STEERING

Task code

Threshold Interval

FUC

Check : 1C

N

AMM 325100-720-810

ALL

GVI

I

N

AMM 325100-210-801

ALL

References

Ctrl

Eff

FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON NOSE WHEEL STEERING ACCUMULATOR. Skills :

0.23 MHrs

1 AF 711

325100-04-1

NOSE WHEEL STEERING

Check : 1A

GENERAL VISUAL INSPECTION OF NOSE WHEEL STEERING ACTUATOR AND ROTATING SELECTOR VALVE. 210

325300-01-1

STEERING ANGLE PROTECTION

800 FH

OP

Check : 1C

N

AMM 325300-710-802

ALL

OP

I

N

AMM 325300/5 AMT 325300-710-801

ALL

N

AMM 326100-710-801

ALL

OPERATIONAL CHECK OF OVERSTEER INDICATION SYSTEM Skills :

0.40 MHrs

1 AF R

210 710

325300-02-1

STEERING ANGLE PROTECTION

800 FH

Check : 1A

OPERATIONAL CHECK OF COCKPIT AND NLG WARNING LAMPS Skills :

0.20 MHrs

1 EL 210

326100-01-1

LANDING GEAR INDICATING AND WARNING

OP

Check : 1C

OPERATIONAL CHECK OF LANDING GEAR INDICATION CIRCUITS. Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [10 / 11] ATA

: 32


32

LANDING GEAR

Task Number

Zone

326100-02-1

210

Task Title

LANDING GEAR INDICATING AND WARNING

Task code

OP

Threshold Interval

Check : 4C

References

Ctrl

N

AMM 323100-710-804

OPERATIONAL CHECK OF GROUND DOORS CLOSURE INHIBIT Skills :

0.66 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 32 [11 / 11] ATA

: 32

Eff ALL


33

LIGHTS

Task Number

Zone

331400-01-1

210

Task Title

ANNUNCIATOR LIGHT TEST AND DIMMING

Task code

OP

Threshold Interval

I

1 600 FH

Eff

N

AMM 331400/5 AMT 331400-710-801

ALL

N

AMM 335100/5 AMT 335100-710-801

ALL

N

AMM 335100/5 AMT 335100-710-802

ALL

Check : 2A

OPERATIONAL CHECK OF LIGHTS

References

Ctrl

Skills :

0.10 MHrs

1 EL 200

335100-01-1

OP

CABIN EMERGENCY LIGHTING

I

1 600 FH

Check : 2A

OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA MCDU Skills :

0.15 MHrs

1 EL 210

335100-02-1

OP

CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK VIA MCDU NOTE: -AS AN ALTERNATIVE, TASK MAY BE ACCOMPLISHED BY REPLACING BATTERIES BY FULLY CHARGED UNITS (REF AMM 335100-710-802-01)AS EXPLAINED IN SIL 33-033 NOTE:As long as all applicable tests of the battery within the aircraft system or under storage conditions are passed, the battery can remain in service.

I

6 MO See note

Skills :

0.10 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 33 [1 / 2] ATA

: 33


33

LIGHTS

Task Number

Zone

335100-03-1

200 210

Task Title

Task code

OP

CABIN EMERGENCY LIGHTING

Threshold Interval

I

20 000 FH

References

Ctrl

N

AMM 335100-710-803

OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM AUTOMATIC CONTROL CIRCUIT AND MANUAL ACTIVATION FROM BOTH CONTROL PANELS AND CHECK ALL LIGHTS AND SIGNS ILLUMINATED BY BATTERIES Skills :

0.30 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 33 [2 / 2] ATA

: 33

Eff ALL


34

NAVIGATION

Task Number

Zone

341300-01-1

210

Task Title

Task code

OP

AIR DATA REFERENCE

Threshold Interval

References

Ctrl

Eff

Check : 2C

N

AMM 341100-710-804

ALL

T

N

AMM 303100-720-801 ISB 34-3215

1019

OPERATIONAL CHECK OF PITOT PROBES HEATING (115 VAC) AND ADR/AOA POWER SUPPLY (26 VAC) IN EMERGENCY CONFIGURATION Skills :

0.20 MHrs

1 RA D

120

341300-02-1

FUC

AIR DATA FUNCTIONAL TEST OF THE HEATING OF THE THREE AOA SENSORS. NOTE: ETOPS PARALLEL SYSTEM

17 000 FH

I

3 800 FH

I

24 MO

366

Skills :

2.25 MHrs

1 RA 121 122

341300-03-1

RS

AIR DATA

N

AMM 341100-170-801 SIL 34-084

ALL

N

AMM 341100-790-801 AMM 341100/5

ALL

FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES NOTE: - THIS TASK PRECLUDES TASK 341300-04-1. NOTE: RII TASK Skills :

1.50 MHrs

1 RA 121 122 210

341300-04-1

FUC

AIR DATA LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS NOTE: RII TASK

Check : 2C

Skills :

0.60 MHrs

1 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [1 / 7] ATA

: 34


R

34

NAVIGATION

Task Number

Zone

341300-05-1

210

Task Title

Task code

OP

AIR DATA

Threshold Interval

I

12 000 FH

References

Ctrl

N

AMM 341300-710-806

Eff 943 946

OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY

962 1019 1256 1266

Skills :

0.20 MHrs

1 RA 341300-06-1

341400-01-1

121 122 123

AIR DATA

210

INERTIAL REFERENCE SYSTEM

OP

I

800 FH

N

AMM 341100-170-804

ALL

OP

I

48 MO

N

AMM 341100-710-802

ALL

OP

Check : 2C

N

AMM 341100-710-803

ALL

CLEANING OF 1 OUT OF 3 PITOT PROBES. NOTE: TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3. NOTE: RII TASK

OPERATIONAL CHECK OF ATT/HDG SWITCHING Skills :

0.15 MHrs

1 RA 210

341400-02-1

INERTIAL REFERENCE SYSTEM OPERATIONAL CHECK OF ADIRU 1, 2 AND 3 POWER SUPPLY IN EMERGENCY CONFIGURATION Skills :

0.40 MHrs

2 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [2 / 7] ATA

: 34


34

NAVIGATION

Task Number

Zone

342100-01-1

120 130 210

Task Title


Task code

Threshold Interval

SER

Check : 1C

References

Ctrl

N

DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS NOTE: - THIS TASK PRECLUDES TASK 342100-02-1. NOTE: RII TASK

AMM 341100-170-803 SIL 34-084

Eff 275 294 299 366

Access panels :

131NF

132AZ

Total access time :

211BW 821 0.20 Hrs

Skills :

1.65 MHrs

1 AV 210

342100-02-1


SER

Check : 2C

N

AMM 341100-790-802

275 294

LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS NOTE: RII TASK

299 366

Skills :

0.30 MHrs

1 AV R

120 130 210

342200-01-1

INTEGRATED STANDBY INSTRUMENT SYSTEM (IS DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS NOTE: - THIS TASK PRECLUDES TASK 342200-02-1. NOTE: RII TASK

FUC

Check : 1C

N

AMM 342225-170-801 SIL 34-084

943 946 962 1019 1256 1266

Skills :

0.25 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [3 / 7] ATA

: 34


R

34

NAVIGATION

Task Number

Zone

342200-02-1

120

Task Title

INTEGRATED STANDBY INSTRUMENT SYSTEM (IS

Task code

Threshold Interval

FUC

Check : 2C

References

Ctrl

N

AMM 342225-790-801

Eff 943 946

LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS NOTE: RII TASK

962 1019 1256 1266

Skills :

0.15 MHrs

1 AF R

120 210

342200-03-1

INTEGRATED STANDBY INSTRUMENT SYSTEM (IS

OP

I

800 FH

N

AMM 342225-710-801

943 946

OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY

962 1019 1256 1266

R

120

344100-02-1

WEATHER RADAR SYSTEM REMOVE WEATHER RADAR TRANSCEIVER MOUNTING TRAY FILTER FOR CLEANING.

REM

I

30 000 FH

I

72 MO

N

AMM 344100-100-801

275 294 299 366 946

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [4 / 7] ATA

: 34


34

NAVIGATION

Task Number

Zone

344200-01-1

150

Task Title

RADIO ALTIMETER

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

30 MO

N

AMM 344200-750-801

ALL

DIS

I

144 MO

N

AMM 344211-920-801 SIL 34-097

ALL

OP

I

6 MO

N

AMM 344211-615-801

ALL

DETAILED INSPECTION AND OPERATIONAL CHECK OF THE RADIO ALTIMETER FAN. NOTE: -36 MONTHS FOR COLLINS RA (POST 41510 OR POST 58883) -30 MONTHS FOR THALES RA (POST 45022 OR POST 51485 OR POST 52991 OR POST 56101) AND HONEYWELL RA (POST 43260 OR POST 46732 OR POST 54901) Access panels :

152PW

152UW

Total access time :

0.60 Hrs

Skills :

0.75 MHrs

1 RA 150

344200-03-1

RADIO ALTIMETER RADIO ALTIMETER ANTENNAS AND COAXIAL CABLES REPLACEMENT. Skills :

0.00 MHrs

1 RA 150

344200-04-1

RADIO ALTIMETER RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE CLEANING.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [5 / 7] ATA

: 34


R

34

NAVIGATION

Task Number

Zone

344800-01-1

210

Task Title

TERRAIN AWARNESS AND WARNING SYSTEM

Task code

OP

Threshold Interval

Check : 2C

References

Ctrl

N

AMM 344800-740-801

Eff 275 294

OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM.

299 366 946 1256 1266

Skills :

0.10 MHrs

1 RA 210

344800-02-1

TERRAIN AWARENESS WARNING SYSTEM

OP

Check : 2C

N

AMM 344300-740-802

962

BITE TEST OF THE T2CAS (TAWS PART).

R

210

345200-01-1

1019

FUC

ATC MODE S (SELECT)

943

I

24 MO

N

AMM 345200-720-801

ALL

N

AMM 345700-710-801

275

FUNCTIONAL CHECK OF THE AIR TRAFFIC CONTROL TRANSPONDER SYSTEM PER 14 CFR PART 91.413. 210

345300-01-1

AUTOMATIC DIRECTION FINDER (ADF)

OP

Check : 1C

294

OPERATIONAL CHECK OF ADF 1 IN EMERGENCY CONFIGURATION

299 366

Skills :

0.40 MHrs

2 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [6 / 7] ATA

: 34


34

NAVIGATION

Task Number

Zone

345500-01-1

210

Task Title

Task code

OP

VOR/MARKER

Threshold Interval

Check : 1C

References

Ctrl

N

AMM 345700-710-802

Eff 275 294

OPERATIONAL CHECK OF VOR 1 IN EMERGENCY CONFIGURATION

299 366

Skills :

0.40 MHrs

2 RA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 34 [7 / 7] ATA

: 34


35

OXYGEN

Task Number

Zone

351200-03-1

210

Task Title

Task code

OP

CREW OXYGEN

Threshold Interval

I

24 MO

References

Ctrl

Eff

N

AMM 351241-710-801

ALL

Check : 1C

OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK Skills :

0.10 MHrs

1 AF 210

351200-04-1

CREW OXYGEN

VCK

I

24 MO

N

AMM 351241-200-803

ALL

SER

I

24 MO

N

AMM 351241-100-802

ALL

FUC

I

6 500 FH

N

AMM 351000-200-806

ALL

I

24 MO

N

AMM 352300-710-808

ALL

DETAILED INSPECTION OF CREW OXYGEN MASKS (OUT OF BOX WITH HARNESS INFLATED). Skills :

0.20 MHrs

1 AF 210

351200-05-1

CREW OXYGEN CLEAN OXYGEN MASKS Skills :

0.40 MHrs

1 CL 122 210

351200-07-1

CREW OXYGEN CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN FILL PANEL AND GAUGES ON OXYGEN CYLINDERS. Skills :

0.20 MHrs

1 AF 200

352001-06-1

PASSENGER OXYGEN (CHEMICAL)

OP

Check : 4C

OPERATIONAL CHECK OF IN SEAT POWER SUPPLY INTERRUPTION Skills :

0.25 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 35 [1 / 4] ATA

: 35


35

OXYGEN

Task Number

Zone

352100-01-1

200

Task Title

PASSENGER OXYGEN ( CHEMICAL )

Task code

OP

Threshold Interval

I

6 YE

References

Ctrl

Eff

N

AMM 352100-710-804

ALL

OPERATIONAL CHECK OF MANUAL MASK RELEASE Skills :

0.50 MHrs

1 AF 120 200 210

352100-02-1


FUC

Check : 4C

N

AMM 352100-720-801

ALL

VCK

I

N

AMM 352100-210-802

ALL

DVI

Check : 4C

N

AMM 352100-210-803

ALL

FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE Access panels :

132AZ Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 200

352100-03-1


6 YE

VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS OF DISCHARGE Skills :

16.50 MHrs

1 AF 200

352100-04-1

PASSENGER OXYGEN (CHEMICAL) DETAILED INSPECTION OF OXYGEN MASKS Skills :

16.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 35 [2 / 4] ATA

: 35


35

OXYGEN

Task Number

Zone

353000-01-1

200

Task Title

Task code

VCK

PORTABLE OXYGEN

Threshold Interval

I

8 DY

References

Ctrl

Eff

N

AMM 353000-210-801

946

N

AMM 353152-210-802

ALL

Check : WY

CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE Skills :

0.10 MHrs

1 AF 210

353100-01-1

FLIGHT CREW PORTABLE BREATHING EQPT

VCK

I

8 DY

Check : WY

CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION OF PROTECTIVE BREATHING EQUIPMENT. Skills :

0.10 MHrs

1 AF 200

353200-01-1

PORTABLE OXYGEN

VCK

I

72 MO

N

AMM 353000-210-803

ALL

VCK

I

8 DY

N

AMM 353000-210-802

ALL

GENERAL VISUAL INSPECTION OF OXYGEN CYLINDER ATTACHMENT. Skills :

1.00 MHrs

1 AF 220 230 240 250 260 270

353200-02-1

Issue No

:

Date

:

10 01/12/2013

CABIN ATTENDANTS PORTABLE BREATHING EQ CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION ON PROTECTIVE BREATHING EQUIPMENT

Amendment No Date

: 01 : 06/09/2014

Check : WY

Page : SYS - 35 [3 / 4] ATA

: 35


35

OXYGEN

Task Number

Zone

353200-06-1

200

Task Title

Task code

DI

PORTABLE OXYGEN

Threshold Interval

I

24 MO

References

Ctrl

N

AMM 353000-210-811

DETAILED INSPECTION OF THE OXYGEN CONTINOUS FLOW MASK. Skills :

0.70 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 35 [4 / 4] ATA

: 35

Eff ALL


36

PNEUMATIC

Task Number

Zone

361100-03-1

450 460

Task Title

ENGINE BLEED AIR SUPPLY FUNCTIONAL CHECK OF OVERPRESSURE VALVE NOTE : EXTENDED RANGE OPERATIONS RELATED TASK. NOTE: ETOPS PARALLEL SYSTEM

Task code

Threshold Interval

References

Ctrl

Eff

OP FUC

I

20 000 FH

N

AMM 361153-720-808

ALL

OP

I

36 MO

N

AMM 361100-710-815 CMP 36-2-0000-002

ALL

Access panels :

415BL

417AL

Total access time :

425BL 427AL 0.00 Hrs

Skills :

1.00 MHrs

1 EN 210

361100-05-1

ENGINE BLEED AIR VALVE OPERATIONAL CHECK OF MANUAL BLEED SHUT OFF NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [1 / 7] ATA

: 36


36

PNEUMATIC

Task Number

Zone

361100-11-1

210 450 460

Task Title

Task code

CHK

ENGINE BLEED AIR SUPPLY

Threshold Interval

I

36 MO

Eff

N

AMM 361100-790-803 SIL 36-049

ALL

N

AMM 361141-220-801

ALL

See note

PERFORM LEAK CHECK OF THE PYLON DUCT SLEEVES COMBO SEALS NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR´S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED NOTE: ETOPS PARALLEL SYSTEM

References

Ctrl

Access panels :

417AL

451BL

Total access time :

451BR 461BL 0.00 Hrs

461BR

Skills :

3.00 MHrs

1 EN 410 420

361141-04-1

REM

ENGINE BLEED AIR SUPPLY

I

10 000 FH

REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.40 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [2 / 7] ATA

: 36


36

PNEUMATIC

Task Number

Zone

361143-01-1

450 460

Task Title

Task code

REM

ENGINE BLEED AIR SUPPLY REMOVE THE FILTER OF THE FAN AIR VALVE-CONTROL THERMOSTAT FOR CLEANING. NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. NOTE: ETOPS PARALLEL SYSTEM

Threshold Interval

I

6 000 FH See note

References

Ctrl

N

AMM 361143-100-801 SIL 36-055

Access panels :

452CL

462CR

Total access time :

0.86 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [3 / 7] ATA

: 36

Eff ALL


36

PNEUMATIC

Task Number

Zone

361148-03-1

520 620

Task code

Task Title

CHK

WING BLEED AIR DUCTING

Threshold Interval

Ctrl

See note

N

AMM 361148-790-801 SIL 36-049

ALL

Check : 4C

PERFORM LEAK CHECK ON BLEED AIR DUCTING IN THE WING AREA BETWEEN BLEED AIR PRECOOLER, WING ANTI ICE VALVES AND WING/FUSELAGE CONNECTION NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR´S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED PREP. : SLATS EXTENDED; NOTE: ETOPS PARALLEL SYSTEM

References

Eff

Access panels :

521AB 522AB 621FB

521BB 522BB 621GB

Total access time :

521CB 522CB 621JB

521DB 621AB 622AB

521FB 621BB 622BB

521GB 621CB 622CB

521JB 621DB

0.60 Hrs

Skills :

2.00 MHrs

1 AF 210

361155-01-1

ENGINE AIR BLEED SUPPLY

OP

I

10 000 FH

N

AMM 361100-710-822

ALL

OP

I

3 600 CY

N

ALL

I

50 MO

AMM 361200-710-802 CMP 36-2-0000-004

OPERATIONAL CHECK OF CLOSING SIGNAL TO ISOLATION SOLENOID FROM FIRE P/B SW. 210

361200-01-3

APU BLEED AIR VALVE AND CROSSBLEED OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM Skills :

0.10 MHrs

1 EN Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [4 / 7] ATA

: 36


36

PNEUMATIC

Task Number

Zone

361241-01-2

100 300

Task Title

Task code

CHK

APU BLEED AIR SUPPLY PERFORM LEAK CHECK ON APU BLEED AIR DUCTING (UPSTREAM THE APU BLEED CHECK VALVE) NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR´S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED PREP. : BELLY FAIRING PANELS Z191; BELLY FAIRING PANELS Z195; BELLY FAIRING PANELS Z197; SIDEWALL LININGS Z151; SIDEWALL LININGS Z161; NOTE: ETOPS PARALLEL SYSTEM

Threshold Interval

Ctrl

See note

N

References

AMM 361200-790-801

Check : 4C

Access panels :

151EW

151GW

Total access time :

151JW 151RW 0.00 Hrs

151TW

Skills :

1.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [5 / 7] ATA

: 36

Eff ALL


36

PNEUMATIC

Task Number

Zone

361242-01-1

191 192 193

Task Title

BLEED AIR SUPPLY AND CROSSBLEED DUCTING

Task code

CHK

Threshold Interval

Ctrl

See note

N

AMM 361242-790-801

ALL

N

AMM 361242-000-802 SIL 36-049

275

References

Eff

Check : 4C

PERFORM LEAK CHECK ON BLEED AIR DUCTING IN THE FUSELAGE AREA BETWEEN THE APU BLEED CHECK VALVE, AIR CONDITIONING PACK AND WING/FUSELAGE CONNECTION NOTE : DEPENDING ON OPERATING ENVIRONMENT ANDATOR´S OPERATOR´S EXPERIENCE, A LESS OR MORE FREQUENTTERVAL INITIAL INTERVAL MAY BE USED. NOTE: ETOPS PARALLEL SYSTEM Access panels :

191FB

192GB

Total access time :

193AB 0.00 Hrs

Skills :

3.00 MHrs

1 EN 191 192 193

361242-02-1

Issue No

:

Date

:

10 01/12/2013

BLEED AIR SUPPLY AND CROSSBLEED DUCTING REMOVE AND REPLACE COMBO SEALS ON THE PACK INLET, ON SLEEVES DOWNSTREAM AND UPSTREAM OF THE FCV NOTE: - TASK MAY BE COMBINED WITH TASK 215000-12-1 - DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR'S EXPERIENCE, A LESS OR MORE FREQUENT INITIAL INTERVAL MAY BE USED

Amendment No Date

: 01 : 06/09/2014

DIS

I

36 MO

294 299 366

Page : SYS - 36 [6 / 7] ATA

: 36


36

PNEUMATIC

Task Number

Zone

361251-01-3

193

Task Title

Task code

DVI

APU BLEED CHECK VALVE

Threshold Interval

I

8 500 FH

References

Ctrl

N

AMM 361251-200-803

Eff 275 294

REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION NOTE: ETOPS PARALLEL SYSTEMS

299 366

Access panels :

191FB Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 EN R

193

361251-01-4

APU BLEED CHECK VALVE

DI

I

10 000 CY

N

AMM 361251-200-803

943 946

REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION TASK APPLICABLE BEFORE 361251-01-3 NOTE: ETOPS PARALLEL SYSTEM

962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 36 [7 / 7] ATA

: 36


38

WATER / WASTE

Task Number

Zone

381000-VNA-1

100

Task Title

Task code

FUC

POTABLE WATER

100 200

POTABLE WATER DISINFECT POTABLE WATER SYSTEM

I

1 600 FH

References

Ctrl

Eff

N

AMM 381000-790-801

ALL

N

AMM 381000-670-801

ALL

Check : 2A

LEAK CHECK OF THE FILL/OVERFLOW/DRAIN VALVES 9MA AND 22MA NOTE: PERFORM ADDITIONAL VISUAL INSPECTION TO THE VALVE 9MA AND CABLE CONTROL ASSY 381000-01-1

Threshold Interval

DIS RS

I

DIS

I

3 MO

N

AMM 381223-920-802

946

DIS

I

3 MO

N

AMM 381223/3 AMT 381223-920-803

943

3 MO See note

Access panels :

133BL

154AR

Total access time :

164AR 0.00 Hrs

Skills :

1.50 MHrs

1 UT R

200

381000-02-1

POTABLE WATER DISCARD WATER FILTER CARTRIDGE OF THE LAVATORIES Skills :

1.60 MHrs

1 UT R

200

381000-03-1

POTABLE DISCARD WATER FILTER CARTRIDGE OF THE GALLEYS NOTE: IF WATER FILTER OF THE GALLEY INSTALLED

946 962 1019 1256 1266

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 38 [1 / 5] ATA

: 38


38

WATER / WASTE

Task Number

Zone

381000-04-1

154 164

Task Title

POTABLE WATER

Task code

Threshold Interval

DIS

Check : 1C

References

Ctrl

N

OPERATIONAL CHECK OF FILL/DRAIN OVERFLOW VALVE FOR LEAKAGE

AMM 381000-710-805 ISB 38-3039

Eff 275 294 299 366

Skills :

3.50 MHrs

1 AF 200

383100-01-1

SER

VACUUM TOILET SYSTEM

See note

N

AMM 383100-100-809

ALL

N

AMM 383100-100-803

ALL

N

AMM 383147-100-801

ALL

Check : 1C

CLEAN THE TOILET ASSEMBLIES SPRAY RING NOTE: INTERVAL MAY BE ADJUSTED ACCORDING TO OPERATOR EXPERIENCE Skills :

0.50 MHrs

1 UT 170 200

383100-02-1

VACUUM TOILET SYSTEM HIGH PRESSURE CLEANING OF THE WASTE LINES NOTE: INTERVAL MAY BE ADJUSTED ACCORDING TO OPERATOR EXPERIENCE

SER RS

I

8 500 FH

I

24 MO

REM

I

3 200 FH

Skills :

1.00 MHrs

1 UT 170

383100-03-1

TOILET SYSTEM DISCARD WATER SEPARATOR. PREP. : TOILET SYSTEM DISINFECTED; TOILET SYSTEM DRAINED AND FLUSHED;

Check : 4A

Skills :

0.50 MHrs

1 UT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 38 [2 / 5] ATA

: 38


38

WATER / WASTE

Task Number

Zone

383100-04-1

200

Task Title

Task code

SER

TOILET SYSTEM

Threshold Interval

I

350 FH

References

Ctrl

Eff

N

AMM 383100-100-812

ALL

N

AMM 383100-100-808 MRB 38.31.00/05 SIL 38-028

ALL

N

AMM 383147-100-802

ALL

Check : WY

CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING AGENT AND CRUSHED ICE. PREP. : TOILET SYSTEM DRAINED AND FLUSHED; Skills :

6.00 MHrs

1 UT 170

383100-05-1

RS

TOILET SYSTEM CLEANING OF LIQUID LEVEL SENSORS, WASTE TANKS AND WASTE DRAIN LINES. PREP. : TOILET SYSTEM DISINFECTED; TOILET SYSTEM DRAINED AND FLUSHED;

I

10 000 FH

I

24 MO

I

3 200 FH

Skills :

1.00 MHrs

1 UT 170

383100-06-1

SER

TOILET SYSTEM REMOVE FILTER OF POLAR CAP ASSY FOR CLEANING. PREP. : TOILET SYSTEM DISINFECTED; TOILET SYSTEM DRAINED AND FLUSHED;

Check : 4A

Skills :

1.50 MHrs

1 UT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 38 [3 / 5] ATA

: 38


38

WATER / WASTE

Task Number

Zone

383100-07-1

170

Task Title

Task code

RS

TOILET SYSTEM

Threshold Interval

I

3 200 FH

References

Ctrl

Eff

N

AMM 383157-100-802

ALL

N

AMM 383200/7 AMT 383200-100-804

ALL

N

AMM 384100-920-801

ALL

Check : 4A

CLEANING OF RINSE NOZZLES AND REFERENCE PRESSURE LINE OF LIQUID LEVEL TRANSMITTER. PREP. : TOILET SYSTEM DISINFECTED; TOILET SYSTEM DRAINED AND FLUSHED; Access panels :

161XW

162ZW

Total access time :

823 0.54 Hrs

Skills :

2.00 MHrs

1 AF 200

383242-01-1

WASTE WATER DRAIN

CLN

I

DIS

Check : 4C

600 FH

CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE Skills :

0.25 MHrs

1 AF 152

384142-01-1

AIR SUPPLY SYSTEM DISCARD SYSTEM FILTER ELEMENT Access panels :

152JW Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 38 [4 / 5] ATA

: 38


38

WATER / WASTE

Task Number

Zone

384200-01-1

172

Task Title

AIR SUPPLY SYSTEM

Task code

Threshold Interval

DIS

I

DIS

Check : 4C

20 000 FH

References

Ctrl

Eff

N

AMM 384200-200-801

ALL

N

AMM 384200-920-801

ALL

DETAILED INSPECTION OF COMPRESSOR INLET FILTER Access panels :

162ZW Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 CA 172

384242-01-1

AIR SUPPLY SYSTEM DISCARD COMPRESSOR OUTLET FILTER ELEMENT Access panels :

162ZW Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 38 [5 / 5] ATA

: 38


47


Task Number

Zone

470000-01-1

191

Task Title

INERT GAS SYSTEM

Task code

DIS

Threshold Interval

I

7 000 FH

References

Ctrl

N

AMM 471041-920-801

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

1256 1266

DISCARD FILTER ELEMENT

Issue No

Eff

Page : SYS - 47 [1 / 1] ATA

: 47


49

AIRBORNE AUXILLIARY POWER UNIT

Task Number

Zone

491200-01-1

315

Task Title

APU MOUNTS

Task code

Threshold Interval

References

Ctrl

Eff

GVI

I

10 000 FH

N

AMM 491200-200-801

ALL

GVI

I

12 000 FH

N

AMM 491300-200-801

ALL

GVI

I

10 000 FH

N

AMM 491700-210-801 MRB 49.17.00/02-35

ALL

GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM INCLUDING SHOCKMOUNT STRUCTURE AND BRACKETS Access panels :

315AL

316AR

Total access time :

0.00 Hrs

Skills :

0.33 MHrs

1 EN 310

491300-01-1

FIRE SEALS GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE SEALS, WALLS INCLUDING FORWARD, AFT, UPPER, SIDES AND COMPARTMENT DOORS. Access panels :

315AL

316AR

Total access time :

0.08 Hrs

Skills :

0.20 MHrs

1 AF 310

491700-02-1

POWERPLANT DRAIN SYSTEM GENERAL VISUAL INSPECTION OF DRAIN PIPES.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 49 [1 / 5] ATA

: 49


49


Task Number

Zone

493100-01-3

310

Task Title

Task code

VCK

APU FUEL DISTRIBUTION VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR BUTTON ON FUEL FILTER NOTE : - TASK TO BE ACCOMPLISHED AT 150FH, 400FH, AND 800FH AFTER AIRCRAFT DELIVERY. THEREAFTER EVERY 1000 AH. - TASK TO BE ACCOMPLISHED AT 150FH AND 400FH AFTER MAJOR TANK REPAIR. THEREAFTER EVERY 1000AH. NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

Threshold Interval

T

150 FH

I

1 000 AH

References

Ctrl

Eff

N

AMM 493241-210-801 CMP 49-2-2003-002

ALL

N

AMM 496200-710-801

ALL

Skills :

0.10 MHrs

1 EN 210

496200-01-1

OP

EMERGENCY SHUTDOWN OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING APU STOP SWITCH 1KL NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 496200-02-1 NOTE: ETOPS PARALLEL SYSTEM

See note Check : 2C

Access panels :

121EL Total access time :

0.01 Hrs

Skills :

0.33 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 49 [2 / 5] ATA

: 49


49


Task Number

Zone

496200-02-1

210

Task Title

EMERGENCY SHUTDOWN

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 2C

N

AMM 496200-710-803

ALL

DI

I

N

AMM 498145-210-802

ALL

OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING APU STOP SWITCH 1KL NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 496200-01-1 NOTE: ETOPS PARALLEL SYSTEM Access panels :

198DB Total access time :

0.00 Hrs

Skills :

0.33 MHrs

1 EN 310

498100-01-1

APU EXHAUST

20 000 FH

DETAILED INSPECTION OF SEALING RING COUPLING AND BELLOWS Access panels :

315AL

316AR

Total access time :

0.00 Hrs

Skills :

0.50 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 49 [3 / 5] ATA

: 49


49


Task Number

Zone

498100-02-1

310

Task Title

APU EXHAUST

Task code

Threshold Interval

References

Ctrl

Eff

DI

I

10 000 FH

N

AMM 498145-210-801

ALL

VCK

I

500 AP

N

AMM 499141-210-801 CMP 49-2-2003-003 CMP 49-2-2003-004

ALL

DETAILED INSPECTION OF V-CLAMP, EXHAUST DUCT AND EXHAUST DUCT HEAT INSULATION. Access panels :

315AL

316AR

Total access time :

317AL 0.00 Hrs

Skills :

0.33 MHrs

1 EN 310

499100-01-2

APU OIL SYSTEM CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON - ON LUBE FILTER - ON GENERATOR SCAVENGE FILTER. NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM RECORD APU HOUR AND CYCLE - APU HOUR: - APU CYCLE:

Check : WY

Access panels :

315AL

316AR

Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 49 [4 / 5] ATA

: 49


49


Task Number

Zone

499100-03-1

310

Task Title

APU OIL SYSTEM

Task code

Threshold Interval

Ctrl

References

Eff

DI

I


N

AMM 242351-210-801 SIL 24-079

ALL

DI

I

N

AMM 499141-210-808 SIL 24-079

ALL

DETAILED INSPECTION OF APU GENERATOR DRAIN PLUG FOR DETECTION OF METALLIC DEBRIS. NOTE: WHICHEVER OCCURS LATER. NOTE: ETOPS PARALLEL SYSTEM Access panels :

315AL

316AR

Total access time :

0.08 Hrs

Skills :

0.75 MHrs

1 EN 310

499100-05-1

APU OIL SYSTEM DETAILED INSPECTION OF APU GENERATOR SCAVENGE OIL FILTER ELEMENT AND HOUSING FOR DETECTION OF MAGNETIC METALLIC DEBRIS. NOTE: WHICHEVER OCCURS LATER. NOTE: ETOPS PARALLEL SYSTEM


Access panels :

315AL

316AR

Total access time :

0.08 Hrs

Skills :

0.75 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 49 [5 / 5] ATA

: 49


52

DOORS

Task Number

Zone

521000-01-1

831 832 833 841 842 843

Task Title

PASSENGER/CREW DOORS

Task code

Threshold Interval

References

Ctrl

Eff

FUC

I

48 MO

N

AMM 521000-720-801

ALL

OP

I

48 MO

N

AMM 521000-710-804

ALL

OP

Check : 1C

N

AMM 521000-710-802

ALL

FUNCTIONAL CHECK OF LOCKING MECHANISM NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT EMERGENCY EXIT. REFER TO MPD 522200-02-1 Skills :

3.00 MHrs

1 AF 831 832 833 841 842 843

521000-02-1

PASSENGER/CREW DOORS OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR IS OPENED FROM OUTSIDE

Skills :

1.80 MHrs

1 AF 831 832 833 841 842 843

521000-03-1

PASSENGER/CREW DOORS OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN POSITION NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT EMERGENCY EXIT. REFER TO MPD 522200-01-1 Skills :

1.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [1 / 10] ATA

: 52


52

DOORS

Task Number

Zone

521000-04-1

831 832 833 841 842 843

Task Title

Task code

OP

PASSENGER/CREW DOORS

Threshold Interval

References

Ctrl

Eff

Check : 4C

N

AMM 521000-710-805

ALL

FUC

I

N

AMM AOT EAD FAD

521000-200-805 52A3063 2010-0135 2011-09-06

ALL

LUB

Check : 1C

N

AMM 122252-600-802

ALL

OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS OPEN Skills :

1.80 MHrs

1 AF R

831 832 833 841 842 843

521000-07-1

PASSENGER/CREW DOOR

18 MO

FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR SLIDER MECHANISM.

Skills :

4.50 MHrs

1 AF 831 832 833 841 842 843

521121-01-1

PASSENGER/CREW DOORS LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL HANDLE NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGER COMPARTMENT EMERGENCY EXIT. REFER TO MPD 522200-03-1 Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [2 / 10] ATA

: 52


52

DOORS

Task Number

Zone

522200-01-1

834 844

Task Title

PASSENGER COMPARTMENT EMERGENCY EXIT

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

24 MO

N

AMM 522200-710-801

ALL

FUC

I

48 MO

N

AMM 522200-720-801

ALL

LUB

I

24 MO

N

AMM 122252-600-807

ALL

OP

Check : 1C

N

AMM 522200-710-802

ALL

OPERATIONAL CHECK OF DOOR UNLOCKING/LOCKING AND DOOR OPENING/CLOSING FROM INSIDE AND OUTSIDE AND DOOR LATCHING IN FULLY OPEN POSITION Skills :

0.20 MHrs

1 AF 834 844

522200-02-1

PASSENGER COMPARTMENT EMERGENCY EXIT FUNCTIONAL CHECK OF LOCKING MECHANISM Skills :

0.40 MHrs

1 AF 834 844

522200-03-1

PASSENGER COMPARTMENT EMERGENCY EXIT LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL HANDLE Skills :

0.40 MHrs

1 LU 834 844

522200-04-1

PASSENGER COMPARTMENT EMERGENCY EXIT OPERATIONAL CHECK OF DOOR DAMPING, ESCAPE SLIDE RELEASE MECHANISM DISARMING, AND TO ENSURE THAT DOOR CANNOT BE LOWERED AND LOCKED WHEN OPEN Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [3 / 10] ATA

: 52


52

DOORS

Task Number

Zone

522200-05-1

834 844

Task Title

PASSENGER COMPARTMENT EMERGENCY EXIT

Task code

Threshold Interval

OP

I

OP

References

Ctrl

Eff

N

AMM 522200-710-803

ALL

Check : 4C

N

AMM 522200-710-804

ALL

I

N

AMM AOT EAD FAD

ALL

48 MO

OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR IS OPENED FROM OUTSIDE Skills :

0.60 MHrs

1 AF 834 844

522200-06-1

PASSENGER COMPARTMENT EMERGENCY EXIT OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS OPEN Skills :

0.20 MHrs

1 AF R

834 844

522200-09-1

PASSENGER COMPARTMENT EMERGENCY EXIT FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR SLIDER MECHANISM.

FUC

18 MO

522200-200-805 52A3063 2010-0135 2011-09-06

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [4 / 10] ATA

: 52


52

DOORS

Task Number

Zone

523100-01-1

821

Task Title

FWD CARGO COMPARTMENT DOOR

Task code

Threshold Interval

LUB

Check : 1C

N

AMM 122252-600-801

ALL

FUC

Check : 4C

N

AMM 523100-720-801

ALL

References

Ctrl

Eff

LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING -, LATCHING - AND INTERLOCK MECHANISM Access panels :

132AR 132HR 821DR

132BR 132JR

Total access time :

132CR 132KR

132DR 132LR

132ER 821AR

132FR 821BR

132GR 821CR

0.00 Hrs

Skills :

0.50 MHrs

1 AF 821

523100-02-1

FWD CARGO COMPARTMENT DOOR FUNCTIONAL CHECK OF : - LATCHING AND LOCKING HANDLE FORCES, - OVERCENTER POSITIONS, - WEAR OF LATCHING AND LOCKING MECHANISM, - ADJUSTMENT OF INTERLOCK MECHANISM NOTE: RII TASK Access panels :

821AR

821BR

Total access time :

821CR

821DR

0.00 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [5 / 10] ATA

: 52


52

DOORS

Task Number

Zone

523200-01-1

822

Task Title


Task code

Threshold Interval

LUB

Check : 1C

N

AMM 122252-600-808

ALL

FUC

Check : 4C

N

AMM 523200-720-801

ALL

References

Ctrl

Eff

LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING -, LATCHING - AND INTERLOCK MECHANISM Access panels :

152AR 152HR 822DR

152BR 152JR

Total access time :

152CR 152KR

152DR 152LR

152ER 822AR

152FR 822BR

152GR 822CR

0.00 Hrs

Skills :

0.50 MHrs

1 LU 822

523200-02-1

AFT CARGO COMPARTMENT DOOR FUNCTIONAL CHECK OF : - LATCHING AND LOCKING HANDLE FORCES, - OVERCENTER POSITIONS, - WEAR OF LATCHING AND LOCKING MECHANISM, - ADJUSTMENT OF INTERLOCK MECHANISM NOTE: RII TASK Access panels :

822AR

822BR

Total access time :

822CR

822DR

0.00 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [6 / 10] ATA

: 52


52

DOORS

Task Number

Zone

523300-01-1

823

Task Title

BULK CARGO COMPARTMENT DOOR

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 523311-710-801

ALL

LUB

Check : 1C

N

AMM 122252-600-803

ALL

I

N

AMM 524200/6 ISB 52-3077

275

OPERATIONAL CHECK OF DOOR BALANCE MECHANISM AND OF DOOR LATCHING IN FULLY OPEN POSITION Skills :

0.10 MHrs

1 AF 823

523300-03-1

BULK CARGO COMPARTMENT DOOR LUBRICATION OF BULK CARGO COMPARTMENT DOOR COMPONENTS Skills :

0.30 MHrs

1 AF 150

524000-01-1

POTABLE WATER SERVICE DOOR

DI

1 200 FH

DETAILED INSPECTION OF HINGES OF THE POTABLE WATER SERVICE DOOR 154AR FOR WEAR. NOTE: REFER TO ISB 52-3077 FOR THRESHOLD AND INTERVAL

294 299 366

Access panels :

154AR

164AR

Total access time :

171AL 0.00 Hrs

Skills :

0.00 MHrs

1 AF 220

525111-02-1

DI

COCKPIT DOOR

I

48 MO

N

AMM 525100-200-801

DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR LOCKING SYSTEM Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [7 / 10] ATA

: 52

ALL


52

DOORS

Task Number

Zone

525111-03-1

220

Task Title

COCKPIT DOOR

Task code

Threshold Interval

References

Ctrl

Eff

OP

I

48 MO

N

AMM 525100-710-805

ALL

DI

I

42 MO

N

AMM 256800-220-801

275

OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS FOR RAPID DECOMPRESSION, CHECK OF DOOR OPENING IN CASE OF POWER OFF AND BY USING THE EMERGENCY CODE Skills :

1.00 MHrs

1 AF 220

525111-05-1

COCKPIT DOOR

294

DETAILED INSPECTION OF FLAP BELLOW

299 366

Skills :

0.50 MHrs

1 AF R

220

525111-07-1

OP

COCKPIT DOOR

I

72 MO

N

AMM 256800-710-805

943 946

OPERATIONAL CHECK OF FLAP RELEASE MECHANISM (MANUAL OPENING).

962 1019 1256 1266

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [8 / 10] ATA

: 52


R

52

DOORS

Task Number

Zone

525111-08-1

220

Task Title

Task code

GVI

COCKPIT DOOR

Threshold Interval

I

72 MO

References

Ctrl

N

AMM 256800-210-803

Eff 943 946

GENERAL VISUAL INSPECTION OF AIR CYLINDER OF DECOMPRESSION PANEL.

962 1019 1256 1266

Skills :

0.10 MHrs

1 AF 210

527100-01-1

OP

Check : 4C

N

AMM 527100-710-801

ALL

OP

I

N

AMM 527100-710-802

ALL

DOOR AND ESCAPE SLIDE CONTROL

OP

Check : 4C

N

AMM 527100-710-803

ALL

OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING SYSTEM AND FUNCTIONAL CHECK OF ASSOCIATED PRESSURE SWITCH

FUC

DOOR WARNING SYSTEM OPERATIONAL CHECK OF DOOR WARNING SYSTEM Skills :

0.50 MHrs

1 AF 210

527100-02-1

DOOR AND ESCAPE SLIDE RELEASE CONTROL

48 MO

OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE WARNING SYSTEM Skills :

0.50 MHrs

1 AF 100 120 200

527100-03-1

Skills :

2.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [9 / 10] ATA

: 52


52

DOORS

Task Number

Zone

527100-04-1

210

Task Title

DOOR AND ESCAPE SLIDE CONTROL

Task code

Threshold Interval

References

Ctrl

Eff

FUC

I

8 MO

N

AMM 527100-740-803

ALL

OP

I

3 200 FH

N

AMM 527100-740-804

ALL

CHECK BATTERY CAPACITY OF AUTONOMOUS STANDBY POWER SUPPLY UNIT (ASPSU) NOTE: AS AN ALTERNATIVE, TASK MAY BY ACCOMPLISHED BY REPLACING BATTERIES BY FULLY-CHARGED UNITS (REF. AMM 527136/4, 52-71-36-000-802) AND SENDING REMOVED BATTERIES TO WORKSHOP. Skills :

0.10 MHrs

1 AF 210

527100-07-1

DOOR AND ESCAPE SLIDE CONTROL BITE TEST OF AUTONOMOUS STANDBY POWER SUPPLY UNIT (ASPSU)

Check : 4A

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 52 [10 / 10] ATA

: 52


53

FUSELAGE

Task Number

Zone

531900-01-1

100

Task Title

FUSELAGE DRAINS

Task code

Threshold Interval

VCK

Check : 1C

N

AMM 530000-200-801

ALL

OP

Check : 1C

N

AMM 530000-200-802

ALL

SDI

T

12 YE

N

AMM 532100-200-814

ALL

I

12 YE

References

Ctrl

Eff

OPERATIONAL CHECK OF DRAIN HOLES IN LOWER PART OF FR1 AND FR80 (FROM INSIDE). Access panels :

121AF

162ZW

Total access time :

811 823 0.00 Hrs

Skills :

0.30 MHrs

1 AF 100

531900-02-1

FUSELAGE DRAINS OPERATIONAL CHECK OF DRAIN HOLES IN UNPRESSURIZED PART OF FUSELAGE (IN RADOME, FORWARD OF FR1, BEHIND REAR PRESSURE BULKHEAD, IN BELLY FAIRING, TAIL CONE AND IN CARGO COMPARTMENT DOORS). Skills :

0.20 MHrs

1 AF 233 234

532136-01-1

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN UNDERNEATH ACOUSTIC INSULATION PANELS FROM FR 18 TO FR 32, BETWEEN STR 3 AND CROWN CENTER LINE, LH/RH AND - BETWEEN STR 7 TO STR 17, LH/RH. NOTE: CPCP Skills :

3.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 53 [1 / 3] ATA

: 53


53

FUSELAGE

Task Number

Zone

532900-01-1

100 821 822

Task Title

FUSELAGE DRAINS OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES IN LOWER FUSELAGE SHELL (FROM OUTSIDE) AND IN FWD AND AFT CARGO COMPARTMENT DOORS.

Task code

Threshold Interval

VCK OP

Check : 1C

N

AMM 530000-200-803

ALL

GVI

Check : 4C

N

AMM 530000-200-804

ALL

References

Ctrl

Eff

Skills :

0.50 MHrs

1 AF 100

532900-02-1

FUSELAGE DRAINS GENERAL VISUAL INSPECTION OF HOLES OF PISTON TYPE DRAIN OR PRESSURE DRAIN VALVES AND PRESSURE SEAL DRAINS FROM INSIDE (IN FUSELAGE BILGE AREA, AT UPPER AFT END OF CENTER WING BOX AND IN CARGO COMPARTMENT DOORS). PREP. : FLOOR PANELS Z120; FLOOR PANELS Z130; FLOOR PANELS Z150; FLOOR PANELS Z160; FLOOR PANELS Z250; INSULATION Z821; INSULATION Z822; LD-MCR IF INSTALLED; LINING Z821; LINING Z822; Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 53 [2 / 3] ATA

: 53


53

FUSELAGE

Task Number

Zone

533900-01-1

140

Task code

Task Title

FUSELAGE DRAINS

Threshold Interval

References

Ctrl

Eff

OP

Check : 1C

N

AMM 533900-200-801

ALL

OP

Check : 1C

N

AMM 530000-200-805

ALL

DI

T

6 YE

N

AMM 535100-200-815

ALL

I

6 YE

I

5 MO

N

AMM 530000/6 AMT 530000-200-806

ALL

OPERATIONAL CHECK OF ( RUBBER FLAP ) PRESSURE SEAL DRAIN AT UPPER AFT END OF CENTER WING BOX (FROM MAIN LANDING GEAR BAY). Skills :

0.10 MHrs

1 AF 823

534900-01-1

BULK CARGO DOOR OPERATIONAL CHECK OF (RUBBER FLAP) PRESSURE SEAL DRAIN OF BULK CARGO DOOR (FROM OUTSIDE) Skills :

0.10 MHrs

1 AF 321 323

535116-01-2

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD FITTINGS Access panels :

321AL

323CL

Total access time :

323CR

323DL

323DR

325LL

325LR

0.00 Hrs

Skills :

1.00 MHrs

1 AF 310

535900-01-1

OP

REAR FUSELAGE DRAIN OPERATIONAL CHECK OF DRAIN MAST AFT OF FR80 Skills :

0.10 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 53 [3 / 3] ATA

: 53


54

NACELLES / PYLONS

Task Number

Zone

545100-03-1

450 460

Task code

Task Title

NACELLE/PYLON DRAIN

Threshold Interval

References

Ctrl

Eff

OP

Check : 2C

N

AMM 545000-200-813

ALL

DI

I

42 MO

N

AMM 545000-220-807

ALL

SDI

I

42 MO

N

AMM 545000-290-807

ALL

OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND F AND OF HYDRAULIC AND FUEL PAN DRAIN SYSTEM Access panels :

415AL 428AR 454KL 464KL

416AR 451DL 461DL

Total access time :

417AL 452CR 462CR

418AR 453BL 463BL

425AL 453CL 463CL

426AR 454BL 464BL

427AL 454DL 464DL

0.00 Hrs

Skills :

0.60 MHrs

1 AF 545100-06-1

545100-09-1

Issue No

:

Date

:

450 460

NACELLE/PYLON DRAIN (PW 4000)

450 460

NACELLE/PYLON DRAIN (PW 4000)

10 01/12/2013

DETAILED INSPECTION OF COMPARTMENT A AND F DRAIN LINE WITH LAPF REMOVED. NOTE: - THIS TASK IS AN ALTERNATIVE TASK TO 545100-09-1

SPECIAL DETAILED (BOROSCOPE) INSPECTION OF COMPARTMENT A AND F DRAIN LINE WITH LAPF INSTALLED. NOTE: - THIS TASK IS AN ALTERNATIVE TASK TO 545100-06-1

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 54 [1 / 2] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545611-01-1

450 460

Task code

Task Title

DI

PYLON/NACELLE

Threshold Interval

Check : 1C

References

Ctrl

N

GENERAL VISUAL INSPECTION OF THE LOWER AFT PYLON FAIRING (LAPF) ASSEMBLY FOR CRACKS AND SEAL DETERIORATION. NOTE: FOR THRESHOLD/INTERVAL, REFER TO ISB PW4G-100-54-03

AMM 545600-210-801 VSB PW4G-100-54-03

Eff 275 294 299 366

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

2.00 MHrs

1 AF 450 460

545611-02-1

DI

NACELLE/PYLONS DETAILED INSPECTION OF THE LOWER AFT PYLON FAIRING (LAPF) FIREWALL FOR CRACKS NOTE: FOR THRESHOLD/INTERVAL, REFER TO AD 2006-10-13

I

1 000 FH

N

AMM EAD FAD ISB VSB

545600-200-804 F-2004-028R2 2006-10-13 54-3021 PW4G-100-54-05

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 54 [2 / 2] ATA

: 54

275 294 299 366


D

55

STABILIZERS

Task Number

Zone

551028-01-4

333 343

Task Title

Task code

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE FAIRINGS

Threshold Interval

References

Ctrl

N

AMM 551100-200-811

Eff 943

T

60 000 FH

T

17 000 CY

962

I

9 800 FH

1019

I

1 500 CY

1256 1266

Skills :

0.00 MHrs

1 AF 333 343

551028-01-8

R

310

551600-01-1

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE FAIRINGS NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-8 NOTE: APPLY TASK 551028-02-8

LUBRICATION OF THS HINGE LINE BEARINGS

60 000 FH

T

20 000 CY

I

9 000 FH

N

AMM 551100-200-811

275

N

AMM 122253-600-801

ALL

I


LUB

THS ATTACH FITTINGS

T

I

10 000 FH

I

24 MO

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 55 [1 / 2] ATA

: 55


55

STABILIZERS

Task Number

Zone

551600-02-1

310

Task Title

Task code

LUB

THS ATTACH FITTINGS LUBRICATION OF UPPER AND LOWER FRAME ATTACHMENT BEARINGS

Threshold Interval

I

10 000 FH

I

24 MO

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 122253-600-802

ALL

N

AMM 553000-210-815

943

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF R

300

553020-01-1

GVI

VERTICAL STABILIZER GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SKIN PANELS FROM FRONT TO REAR SPAR AND FROM FIN/FUSELAGE FAIRING TO TOP, EXTERNAL SURFACE LH/RH.

946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 323

553024-01-1

VERTICAL STABILIZER DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

T

6 YE

I

6 YE

N

AMM 553000-210-805

275 294 299 366

Page : SYS - 55 [2 / 2] ATA

: 55


56

WINDOWS

Task Number

Zone

561000-01-1

210

Task Title

Task code

DVI

COCKPIT WINDOWS

Threshold Interval

I

800 FH

Eff

N

AMM 561000/6 AMT 561000-200-801 SIL 56-017

ALL

N

AMM 561000-200-802 SIL 56-017

ALL

N

AMM 561200-200-801

ALL

Check : 1A

DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROM INSIDE.

References

Ctrl

Skills :

0.30 MHrs

1 AF 210

561000-02-1

COCKPIT WINDOWS

DVI

I

DVI

Check : 2C

18 MO

DETAILED INSPECTION OF -FRONT WINDSHIELD WEATHER SEAL -SIDE WIMDOWS BONDING STRIP RECOVERING SEAL -FRONT WINDSHIELD IN AREA OF BUS BAR FOR BURN SPOTS Skills :

0.30 MHrs

1 AF 210

561200-01-1

SLIDING WINDOWS DETAILED INSPECTION OF WINDOW SEALS

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 56 [1 / 1] ATA

: 56


57

WINGS

Task Number

Zone

572900-01-1

540 640

Task Title

SLAT TRACK CANS DRAIN

Task code

Threshold Interval

References

Ctrl

Eff

OP

Check : 4C

N

AMM 572900-210-801

ALL

OP

Check : 4C

N

AMM 573900-210-801

ALL

OP

Check : 4C

N

AMM 57-59-00-210-801 AMM 575900-210-801

ALL

OPERATIONAL CHECK OF DRAIN HOSES AND DESIGNATED DRAIN HOLES FOR CLOGGING Skills :

0.60 MHrs

1 AF 535 635

573900-01-1

WING TIP DRAIN OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING Skills :

0.60 MHrs

1 AF 500 600

575900-01-1

WING TRAILING AND LEADING EDGES DRAIN OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 57 [1 / 1] ATA

: 57


71


Task Number

Zone

711300-P1-1

411 421

Task Title

Task code

DI

FAN COWL

Threshold Interval

References

Ctrl

Eff

Check : 1C

N

AMM 716100-220-801

ALL

I

N

AMM 711300-720-802

ALL

N

AMM EAD FAD ISB VSB

712111-210-803 2012-0094 2006-16-05 71-3028 PW4G-100-A71-32

ALL

N

SB

PW4G-100-71-10

ALL

DETAILED INSPECTION OF AIR INTAKE COWL LIP AND INNER SKIN Skills :

0.00 MHrs

1 EN 410 420

711300-P4-1

FUC

FAN COWL

24 MO

Check : C1

FUNCTIONAL CHECK OF FAN COWL LATCH TENSIONS Skills :

0.60 MHrs

1 AF 413 423

712101-P6-1

CHK

FORWARD ENGINE MOUNT TORQUE CHECK OF THE FORWARD ENGINE MOUNTING BOLT (MP159) 1000 LBF-IM (112.985) NOTE : IF ANY OF THE FOUR BOLTS MOVE, ALL FOUR BOLTS MUST BE REPLACED REF: AD2000-16-02R1; DN 01-20-01-E2; PW4G-100-A71-20

I

24 320 FH

I

2 350 CY

Skills :

1.00 MHrs

1 AF 411 421

716100-P1-1

Issue No

:

Date

:

10 01/12/2013

AIR INTAKE COWL

DI

Check : 1C

INSPECTION/REPAIR OF INTAKE COWL ASSEMBLY OUTER BARREL RIBS NOTE: TASK APPLY FOR A/C INSTALL INTAKE COWL S/N FROM C9A2AH007 TO C9A2AH088 (I.A.W VSB PW4G-100-71-10)

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 71 [1 / 1] ATA

: 71


72

ENGINE

Task Number

Zone

723100-P1-1

410 420

Task Title

LOW PRESSURE COMPRESSOR

Task code

Threshold Interval

References

Ctrl

Eff

VCK

I

2 100 FH

N

AMM 723112-200-801

ALL

DVI

I

3 200 FH

N

AMM 723111-210-801

ALL

DETAILED INSPECTION OF FAN BLADES NOTE: ETOPS PARALLEL SYSTEM Skills :

0.50 MHrs

1 EN 723100-P4-1

723112-P1-1L

410 420

LOW PRESSURE COMPRESSOR

410

LOW PRESSURE COMPRESSOR (LPC)

Check : 4A

DETAILED INSPECTION OF INLET CONE NOTE: ETOPS PARALLEL SYSTEM LUB

I

2 500 CY See note

N

AMM 710000-640-801

ALL

LUB

I

2 500 CY See note

N

AMM 710000-640-801

ALL

LUBRICATION OF THE 1ST STAGE LOW PRESSURE COMPRESSOR (LPC) BLADE ASSEMBLY (FAN BLADE) ROOT NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE. NOTE: ETOPS PARALLEL SYSTEM 723112-P1-1R

420

LOW PRESSURE COMPRESSOR (LPC) LUBRICATION OF THE 1ST STAGE LOW PRESSURE COMPRESSOR (LPC) BLADE ASSEMBLY (FAN BLADE) ROOT NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE. NOTE: ETOPS PARALLEL SYSTEM

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 72 [1 / 3] ATA

: 72


R

72

ENGINE

Task Number

Zone

723300-P1-1

410 420

FAN CASE GROUP

412 422

FAN CASE GROUP

413 423

DIFFUSER, COMBUSTION & TURBINE NOZZLE GR

723300-P2-1

724100-P1-1

Task code

Task Title

CHK

I

800 FH

References

Ctrl

PW4G-100-72-173

GVI

GENERAL VISUAL INSPECTION OF FAN CASE, ACOUSTIC LINERS AND FAN EXIT GUIDE VANES.

N

ISB

SDI

I

10 000 FH

N

AMM 723300-210-801 MRB 72.33.00/02-PW

ALL

I

24 MO

I

2 400 FH

I

700 CY

N

AMM 720000-290-833

ALL

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

6.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff ALL

Check : 1A

INSPECTION OF FAN EXIT CASE (FECR), REAR BRACKET ASSEMBLY NOTE: TASK APPLICABLE FOR ENG PW4168A Engine Serial No. P733429 thru P733514 NOTE: ETOPS PARALLEL SYSTEM

BORESCOPE INSPECTION OF INNER AND OUTER COMBUSTION CHAMBER ASSEMBLIES AND FIRST STAGE VANES NOTE: ETOPS PARALLEL SYSTEM NOTE: RII TASK

Threshold Interval

Page : SYS - 72 [2 / 3] ATA

: 72


72

ENGINE

Task Number

Zone

725200-P1-1

413 423

Task code

Task Title

SDI

HIGH PRESSURE TURBINE GROUP BORESCOPE INSPECTION OF THE FIRST AND SECOND STAGE HIGH PRESSURE TURBINE BLADES NOTE: ETOPS PARALLEL SYSTEM NOTE: RII TASK

Threshold Interval

I

2 400 FH

I

700 CY

References

Ctrl

Eff

N

AMM 720000/6 AMT 720000-290-835

ALL

N

AEO P4-72-VN01-1/01 CMP 72-2-0204-007 VSB PW4G-100-72-195

ALL

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

1.20 MHrs

1 NDT 413 423

725200-P3-1

Issue No

:

Date

:

10 01/12/2013

HIGH PRESSURE TURBINE GROUP BORESCOPE INSPECTION OF SECOND STAGE HIGH PRESSURE TURBINE VANES NOTE: - REFER TO VSB PW4G-100-72-195 FOR THRESHOLD AND INTERVAL NOTE:TASK APPLICABLE ONLY FOR ENG PRE SB PW 72-206 NOTE : CMP TASK NOTE: RII TASK

Amendment No Date

: 01 : 06/09/2014

BSI

Check : NT

Page : SYS - 72 [3 / 3] ATA

: 72


R

73

ENGINE FUEL CONTROL

Task Number

Zone

731000-P1-1

413 423

Task Title

ENGINE FUEL FILTER

Task code

Threshold Interval

Ctrl

References

Eff

DIS

I

5 000 FH See note Check : A04

N

AMM 731100-920-801 SIL 73-024

ALL

FUC

I

N

AMM 732100/5 AMT 732100-710-821 VSB PW4G-100-2-96

ALL

DISCARD FUEL FILTER ELEMENT NOTES: - DISCARD FUEL FILTER ELEMENT AT 150 FH, 800 FH AND 1600 FH AFTER AIRCRAFT DELIVERY THEREAFTER EVERY 5000FH FH - DISCARD FUEL FILTER ELEMENT AT 150 FH AND 800 FH AFTER MAJOR TANK INTERVENTION THEREAFTER EVERY 5000FH FH NOTE: ETOPS PARALLEL SYSTEM Access panels :

416BR

418AR

Total access time :

426BR 428AR 0.00 Hrs

Skills :

1 ENG 210

732100-P1-1

0.00 MHrs

FUEL CONTROL SYSTEM FADEC READ ENGINE SCHEDULED MAINTENANCE REPORT NOTE: ETOPS PARALLEL SYSTEM

800 FH

Skills :

0.50 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 73 [1 / 2] ATA

: 73


73

ENGINE FUEL CONTROL

Task Number

Zone

771300-P1-1

410 420

Task Title

ENGINE PRESSURE RATIO INDICATING SYSTEM INSPECTION AND CLEANING OF CONDENSATION TRAP ASSEMBLIES (WATER TRAPS), FOR OBSTRUCTIONS OR BLOCKAGE NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

Task code

DI

Threshold Interval

I

1 000 CY

References

Ctrl

N

AMM 732134-280-801 CMP 72-2-0204-009 VSB MAN-PW4G-100-2-00

Access panels :

415BL

417AL

Total access time :

425BL 427AL 0.08 Hrs

Skills :

2.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 73 [2 / 2] ATA

: 73

Eff ALL


R

78

ENGINE EXHAUST

Task Number

Zone

783200-P3-1

410 420

Task code

Task Title

THRUST REVERSER STRUCTURE

Threshold Interval

References

Ctrl

Eff

GVI

I

18 MO

N

AMM 783000-210-807 MRB 78.32.00/03-PW

ALL

GVI

I

24 MO

N

AMM 783000-210-808 MRB 78.32.00/04-PW

ALL

GENERAL VISUAL INSPECTION OF FIXED STRUCTURE SEALS NOTE: ETOPS PARALLEL SYSTEM Access panels :

415AL 425BL

415BL 426AR

Total access time :

416AR 426BR

416BR 427AL

417AL 428AR

418AR

425AL

0.28 Hrs

Skills :

1.00 MHrs

1 EN 410 420

783200-P4-1

THRUST REVERSER STRUCTURE GENERAL VISUAL INSPECTION OF FIRE BLANKET NOTE: ETOPS PARALLEL SYSTEM Access panels :

415AL 425BL

415BL 426AR

Total access time :

416AR 426BR

416BR 427AL

417AL 428AR

418AR

425AL

0.28 Hrs

Skills :

1.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 78 [1 / 1] ATA

: 78


79

ENGINE OIL

Task Number

Zone

792000-P1-1

413 423

Task code

Task Title

DI

ENGINE OIL SYSTEM DISTRIBUTION

Threshold Interval

I

800 FH

References

Ctrl

Eff

N

AMM 792200-200-801

ALL

N

AMM 792122/3 AMT 792122-920-801 VSB MAN-PW4G-100-1-96

ALL

Check : 1A

INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES NOTE: ETOPS PARALLEL SYSTEM Access panels :

417AL

427AL

Total access time :

410 420

792000-P3-1

0.00 Hrs DIS

OIL DISTRIBUTION DISCARD ENGINE OIL FILTER ELEMENT. NOTE: - REFER TO MAN-PW4G-100-1-96 FOR INTERVAL NOTE: ETOPS PARALLEL SYSTEM

I

2 000 FH See note

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.20 Hrs

Skills :

1.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 79 [1 / 1] ATA

: 79


80

STARTING

Task Number

Zone

800000-P2-1

413 423

Task code

Task Title

ENGINE STARTING SYSTEM CHANGE STARTER OIL NOTE: ETOPS PARALLEL SYSTEM

Threshold Interval

References

Ctrl

SRV SER

I

600 FH

B1 AMM 121380/3 AMT 121380-610-803

DI

I

600 FH

N

Eff ALL

Access panels :

415BL 428AR

416BR

Total access time :

417EL

418AR

425BL

426BR

427EL

0.00 Hrs

Skills :

0.20 MHrs

1 EN 413 423

800000-P3-1

ENGINE STARTING SYSTEM INSPECT STARTER CHIP DETECTOR FOR PARTICLES NOTE: ETOPS PARALLEL SYSTEM

AMM 801118/6 AMT 801118-200-801

Access panels :

416BR

418AR

Total access time :

426BR 428AR 0.00 Hrs

Skills :

0.20 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : SYS - 80 [1 / 1] ATA

: 80

ALL

A330 Maintenance Schedule LIST OF EFFECTIVE PAGES TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

CMR-21

1

01/10

CMR-21

2

01/10

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1

01/10

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2

01/10

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3

01/10

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1

01/10

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1

01/10

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01/10

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3

01/10

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4

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CMR-52

1

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ISSUE 10 AMD 01

TITLE/CHAPTER/ZONE

PAGE

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TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

Page: 1


ALS Part 3 Certification Maintenance Requirements (CMR)

AIRBUS SAS 2013. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS SAS. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein) without the express written consent of AIRBUS SAS. This document and its content shall not be used for any purpose other than that for which it is supplied.

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 3-0 INTRODUCTION From revision 20 and on, the content of A330 Certification Maintenance Requirements (CMR) Document (Referenced 955.2074/93) applicable to A330 models, has been transferred to the A330 Airworthiness Limitations Section (ALS) Part 3 Certification Maintenance Requirements (CMR) This change is part of a process to provide Operators and Maintenance, Repair and Overhaul Organizations (MRO) with a series of stand-alone documents in a location dedicated to the limitations. The data provided under ALS Part 3 has been established with the following rules: 1.

SCOPE Though not addressed by the paragraph H25.4 of Joint Aviation Requirements (JAR) 25 appendix H, CMRs may be considered as the systems equivalent to the structural Airworthiness Limitation Items. For this reason, it is considered appropriate to identify them as part of the ALS. This document constitutes the ALS Part 3 - Certification Maintenance Requirements. Compliance with the requirements stated in this document is mandatory. No person may operate an aircraft to which an ALS applies except in accordance with the requirements of that ALS, unless otherwise agreed with the Authority of the State of aircraft registry.

R R

This document is applicable from first delivery of an aircraft configuration into an Operator's fleet. The starting times for CMR task intervals are defined in paragraph 8 of this sub-section. Possible interval escalations must be justified in accordance with the procedure given in paragraph 7 of this sub-section. If a more restrictive CMR is issued on an aircraft configuration already in service, the requirement for existing Operators to follow the revised ALS Part 3 will normally be mandated by Airworthiness Directive (AD). Non-compliance could suspend the validity of the Airworthiness Certificate. Airworthiness Directives dedicated to specific concerns may override the specific requirement(s) given in this document. The identification of CMR tasks in no way diminishes the importance of non-CMR tasks and changes to these are subject to normal practices and procedures agreed between the Operator and the Authority of the State of aircraft registry.


APPLICABILITY The applicability of this ALS Part 3 revision is restricted to the aircraft models listed below: A330-201 A330-202 A330-203 A330-223 A330-243 A330-223F A330-243F

A330-301 A330-302 A330-303 A330-321 A330-322 A330-323 A330-341 A330-342 A330-343

Note: The engine Time Limits and Maintenance Checks are not included in this manual: refer to the relevant Engine Manufacturer Chapter 05 manual. N 3.

A330 AICRAFT SYSTEMS UTILISATION

R R R

The CMRs contained in the ALS Part 3 are valid up to the limitations published in this document which have been identified in consideration of a maximum number of Flight Hours (FH) that may be accrued by an individual aircraft, as follows:

R R R R R R R R R R

Aircraft Series A330-200 series PRE 49144 PRE 200103 A330-200 series PRE 49144 POST 200103 A330-200 series POST 49144 A330-30x series PRE 49144 PRE 58269 A330-30x series PRE 49144 POST 58269 A330-30x series PRE 49144 POST 200103 A330-32x & A330-34x series PRE 49144 PRE 200103 A330-32x & A330-34x series PRE 49144 POST 200103 A330-300 series POST 49144 A330-200F series

N N N N D

Flight Hours (FH) 060000 FH 100000 FH 100000 FH 060000 FH 080000 FH 100000 FH 060000 FH 100000 FH 100000 FH 100000 FH

Depending on fleet leader operation, the impact of a greater aircraft accumulated FH/FC value may subsequently be investigated and might demonstrate a need for new or revised limitations. As a consequence, should any operator envisage future aircraft operations beyond the quoted values, they must first contact Airbus for advice. Note:

R

(1) Within the context of ALS Part 3, MOD 49144 is used to identify WV050 series and WV060 series aircraft (Enhanced aircraft) since this modification cannot be retrofitted on WV000, WV010 and WV020 series aircraft. (2) MOD 58269 refers to Design Service Goal (DSG) extension of A330-30x (i.e. A330-300 with GE engines) from 60000 FH up to 80000 FH.

A330 AIRWORTHINESS LIMITATIONS SECTION (3) MOD 200103 refers to Design Service Goal (DSG) extension of all A330-200/-300 up to 100000 FH. 4.

MODIFICATIONS/REPAIRS NOT DEVELOPED UNDER AIRBUS DOA CERTIFICATE EASA. 21J.031 If an aircraft/ a sub-assembly/a component/an item has a modification or repair embodied that has not been developed under the Design Organisation Approval (DOA) Certificate EASA. 21J. 031 (e.g. under a Supplemental Type Certificate) and which affects the content of the ALS Part 3, the Operator is responsible for obtaining approval by the relevant Airworthiness Authority for any necessary adaptations of the airworthiness limitations. When such an aircraft/a sub-assembly/a component/an item is transferred from one Owner/Operator to another, the associated approvals and documents indicating the necessary adaptations of airworthiness limitations must be transferred as well.

5.

ALTERNATIVE METHODS OF COMPLIANCE Limitations of the ALS Part 3 may be negated by instructions given in an Alternative Method Of Compliance (AMOC). When limitations evolve in a revision of the ALS Part 3 subsequent to the issuance date of the AMOC, Operators are requested to contact Airbus for guidance. It is Operator’s responsibility to refer to the applicable limitations.

6.

CRITERIA FOR IDENTIFICATION CMRs are tasks arising from the Type Certification process, which are associated with the most significant failure conditions. These have been shown to be necessary either by System Safety Assessment (e.g. JAR 25.1309 compliance) or, in a minority of cases, by engineering judgement. These requirements are allocated to one of two categories (identified as One Star or Two Star) in accordance with the EASA agreed methodology. Tasks associated with the following criteria are not identified as CMRs: Tasks associated with qualitative assessment (unless specifically requested by EASA), Tasks for which the maximum acceptable interval is in excess of the aircraft systems utilisation values in the paragraph 3, Tasks normally accomplished by the flight crew, Tasks considered being routine state of the art maintenance activity. For these, the safety reason for performing the task is considered to be immediately evident to the Operator and the Authority of the State of aircraft registry.

R R

7.

HANDLING OF CERTIFICATION MAINTENANCE REQUIREMENTS A.

One Star CMRs (*) One Star CMRs specified in the ALS Part 3 are mandatory tasks and cannot be changed or deleted without the concurrence of the Primary Certification Authority (EASA). One Star CMR task intervals quoted in ALS Part 3 are absolute limitations and cannot be escalated without the concurrence of the Primary Certification Authority (EASA).

A330 AIRWORTHINESS LIMITATIONS SECTION B.

Two Star CMRs (**) Two Star CMRs specified in the ALS Part 3 are mandatory tasks and cannot be changed or deleted without the concurrence of the Primary Certification Authority (EASA). Two Star CMR task intervals may be adjusted in accordance with an Operator's approved escalation practices or an approved reliability program, but the task content may not be changed or deleted without prior Primary Certification Authority (EASA) approval. This statement has been agreed on the basis that Operators with approved escalation practices or an approved reliability program make adjustments to their maintenance programs based on data collection and analytical techniques. It has been demonstrated that the use of such methods to manage a maintenance program does not give rise to undue escalation.

8.

STARTING TIME FOR CMR INTERVAL This paragraph provides general rules related to the starting time to be considered for CMR interval counting according to the different usage parameters. For CMR tasks whose interval is given in Calendar time, the starting time may be considered as the date of Transfer of Title to the first Operator of the aircraft, unless otherwise stated in the delivery documentation of the dedicated aircraft. For CMR tasks whose interval is given in Flight Hours (FH), the starting time may be considered as the date of Transfer of Title to the first Operator of the aircraft, unless otherwise stated in the delivery documentation of the dedicated aircraft. Considering the very low number of Flight Hours performed between first flight and delivery, and the methodology used to define CMR task intervals, EASA agree to consider the date of delivery of the aircraft as the starting time for CMR tasks whose intervals are given in Flight Hours. For CMR tasks whose interval is given in Flight Cycles (FC), the starting time to be considered is the date of the aircraft first flight, unless otherwise stated in the delivery documentation of the dedicated aircraft.

9.

D N N N

DEFINITIONS Calendar time (Cal.):

Thresholds/intervals in Years (Ye), Months (MO) etc…

Flight Cycle (FC):

A complete take-off and landing sequence.

Flight Hour (FH):

The accumulated time intervals between “wheels-off” and “wheelson”.

Interval:

The period expressed in usage parameters like FH and/or FC and/or Calendar time between successive accomplishments of a specific task.

Visual check:

Observation to determine that an item is fulfilling its intended purpose. It is a failure finding task and does not require quantitative tolerances.

A330 AIRWORTHINESS LIMITATIONS SECTION Operational Check:

A qualitative check to determine that an item is fulfilling its intended purpose. It is a failure-finding task and does not require quantitative tolerances.

Functional Check:

A quantitative check to determine if one or more functions of an item performs within specified limits.

Detailed lnspection:

An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required.

First flight:

Unless otherwise stated, the use of this term in the ALS Part 3 implies that the life accumulated before the aircraft delivery date/transfer of title date (e.g. as a result of test flights) must be taken into account.

10. EXCEPTIONAL SHORT-TERM EXTENSIONS Since CMR intervals are based on statistical averages and reliability rates, an exceptional short-term extension for a specific CMR interval may be made on one aircraft for a limited period of time without jeopardising safety. The term 'exceptional short-term extension' is defined as an increase in a CMR interval that may be needed to cover an uncontrollable or unexpected situation. Repeated use of such extensions, either on the same aircraft or on similar aircraft in the Operator's fleet, should not be used as a substitute for good management practices. Short-term extensions must not be used for fleet CMR escalation. Unless noted adjacent to the task, for all CMRs (One Star and Two Star) identified in this ALS Part 3, it has been accepted by the Primary Certification Office (EASA) that short-term extensions up to the following maximum values may be granted without consultation with that office. Requests for extensions in excess of these values must be submitted with full justification to the Primary Certification Office (EASA) such that approval, if granted, can be given prior to their use. A.

CMRs controlled by Flight Hours (FH) Extensions up to 10% or 500 FH (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of Flight Hours.

B.

CMRs controlled by Flight Cycles (FC) Extensions up to 5% or 250 FC (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of Flight Cycles.

A330 AIRWORTHINESS LIMITATIONS SECTION C. CMRs controlled by Calendar time (MO) Where the repeat interval is 12 months or less, extensions up to 10% or 1 month (whichever is the lesser) may exceptionally be granted on CMR intervals quoted in terms of months. Where the repeat interval is greater than 12 months, extensions up to 2 months may exceptionally be granted. It is the Operator's responsibility to identify appropriate procedures with the Authority of the State of aircraft registry for the control and development of his maintenance program. This paragraph in the ALS Part 3 is written to confirm to the Authority of the State of aircraft registry that exceptional short-term extensions of CMR intervals are permissible. Approval of such extensions rests with the Authority of the State of aircraft registry in the same way as it does for any other scheduled maintenance task interval extension


21


Task Number

Zone

212800-01-2

210

Task Title

LOWER DECK CARGO COMPARTMENT HEATING, VE

Task code

Threshold Interval

Ctrl

References

Eff

OP

I

2 500 FH See note

N

AMM 212800-710-804 CMP 21-2-0000-001 CMR 212800-00001-1-C

ALL

OP

I

2 500 FH See note

N

AMM 212800-710-805 CMP 21-2-0000-002 CMR 212800-00002-1-C

275

LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING (FWD, AFT AND BULK) OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF ISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN CASE OF SMOKE WARNING NOTE : CMP TASK Skills :

0.50 MHrs

1 AF R

210

212800-02-2

LOWER DECK CARGO COMPARTMENT HEATING, VE OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD AIR VALVE IN CASE OF SMOKE WARNING NOTE : CMP TASK

294 299 366 946 1256 1266

Skills :

0.25 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : CMR - 21 [1 / 2] ATA

: 21


21


Task Number

Zone

213100-05-1

210 270 310

Task Title

PRESSURE CONTROL AND MONITORING FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P PROTECTION OF SAFETY VALVES NOTE: THIS TASK MAY BE ALTERNATIVELY ACCOMPLISHED AN OFF AIRCRAFT TASK. REFER TO AMM PROCEDURE FOR REMOVAL AND INSTALLATION 213152-000-801 AND 213152-400-801 PREP. : ACCESS THROUGH PANEL OF REAR GALLEY;

Task code

FUC

Threshold Interval

I

24 000 FH

I

6 YE

References

Eff

AMM 213100-720-801 CMR 213100-00001-2-C

275

Ctrl

N

299 366

Access panels :


0.00 Hrs

Skills :

0.83 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : CMR - 21 [2 / 2] ATA

: 21


24

ELECTRICAL POWER

Task Number

Zone

242400-01-2

210

Task Title

AC GENERATION

Task code

Threshold Interval

Ctrl

References

Eff

OP

I

50 FH

N

AMM 242400-710-801 CMP 24-2-0000-011 CMR 242000-00001-1-C

ALL

OP

I

50 FH

N

AMM 242400-710-801 CMP 24-2-0000-011 CMR 242000-00001-1-C

ALL

OP

I

4 000 FH

N

ALL

I

24 MO

AMM 242400-710-802 CMR 242000-00003-1-C

OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM apply task 242400-01-3 Skills :

0.15 MHrs

1 EL 210

242400-01-3

AC GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM Skills :

0.30 MHrs

1 EL 210

242400-02-2

AC EMERGENCY GENERATION OPERATIONAL CHECK OF EMERGENCY GENERATOR MANUAL CONNECTION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.08 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : CMR - 24 [1 / 3] ATA

: 24


24

ELECTRICAL POWER

Task Number

Zone

242400-04-2

210

Task Title

Task code

OP


Threshold Interval

I I

OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC CONNECTION NOTE : CMP TASK NOTE: ETOPS PARALLEL SYSTEM

4 000 FH

References

Eff

N

AMM 242400-710-806 CMP 24-2-0000-002 CMR 242000-00004-1-C

ALL

N

AMM 242500-710-801 CMR 242000-00005-1-C

ALL

B2 AMM 242800-710-801 CMP 24-2-0000-003 CMR 242000-00002-1-C

ALL

Ctrl

24 MO See note

Skills :

0.18 MHrs

1 EL 210

242500-01-1

AC ESSENTIAL GENERATION SWITCHING

OP

I

12 000 FH

I

24 MO

OP

I

650 FH

OP

I

12 000 FH

I

24 MO

OPERATIONAL CHECK OF AC ESSENTIAL GENERATION MANUAL AND AUTOMATIC SWITCHING. Skills :

0.10 MHrs

1 EL 210

242800-01-2

STATIC INVERTER AC GENERATION OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS SUPPLY NOTE : CMP TASK Skills :

0.30 MHrs

2 EL 210

243500-01-1

DC GENERATION SWITCHING OPERATIONAL CHECK OF DC MAIN GENERATION SWITCHING

N

AMM 243200-710-801 CMR 243000-00001-1-C

Skills :

0.15 MHrs

1 EL

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : CMR - 24 [2 / 3] ATA

: 24

ALL


24

ELECTRICAL POWER

Task Number

Zone

243500-02-1

210

Task Title

Task code

OP

DC GENERATION OPERATIONAL CHECK OF DC ESSENTIAL GENERATION SWITCHING

Threshold Interval

I

12 000 FH

I

24 MO

I

8 000 FH

I

24 MO

References

Eff

N

AMM 243400-710-801 CMR 243000-00002-1-C

ALL

N

AMM 282100-710-809 CMR 245000-00001-1-C

ALL

Ctrl

Skills :

0.10 MHrs

2 EL 210

245000-04-1

AC ELECTRICAL LOAD DISTRIBUTION OPERATIONAL CHECK OF LEFT AND RIGHT FUEL PUMP 2 SHEDDING IN LAND RECOVERY CONFIGURATION NOTE: ETOPS PARALLEL SYSTEM

OP

Skills :

0.15 MHrs

1 AV

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : CMR - 24 [3 / 3] ATA

: 24


R

26

FIRE PROTECTION

Task Number

Zone

262300-04-2

130

Task Title


Task code

DI

Threshold Interval

I

14 000 FH

References

Ctrl

N

AMM 262300-200-803

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943 946

DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND CHECK VALVE PREP. : CHECK VALVES FILTERS ACCESS: 132SW 821 831 NOTE: ETOPS SIGNIFICATION SYSTEMS

Issue No

Eff

962 1019 1256 1266

Page : CMR - 26 [1 / 1] ATA

: 26


R

27


Task Number

Zone

271400-01-2

210

Task Title


Task code

OP

Threshold Interval

I

12 000 FH

N

OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY BITE. NOTE: FOR AIRCRAFT WHICH ARE PRE-MOD 49144 AND ON WHICH SB A330-00-3068 (MOD 200103) IS EMBODIED, FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 60000 FH. 311

272300-04-3


References

Eff

AMM 271400-740-802 CMR 271400-00001-1-C

943

Ctrl

946 962 1019 1256 1266

DI

DETAILED INSPECTION OF CONTROL ROD (ITEM 220 IN IPC 272147-1A) IN PTLU LINKAGE.

I

20 000 FH

I

72 MO

N

AMM 272300-210-803 CMR 272100-00002-2-C

275 294 299 366

Skills :

0.20 MHrs

1 AF R

210

272400-08-1


OP

I

10 000 FH

N

AMM 272400-740-802

943 946

OPERATIONAL CHECK OF RUDDER DAMPING MEASUREMENT BY BITE

962 1019 1256 1266

Skills :

0.20 MHrs

1 AF 210

272600-05-1

RUDDER MECHANICAL CONTROL OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE

OPC

I

2 400 FH

N

AMM 272600-740-802 CMR 272100-00001-1-C

275 294 299 366

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : CMR - 27 [1 / 4] ATA

: 27


R

27


Task Number

Zone

273400-01-1

210

Task Title


Task code

OP

Threshold Interval

I

12 000 FH

References

Ctrl

N

AMM 273400-740-802

Eff 943 946

OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY BITE NOTE: FOR AIRCRAFT WHICH ARE PRE-MOD 49144 AND ON WHICH SB A330-00-3068 (MOD 200103) IS EMBODIED, FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN THE AIRCRAFT ACCUMULATING 60000 FH.

962 1019 1256 1266

Skills :

0.10 MHrs

1 AF R

210 310

274000-18-1

Issue No

:

Date

:

10 01/12/2013


OP

I

10 000 FH

N

AMM 274451-710-801

294

OPERATIONAL CHECK OF THSA CHECKABLE SHEAR PIN. NOTE: THSA MODIFICATIONS AND ASSOCIATED SBS: - PRODUCTION SOLUTION: 55780 - RETROFIT SOLUTION: 54880 (27-3137) OR 54881 (27-3143) ELECTRICAL HARNESSES MODIFICATIONS AND ASSOCIATED SBS: - PRODUCTION SOLUTION: (52269 AND 56056) - RETROFIT SOLUTION: (52270 AND 56057 AND 58493 (92-3046)) OR (52359 AND 56057 AND 58493 (92-3046))

Amendment No Date

: 01 : 06/09/2014

275 366 943 946 962 1019 1256 1266

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: 27


27


Task Number

Zone

274400-01-1

310

Task Title


Task code

Threshold Interval

Ctrl

References

Eff

OP

I

5 600 FH

N

AMM 274400-710-801 CMR 274000-00001-1-C

ALL

OPC

I

800 FH

N

AMM 274400-710-802 CMR 274000-00002-1-C

ALL

OPC

I

800 FH

N

AMT 279600-710-803 CMR 279000-00001-1-C

ALL

OP

I

12 000 FH

N

24 MO

AMM 279600-710-806 CMR 279000-00002-1-C

ALL

I

OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION DEVICE Access panels :


0.00 Hrs

Skills :

1.60 MHrs

1 AF 210

274400-02-1

TRIMMABLE HORIZONTAL STABILIZER (THS) OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL HYDRAULIC SYSTEMS Skills :

0.30 MHrs

1 AF 210

279000-03-3

ELECTRICAL FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF FCPCS AND FCSCS STANDBY SERVO LOOPS ON PITCH CONTROL Skills :

0.20 MHrs

1 AF 210

279000-05-1

ELECTRICAL FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF GREEN SERVOCONTROLS TRAVEL SPEED LIMITATION WHEN RAT IS EXTENDED PREP. : RAT EXTENDED Skills :

0.50 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

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: 27


R

27


Task Number

Zone

279000-09-2

210

Task Title

ELECTRICAL FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2

Task code

OP

Threshold Interval

I

12 000 FH

I

24 MO

References

Ctrl

N

AMM 279600-710-819

Eff 943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

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: 27


28

FUEL

Task Number

Zone

282100-03-1

210

Task code

Task Title


Threshold Interval

Ctrl

References

Eff

OP

I

4 000 FH

N

AMM 282100-710-805 CMR 282100-00001-1-C

ALL

OP

I

4 000 FH

N

AMM 282100-710-806 CMR 282100-00001-1-C

ALL

OP

I

29 000 FH

N

ALL

I

6 500 CY

AMM 282400-710-808 CMR 282400-P0001-1-C

I

12 YE

OPERATIONAL CHECK TO VERIFY THAT THE LEFT NO 2 PUMP OFF FUNCTION IS OPERATIVE NOTE: ETOPS PARALLEL SYSTEM Skills :

0.20 MHrs

1 EL 210

282100-04-1

MAIN FUEL PUMP SYSTEM OPERATIONAL CHECK TO VERIFY ISOLATION OF RIGHT PUMP 2 CONTROL WHEN LEFT MAIN PUMP 2 IS RUNNING IN ELECTRICAL EMERGENCY CONFIGURATION NOTE: ETOPS PARALLEL SYSTEM Skills :

0.20 MHrs

1 EL 210 410 420

282400-06-1

ENGINE LP FUEL SHUT-OFF OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL SUPPLY TO ASSOCIATED ENGINE Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.00 Hrs

Skills :

1.50 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

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: 01 : 06/09/2014

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: 28


28

FUEL

Task Number

Zone

282600-04-1

210

Task Title

REFUEL/DEFUEL SYSTEM

Task code

Threshold Interval

Ctrl

References

Eff

OP

I

82 700 FH

N

AMM 282600-710-810 CMR 282600-00001-1-C

ALL

OP

I

25 000 FH

N

943

I

42 MO

AMM 282700-710-801 CMR 282700-00001-3-C

OPERATIONAL CHECK OF MANUAL OVERRIDE PB/SW AND AND ASSOCIATED CIRCUITRY. Skills :

0.00 MHrs

1 EL R

210

282700-02-4

TRIM TANK TRANSFER SYSTEM OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES FOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH

946 962 1019 1256 1266

Skills :

0.00 MHrs

1 EL 100

282700-05-1

FUC

TRIM TRANSFER SYSTEM FUNCTIONAL CHECK OF TRIM TANK TRANFER LINE SHROUD CONNECTORS

I

28 000 FH

I

36 MO

N

AMM 282700-790-801 CMR 282700-00002-1-C

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

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: 28

ALL


29

HYDRAULIC POWER

Task Number

Zone

292400-03-1

210 630

Task Title

AUXILIARY HYDRAULIC POWER OPERATIONAL CHECK OF MANUAL RAT DEPLOYMENT FOLLOWED BY FUNCTIONAL CHECK OF RAT OPERATION AND INSPECTION OF FILTER ELEMENT BY REFERENCE TO DIFFERENTIAL PRESSURE INDICATOR.

Task code

FUC

Threshold Interval

I

12 000 FH

I

24 MO

References

Eff

AMM 292400-720-801 CMR 292000-00001-1-C

ALL

Ctrl

N

Access panels :

196BB

197CB

Total access time :

633HB 633JR 0.00 Hrs

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

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: 29


52

DOORS

Task Number

Zone

525111-04-1

220

Task Title

Task code

OP

COCKPIT DOOR OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE MECHANISM

Threshold Interval

I

11 000 FH

References

Eff

AMM 256800-710-804 CMR 525111-00001-1-C

275

Ctrl

N

299 366

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : CMR - 52 [1 / 1] ATA

: 52


R

27


Task Number

Zone

274400-09-1

310

Task Title

TRIMMABLE HORIZONTAL STABILIZER (THS) LUBRICATION OF THS ACTUATOR BALL SCREW NUT. NOTE: - NO SHORT-TERM EXTENSION IS ALLOWED. - PRIOR TO THIS TASK PERFORM EITHER TASK 274400-13-1 OR 274400-14-1 (IF APPLICABLE). - RELUBRICATION AT 700FH ACCORDING TO EASA AD 2010-0192 (FAA AD 2005-07-04) SATISFIES REQUIREMENT OF MPD TASK 274400-09-1. - AMOC (REF. 10037783) ALLOWS LUBRICATION INTERVAL AT AT 1000 FH IF MPD TASKS 274400-13-1 AND 274400-14-1 ARE NOT APPLICABLE.(MSN 943, 962, 1019, 1256, 1266)

Task code

LUB

Threshold Interval

I

700 FH

Check : NT

References

Eff

B1 AMM 122227-640-801 ASM 274400-00002-1-E

ALL

Ctrl

Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

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: 27


27


Task Number

Zone

274400-13-1

310

Task Title

Task code

DI

THS HYDRAULIC ACTUATION DETAILED INSPECTION OF THSA BALLSCREW ASSY FOR INTEGRITY OF PRIMARY AND SECONDARY LOAD PATH AND CHECK THE GAP AT SECONDARY NUT TRUNNION MCC Note: A372, A374 - C/O WITH EO/2015/2011; : A375 - C/O WITH EO-2012-2101. NOTE: - THIS TASK MUST BE PERFORMED PRIOR TO TASK 274400-09-1. - NO SHORT TERM EXTENSION IS ALLOWED. - RELUBRICATION ACCORDING TO EASA AD 2010-0192 (FAA AD 2005-07-04) SATISFIES REQUIREMENT OF MPD TASK 274400-09-1. - FOR 100% THRESHOLD: IN COMPUTING THE LIFE ACCUMULATED BY THE THSA FOR COMPLIANCE WITH THE THRESHOLD, CALCULATIONS MUST INCLUDE FLIGHT HOURS SINCE THE INITIAL ENTRY INTO SERVICE OR SINCE 17-AUG-2002, WHICHEVER OCCURS LATER.

Threshold Interval

I

700 FH

References

Ctrl

B1 AD AD AMT ASM SIL

F-2002-414B 03 01 F-2005-07-04 274451-210-805 274400-00001-1-E 27-109

Access panels :


0.00 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ASM - 27 [2 / 4] ATA

: 27

Eff 299


27


Task Number

Zone

275400-11-1

530 630

Task code

Task Title

CHK

FLAPS DETAILED INSPECTION OF ALL LH AND RH INPUT GEARBOXES (IPGB) AND DOWN DRIVE SHAFTS (DDS) FOR CORROSION AND WEAR. NOTE: - FIRST INSPECTION IS PERFORMED IN ACCORDANCE WITH SB A330-27-3151. REPORT INSPECTION RESULTS, WHATEVER THEY ARE, TO AIRBUS. SUBSEQUENT REPETITIVE INSPECTION PERFORMED IN ACCORDANCE WITH SB A330-27-3152. - NO SHORT-TERM EXTENSION IS ALLOWED. - 100% THRESHOLD: 16. AUGUST 2009 PREP. : FLAPS EXTENDED; FLAP TRACK FAIRINGS;

Threshold Interval

T

6 YE

I

6 YE

References

Eff

275400-220-801 275000-00001-2-E 27-3151 27-3152

275

Ctrl

N

AMM ASM ISB ISB

Access panels :

531EL 574EB 674CB

533EL 574FB 674EB

Total access time :

534EL 574KB 674FB

573BB 574LB 674KB

573FB 673BB 674LB

574BB 673FB

574CB 674BB

0.00 Hrs

Skills :

8.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ASM - 27 [3 / 4] ATA

: 27

294 299 366


R

27


Task Number

Zone

275400-11-2

530 630

530 630

275400-12-1

Issue No

:

Date

:

10 01/12/2013

Task Title

Task code

DI

FLAPS DETAILED INSPECTION OF ALL LH AND RH INPUT GEARBOXES (IPGB) AND DOWN DRIVE SHAFTS (DDS) FOR CORROSION AND WEAR. NOTE: - NO SHORT-TERM EXTENSION IS ALLOWED. - 100% THRESHOLD: 26. OCTOBER 2009, WHICHEVER OCCURS LATER. PREP. : FLAPS EXTENDED; FLAP TRACK FAIRINGS;

LUBRICATE THE SPLINE JOINT BETWEEN THE INPUT GEAR BOXES (IPGB) AND THE DOWN DRIVE SHAFTS (DDS) FOR ALL FLAP TRACKS ON BOTH WINGS.

Amendment No Date

: 01 : 06/09/2014

T

6 YE

I

6 YE

References

Ctrl

N

AMM EAD FAD ISB ISB

275400-220-801 2008-0026 2010-15-02 27-3151 27-3152

Eff 943 946 962 1019 1256 1266

LUB

FLAPS

Threshold Interval

T

24 MO

I

24 MO

N

AMM 122227-640-817 ASM 275000-00001-4-E

Page : ASM - 27 [4 / 4] ATA

: 27

1256 1266


29

HYDRAULIC POWER

Task Number

Zone

292400-04-1

633

Task Title

AUXILIARY HYDRAULIC POWER REMOVAL OF RAM AIR TURBINE (RAT) FOR OVERHAUL. PREP. : FIXED FLAP TRACK FAIRING 4 RH; NOTE: RII TASK

Task code

RS

Threshold Interval

I

20 YE

Check : PCI

References

Eff

AMM 292452-960-801 ASM 292400-00001-1-E

ALL

Ctrl

N

Skills :

1 AF 1 PRE

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

4.00 MHrs 0.00 MHrs

Page : ASM - 29 [1 / 1] ATA

: 29


ALS Part 5 Fuel Airworthiness Limitations

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 5-0 INTRODUCTION 1.

GENERAL Compliance with the requirements contained in this document is mandatory. No person may operate an aircraft to which an Airworthiness Limitations Section (ALS) applies except in accordance with the requirements of that ALS, unless otherwise agreed with the Authority of the State of aircraft registry. A. ALS Part 5 Scope This document contains the Fuel Airworthiness Limitations that arise from compliance with JAA’s Interim Policy on Fuel Tank Safety (INT/POL/25/12), FAA’s Special Federal Aviation Regulation (SFAR) 88 and FAA’s 14 CFR 26.33. They have been derived in accordance with JAA’s draft Temporary Guidance Leaflet (TGL) 47 and FAA’s Advisory Circular (AC) 25.981-1B. The nomenclature and means of promulgation follow the FAA’s memorandum ref PS-ANM100-2004-10029 ‘Policy Statement on Process for Developing SFAR 88-related Instructions for Maintenance and Inspection of Fuel Tank Systems’. This latter document has been jointly developed between FAA and JAA to ensure a unified approach. These requirements, together with the Life Limits / Monitored Parts, structural Airworthiness Limitation Items (ALI) and systems Certification Maintenance Requirements (CMR) comprise the Airworthiness Limitation Section which satisfies the requirements of JAR 25.1529 Appendix H paragraph 25.4. IMPORTANT: At first delivery of an aircraft configuration into an operator’s fleet, the requirements given in this document are mandatory, except in so far that interval escalations can be justified in accordance with the procedure stated herein. If a more restrictive Fuel ALI is issued on an aircraft configuration already in service, the requirement for existing operators to follow the revised FAL document will normally be mandated by Airworthiness Directive (Consigne de Navigabilité). Non-compliance suspends the validity of the Airworthiness Certificate. The identification of Fuel Airworthiness Limitations in no way diminishes the importance of other tasks and practices associated with the fuel system. Changes to these are subject to normal practices and procedures between the operator and his national authorities. This document does not take into account Airworthiness Directives (Consignes de Navigabilité) which, if issued against an existing Fuel Airworthiness Limitation, supersede the specific requirement given in this document.

A330 AIRWORTHINESS LIMITATIONS SECTION B. ALS Part 5 Applicability The applicability of this ALS Part 5 revision is restricted to the aircraft series and models listed in the table below: Aircraft series

A330-200

A330-200F

A330-300

Aircraft models -201 -202 -203 -223 -243 -223F -243F -301 -302 -303 -321 -322 -323 -341 -342 -343

C. Reporting Accountable persons or organizations should report to Airbus, any identified condition affecting components listed in this ALS Part 5 which could endanger flight safety. “Endanger flight safety” for this ALS means any condition that could contribute to the occurrence of an ignition source in or adjacent to the fuel tanks. The finding report should include at least the information stated below: − Aircraft MSN affected, − FAL maintenance requirement reference, − Identification of the affected component/item, − Life since new (in Flight Hours and/or Flight Cycles and/or landings and/or calendar time, as applicable) accumulated by the affected system/component/item at the time of the finding, − Location and description of the finding, with indication of the size and orientation, − Circumstance of detection and inspection method used.

A330 AIRWORTHINESS LIMITATIONS SECTION D. Sub-part 5-1: Illustrations ALS Sub-part 5-1 provides illustrations of aircraft zone where the repetitive maintenance/inspection tasks listed in the sub-part 5-4 are performed. Illustrations included in this sub-part are for information only. Refer to the AMM for illustrations applicable to an actual aircraft configuration. E. Sub-part 5-2: Design changes The Sub-part 5-2 is approved by the EASA. This section provides mandatory changes to type design related to SFAR 88 and INT/POL/25/12 in accordance with the EASA policy statement on the process for developing instructions for maintenance and inspection of fuel tank system ignition source prevention. Each modification and associated instructions arise from Airworthiness Directives previously issued by EASA or French DGAC. Airbus has introduced only the requirements concerning A330 aircraft as defined in paragraph 1-B (Applicability of the document). F.

Sub-part 5-3: Life limitations The Sub part 5-3 is approved by the EASA. Components listed under this sub-part are those affected by a replacement requirement associated to a life limitation less than the applicable aircraft life limit due. Failure of these components in combination with other failure conditions can contribute to an unsafe condition. a.

Traceability and replacement requirements In order to maintain aircraft airworthiness, it is mandatory to replace components listed under sub-part 5-3 at or prior to whichever of the life limitations (if applicable) occurs first. Therefore, it is necessary to assure traceability and monitoring of the components listed in the sub-parts 5-3. Non-compliance with these requirements could suspend the validity of the Certificate of Airworthiness. New PNRs are introduced as a result of modifications and Service Bulletins Airbus publishes. These new PNRs may not be listed in the current ALS Part 5, when the related modifications and/or Service Bulletins have been released after the approval of this revision. However, it is recommended to assure traceability and monitoring of such items whatever their PNR in case of future introduction in the ALS Part 5. For further guidance, Operators are requested to contact Airbus.

A330 AIRWORTHINESS LIMITATIONS SECTION Note:

In the context of this revision, traceability means records that clearly demonstrate the history of each component back to initial entry into service of the component, so that life limitations are accurately applied. Traceability records may comprise, but are not limited to, the following: − − −

b.

Application history (aircraft type, model, weight variant, MSN i.e. Manufacturer Serial Number, etc…), Maintenance actions carried out (Airworthiness Directives, modifications, repairs, inspections, etc…), Life accumulation (accounting for any individual aircraft to which a component may have been fitted).

Disposal/quarantine action When a component listed under sub-part 5-3 reaches the life limitation, disposal/quarantine action must be taken. Appropriate means must be implemented to deter their installation on aircraft pending possible extension of their life limitations. Examples of means are: − Record keeping system, − Non-permanent markings, − Segregation (items stored separately from those currently eligible for installation). The ultimate solution is the mutilation beyond repair limits to prevent rework to appear to be airworthy.

G. Sub-part 5-4: Repetitive maintenance/inspection tasks The Sub-part 5-4 is approved by the EASA. It is mandatory to perform/repeat the maintenance requirements listed in Sub-part 5-4 at or prior to whichever of the limitations threshold/interval (if applicable) occurs first. The sub-part 5-4 identifies repetitive maintenance/inspection tasks at aircraft level. The maintenance requirements are applicable no later than the aircraft reaching the airworthiness limitation. These tasks must be included in an Operator’s Approved Maintenance Program. The task interval may be quoted in any usage parameter (Flight Hour, Flight Cycle or Calendar time) depending on the cause of potential degradation that, if not detected and addressed, could lead to a catastrophic failure of the airplane. Unless otherwise stated, the tasks and intervals specified in sub-part 5-4 of the ALS Part 5 are mandatory and cannot be changed, escalated or deleted without the concurrence of the Primary Certification Authority (EASA).

A330 AIRWORTHINESS LIMITATIONS SECTION Where explicitly stated, task intervals may be adjusted in accordance with an operator's approved escalation practices or an approved reliability program, but the task content may not be changed or deleted without prior Primary Certification Authority (EASA) approval. This statement has been agreed on the basis that operators with approved escalation practices or an approved reliability program make adjustments to their maintenance programs based on data collection and analytical techniques. It has been demonstrated that the use of such methods to manage a maintenance program does not give rise to undue escalation. With respect to tasks requiring tank entry, the interval quoted in this document is intended to allow Operators to perform the task during an extended hangar visit during which tank entry is already likely to be required for accomplishment of structural and Zonal inspections. a.

Exceptional Short-Term Extensions Since Fuel ALI Maintenance / Inspection intervals are based on statistical averages and reliability rates, an exceptional short-term extension for a specific Fuel ALI interval may be made on one aircraft for a limited period of time without jeopardising safety. The term 'exceptional short-term extension' is defined as an increase in a Fuel ALI interval that may be needed to cover an uncontrollable or unexpected situation. Repeated use of such extensions, either on the same aircraft or on similar aircraft in the operator's fleet, should not be used as a substitute for good management practices. Unless noted adjacent to the task, for all Fuel ALIs identified in this document, it has been accepted by the Primary Certification Office (EASA) that short-term extensions up to the following maximum values may be granted without consultation with that office. Requests for extensions in excess of these values must be submitted with full justification to the Primary Certification Office (EASA) such that approval, if granted, can be given prior to their use. (1) Fuel ALIs controlled by Flight Hours (FH) Extensions up to 10% or 500FH (whichever is the lesser) may exceptionally be granted on Fuel ALI intervals quoted in terms of flight hours. (2) Fuel ALIs controlled by Flight Cycles (FC or LDGS) Extensions up to 5% or 250FC (whichever is the lesser) may exceptionally be granted on Fuel ALI intervals quoted in terms of flight cycles or landings. (3) Fuel ALIs controlled by Calendar Time (MTHS or MO) Where the repeat interval is 12 months or less, extensions up to 10% or 1 month (whichever is the lesser) may exceptionally be granted on Fuel ALI intervals quoted in terms of months.

A330 AIRWORTHINESS LIMITATIONS SECTION Where the repeat interval is greater than 12 months but less than 3 years, extensions up to 2 months may exceptionally be granted. Where the repeat interval is 3 years or greater, extensions up to 3 months may exceptionally be granted. It is the operator's responsibility to identify appropriate procedures with his local regulatory authority for the control and development of his maintenance program. This paragraph in the Fuel Airworthiness Limitation document is written to confirm to the local regulatory authority that exceptional short-term extensions of Fuel ALI intervals are permissible. Approval of such extensions rests with the local authority in the same way as it does for any other scheduled maintenance task interval extension. H. Sub-part 5-5: Critical Design Configuration Control Limitations The Sub part 5-5 is approved by the EASA. A CDCCL is a limitation requirement to preserve either a critical ignition source prevention feature of the fuel system design that is necessary to prevent the occurrence of an unsafe condition or a critical design feature of the flammability reduction system. The purpose of the CDCCL is to provide instructions to retain the critical ignition source prevention or critical flammability reduction system design feature during configuration change that may be caused by alterations, repairs, or maintenance actions. It is the operator’s responsibility to ensure that their internal documentation is amended to reflect the limitations and associated instructions contained within this sub-part and provide appropriate text to highlight the existence of each CDCCL. Such identification is necessary in the instructions used by the person performing an installation, alteration, repair or modification so as to minimize the risk that the work performed compromises the original design criteria. Regulatory oversight of the operator’s compliance with this mandatory requirement is based on the appropriate identification of the CDCCL in the accomplishment instructions associated with the installation, alteration, repair or modification. I.

Modifications/repairs not developed under Airbus DOA Certificate EASA.21J.031 If an aircraft/a component/an item has a modification or repair embodied that has not been developed under the Design Organization Approval (DOA) Certificate EASA.21J.031 (e.g. under a Supplemental Type Certificate) and which affects the content of the ALS Part 5, the Operator is responsible for obtaining approval by the relevant Airworthiness Authority for any necessary adaptations of the airworthiness limitations. When such an aircraft/a component/an item is transferred from one Owner/Operator to another, the associated approvals and documents indicating the necessary adaptations of airworthiness limitations must be transferred as well.


DEFINITIONS The initial entry into service is defined for the aircraft (systems installations) as: −

−

The date of Transfer of Title (ToT) to the first Operator for airworthiness limitations in Calendar times and/or flight hours, unless otherwise stated in any delivery documentation to the first Operator. Considering the very low number of Flight Hours performed between first flight and delivery, and the methodology used to define task intervals, EASA agree to consider the date of delivery of the aircraft as the starting time for Fuel ALI tasks whose intervals are given in Flight Hours. The date of aircraft first flight for airworthiness limitations in Flight Cycles and/or Landings.

The initial entry into service for the transferable systems components/items is defined as the date at which the component/item accomplishes the first flight for which it will undertake its intended function. Note:

Unless otherwise stated, this means for transferable components/items delivered on new aircraft (i.e. from Airbus Final Assembly Line) that the life accumulated between aircraft first flight and the aircraft delivery date/transfer of title date (e.g. as a result of test flights) must be taken into account.

Calendar times (Cal.):

Thresholds/intervals in Years (Ye), Months (Mo) etc… must be counted from the date of initial entry into service (unless otherwise stated). In considering the accumulated time since the initial entry into service, it should be noted that Calendar time usage parameter cannot be frozen (unless otherwise stated).

Flight Cycle (FC):

A complete take-Off and landing sequence.

Flight Hour (FH):

The accumulated time intervals between ‘wheels-off’ and ‘wheelson’.

Interval:

The period expressed in usage parameters like FH and/or FC and/or LDG and/or Calendar time between successive accomplishments of a specific task.

Operational Check:

A qualitative check to determine that an item is fulfilling its intended purpose. It is a failure finding task and does not require quantitative tolerances.

Threshold:

The initial accomplishment of a specific maintenance task from the initial Entry Into Service (EIS). It may be expressed in usage parameters like FH and/or FC and/or LDG and/or Calendar time.

Detailed Inspection:

An intensive examination of a specific item, installation or assembly, to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required.


LIMITATION/REPLACEMENT TIME INDICATION A. General In computing the part’s accumulated life, calculations must include flight hours and/or flight cycles and/or landings and/or calendar time (as applicable) since the initial entry into service of the part (unless otherwise stated). The life limitation indicated against PNR originally fitted is counted from the part’s initial entry into service. The life limitation indicated against PNR evolutions is also to be counted from the part’s initial entry into service (unless otherwise stated). B. ALS Part 5 Life Limitation Life limitations quoted in Sub-part 5-3 are applicable to the undamaged detail parts as listed, not to the assembly or the aircraft on which they are installed. The limitation/replacement time indication is quoted on the same line/block of lines as the PNR. C. Production/Repair concessions, ALS Variation and Alternative Method Of Compliance The life limitation of the ALS Part 5 may be negated by instructions given in either a Production concession, a Repair design Approval Sheet (RAS), an ALS Variation (AV) or an Alternative Method Of Compliance (AMOC). It is the operator’s responsibility to refer to the applicable limitations. When limitations change in a revision of the ALS Part 5 subsequent to the issuance date of the Production concession/RAS/AV/AMOC, Operators are requested to contact Airbus for guidance. The restrictions of limitation(s) indicated in the RAS/AV/AMOC (or absence thereof) depend on the part's accumulated life considered during the original evaluation of the repair solution/AV/AMOC. Production concessions are provided to the initial Operator of the aircraft in the delivery documentation (Aircraft Inspection Report ‘Recordable concessions’).

4.

RULES SPECIFIC TO ALS PART 5 A. Sub-part 5-2: Design changes The modifications and associated Service Bulletins are presented in the sub-part 5-2 and are classified by ATA chapters by ascending numbers. The requirements arising from airworthiness directives introduced in this revision concern only the A330 series aircraft as defined in paragraph 1-B of this sub-part.

A330 AIRWORTHINESS LIMITATIONS SECTION Unless otherwise stated, where no revision number is made for an Airbus SB, it must be assumed that the latest approved revision of the SB is applicable but any previous revision is acceptable. Where a revision number is stated, Operators must use this revision number. The use of any further approved revision is an acceptable mean of compliance for modification requirements. B. Sub-part 5-3: Life limitations The life limitation and associated instructions must be applied from: − The initial Entry Into Service of the part (Refer to paragraph 2 of this sub-part for Definitions). Life limitation applicability is allocated to all affected aircraft (refer to Sub-part 5-0 paragraph 1-B Applicability system). C.

Sub-part 5-4: Repetitive maintenance/inspection tasks The limitations and associated instructions must be applied from: − The Entry Into Service of the aircraft for the first accomplishment and then the date of last accomplishment of the task. The repetitive maintenance/inspection tasks are presented in the sub-part 5-4 in accordance with the following method: a.

FAL reference number The FAL reference numbering system follows a similar format to the Maintenance Planning Document (MPD) system, as follows: The FAL reference number comprises 12 digits and 1 letter organised as follows: XXXXXX-YYYYY-I-F XXXXXX: The ATA reference identifies the system/sub-system or component on which the task is to be accomplished. YYYYY:

Stands for the Sequence Number, apart from a few cases, the sequence number is used to discriminate between different tasks relating to the same hardware.

I:

The Applicability Index identifies successive developments of a task, introduced by modifications or specific requirement.

F:

Stands for discriminating task related to ALS Part 5.

A330 AIRWORTHINESS LIMITATIONS SECTION b.

Description column The description column provides the following information: − A task description: Gives a concise description of the work to be performed. − A reference to the related illustration identified in the sub-part 5-1.

c.

Threshold/Interval column These columns are used to record the selected threshold and interval for the task. The threshold and interval may be expressed in terms of usage parameters or notes. Usage parameters are defined in the paragraph 2 of this sub-part.

d.

Reference column The reference column provides reference(s) to Instruction for Continued Airworthiness where maintenance practices/procedures necessary for the task accomplishment are provided. E.g.: Reference to Aircraft Maintenance Manual (AMM). The reference column is for guidance only as its content is not approved by EASA. Should a reference change between two successive revisions of the ALS Part 5, the Operator should consider the updated reference.

e.

Limitations applicability column Applicability

A330-xxx POST nnnnn A330-xxx POST nnnnn OR POST SB A330-yy-yyyy A330-xxx POST nnnnn PRE mmmmm A330-xxx POST nnnnn PRE mmmmm A330-yyy POST aaaaa PRE bbbbb

Task applicable to All A330-xxx that do have MOD nnnnn embodied All A330-xxx that do have MOD nnnnn embodied OR All A330-xxx that do have SB A330-yy-yyyy embodied. All A330-xxx that do have MOD nnnnn embodied but that do not have MOD mmmmm embodied.

All A330-xxx that do have MOD nnnnn embodied but do not have MOD mmmmm OR A330-yyy that do have MOD aaaaa but do not have MOD bbbbb embodied.

D. Sub-part 5-5: CDCCL The CDCCL items related to fuel tank system are presented in the ALS part 5 sub-part 5-5. a.

CDCCL column The CDCCL column identifies the critical component/part or design features of the fuel tanks and, if fitted, the Flammability Reduction System (FRS) which provides an inerting function.

A330 AIRWORTHINESS LIMITATIONS SECTION b.

Requirements column The requirements column explains why critical component/ part or design features of the fuel tanks or of the FRS are considered critical with regards to ignition risk. This column provides instructions to retain the critical ignition source prevention or critical flammability reduction features during configuration change that may be caused by alterations, repairs, or maintenance actions that Operators are required to comply with.

c.

Reference column This column provides a reference to Instruction for Continued Airworthiness where a CDCCL is contained. E.g: Reference to Aircraft Maintenance Manual (AMM), or Component Maintenance Manual (CMM). Operators must ensure that the person performing an installation, a repair or a modification will not compromise the original design criteria and must reflect CDCCL in their internal documentation.

d.

Applicability column Due to their general nature, CDCCL n°5 and n°8 are considered impracticable to identify in aircraft documentation. The applicability column gives the combination of critical design features with aircraft that requires the identification of CDCCL items. Note: CDCCL n°8 applies only to FAA registered aircraft. “FAA only” term in the limitation applicability means that all aircraft operated under FAA registration or aircraft registered under an Airworthiness Authority which follow FAA rules, have to comply with this limitation. It is the operator’s responsibility to check the limitation applicability with the authority of the state of aircraft registration.

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 5-2 CHANGES TO TYPE DESIGN Note: Where reference is made to an Airbus Service Bulletin (SB), it must be assumed that the latest approved revision of the SB is applicable, but any previous revision is acceptable. Where a particular revision is stated, the revision or any later approved revision must be used. ATA 21-00 AIR CONDITIONING SYSTEM MOD

SB

EASA AD

FAA AD

EMBODIMENT LIMITS (Whichever occurs first)

DESCRIPTION FH

FC

Cal.

LIMITATIONS APPLICABILITY

49520

A330-21-3096 R01

2006-0191

2006-21-08

Air conditioning - Center fuselage – Install heatshields in belly fairing to segregate air system.

N/A

N/A

31-Oct-2008 A330-200

58551

A330-21-3148

2009-0150

2010-04-09

Air conditioning - Air cooling - Modify heatshields

N/A

N/A

23-Jul-2011 A330-200 (1)

(1) Except on which Airbus modification 49520 has been embodied in production or on which Airbus Service Bulletin (SB) A330-21- 3096 Revision 01 has been embodied in service

Note: The embodiment limits given in the table above are for EASA compliance.

ISSUE: NOV 16/11

ALS PART 5-2 EASA APPROVED

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document.

PAGE: 1

A330 AIRWORTHINESS LIMITATIONS SECTION Note: Where reference is made to an Airbus SB, it must be assumed that the latest approved revision of the SB is applicable, but any previous revision is acceptable. Where a particular revision is stated, the revision or any later approved revision must be used. ATA 28-00 FUEL SYSTEM MOD

SB

EASA AD

FAA AD


DESCRIPTION FH

FC

Cal.


N/A

A330-28-3092 R01

2007-0278

2008-25-02

Fuel - General - Inspection of p-clips in the wings and center fuel Tanks.

N/A

N/A

31-Dec-2009 A330-200 (1) A330-300 (1)

42969

A330-28-3044 R01

1998-099-066 (B)

N/A

Fuel - FQI - Fit modified densitometer electrically bonded to aircraft structure.

N/A

N/A

Within the first scheduled inner fuel tank opening but no later than 72 Months since Entry In Service

A330-301 A330-321 A330-322 A330-341 A330-342

1998-099-066 (B)

N/A

Fuel − Quantity indication − Improve electrical N/A bonding of densitometer to aircraft structure.

Within the first scheduled inner fuel tank opening but no later than 72 Months since Entry In Service

A330-301 A330-321 A330-322 A330-341 A330-342

45580

A330-28-3053

N/A

55118

A330-28-3101 R01

2007-0278

2008-25-02

Fuel - general - bonding of fuel diffuser support bracket to wing Structure.

N/A

N/A

31-Dec-2009 A330-200 (2) A330-300 (2)

49135 51825 50104

A330-28-3082 R01

2007-0278

2008-25-02

Fuel - General - Revise the electrical bonding of the equipment in the fuel tanks.

N/A

N/A

31-Dec-2009 A330-200 (2)(3) A330-300 (2)(3)


MOD 200242

SB A330-28-3113 R00

EASA AD 2011-0196

FAA AD N/A


DESCRIPTION Fuel – Main transfer system – Intro ground fault interrupters to center tank fuel pump control circuit.

FH

FC

N/A

N/A

Cal.


21-Oct-2015 A330-200 A330-200F PRE 58623 POST 200281

(1) On which AIRBUS modification No. 47634 has been embodied in production. (2) Except for aircraft on which the four AIRBUS modifications No. 49135 and 49630 and 51825 and 55118 have been embodied in production or modified in-service in accordance with both SB A330-28-3082 Revision 04 and SB A330-28-3101 Revision 01. (3) For aircraft that have already been modified in accordance with SB A330-28-3082 at original issue: Not later than December 31st, 2011, perform the additional work in accordance with the instructions of SB A330-28-3082 at Revision 04.


A330 AIRWORTHINESS LIMITATIONS SECTION Note: Where reference is made to an Airbus SB, it must be assumed that the latest approved revision of the SB is applicable, but any previous revision is acceptable. Where a particular revision is stated, the revision or any later approved revision must be used. ATA 31-00 INDICATING & RECORDING SYSTEMS MOD 58751

SB A330-31-3146

EASA AD 2010-0089

FAA AD 2011-01-02


DESCRIPTION Indicating/recording systems - Flight warning computer (FWC) - Install FWC standard T3-0.

FH

FC

N/A

N/A

Cal.


24-Nov-2010 A330-200 (1) A330-300 (1)

(1) Except those on which Airbus modification 51790 has been embodied in production or Airbus Service Bulletin (SB) A330-31-3066 or SB A330-313082 or SB A330-31-3093 or SB A330-31-3105 has been embodied in Service


A330 AIRWORTHINESS LIMITATIONS SECTION Note: Where reference is made to an Airbus SB, it must be assumed that the latest approved revision of the SB is applicable, but any previous revision is acceptable. Where a particular revision is stated, the revision or any later approved revision must be used. ATA 55-00 HORIZONTAL STABILIZER MOD 44848

SB A330-55-3016 R01

EASA AD 2007-0278

FAA AD 2008-25-02


DESCRIPTION Stabilizer - Horizontal stabilizer - Rework of some metallic parts for improvement of lightning strike protection.

FH

FC

N/A

N/A

Cal.


31-Dec-2009 A330-301 (1) A330-321 (1) A330-322 (1) A330-341 (1) A330-342 (1)

(1) Except for aircraft on which AIRBUS modification No. 44252 has been embodied in production.

Notes: For all aircraft where the improvement of the THS lighting strike protection has already been performed in accordance with AOT 55-03 dated 22 August 1996 (“solution A”), mandated by DGAC AD F-1996-178-049(B) R1 and DGAC AD F-1996-177-038(B) with a compliance time of November,15th 1996, it is allowed to increase the distance between metallic parts on the THS Trim Tank in accordance with the instructions of SB A330-55-3016 after 31st December 2009, whenever the THS removal from aircraft and put on ground on support Tool (Lifting and Resting points Fittings must be installed) for any reason (fuselage stress jacking, repair...) is performed for the first time after such date, or at the first aircraft maintenance task requiring the use of THS Lifting and Resting points Fittings performed after such date. -

The embodiment limits given in the table above are for EASA compliance.

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 5-3 LIFE LIMITATIONS ATA 47-10-00 INERT GAS SYSTEM – GENERATION/STORAGE Nomenclature Air Separation Module (ASM)

Part Number (1) 2060032-1XX

LIFE LIMITS (whichever occurs the first) FH

FC

Cal.

27000

N/A

N/A

(1) XX at the end of the Part Number stands for any number between 01 and 99

LIFE LIMITS APPLICABILITY A330-200 POST MOD 58723

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-Part 5-4 REPETITIVE MAINTENANCE/INSPECTION TASKS ALS PART 5 REPETITIVE MAINTENANCE/INSPECTION TASKS Description

FAL reference number

GROUND FAULT INTERRUPTERS – FIG. 01

281800-00001-1-F

REFERENCE AMM 28-18-00-710

INTERVAL 4000 FH

APPLICABILITY FAA only (1) A330-200 POST MOD 200242

Operational check of centre tank fuel pump Ground Fault Interrupter (GFI)

A330-200F POST MOD 200242

VAPOUR HEATSHIELDS – FIG. 02

281800-00002-1-F

AMM 28-18-52-210

6 Ye (2)

A330-200 POST MOD 49520

Detailed inspection of the heatshields below the centre tank. A330-200F POST MOD 49520 POST 200281 PRE 58623

NEA and DFCV – FIG. 02 IGGS and DFSOV – FIG. 04

470000-00001-1-F

AMM 47-21-43-710

12000FH

A330-200 POST MOD 58020

470000-00002-1-F

AMM 47-20-43-710

60000FH (3)

A330-200 POST MOD 58020

Operational check of Dual Flow Shut Off Valve (DFSOV), Dual Flapper Check Valve (DFCV) and Nitrogen Enriched Air (NEA) pipeline for leaks.

NEA and DFCV – FIG. 03 Operational check of both Dual Flapper Check Valves (DFCV) for leaks.


ALS PART 5 REPETITIVE MAINTENANCE/INSPECTION TASKS Description

FAL reference number

NEA and DFCV – FIG. 03

470000-00003-1-F

Operational check of Dual Flapper Check Valves (DFCV) for reverse flow.

REFERENCE AMM 47-20-43-710

INTERVAL 12000FH

APPLICABILITY A330-200 POST MOD 58019 PRE MOD 58020

(1) “FAA only” term in the limitation applicability means that all aircraft operated under FAA registration or aircraft registered under an Airworthiness Authority which follow FAA rules, have to comply with this limitation. It is the operator’s responsibility to check the limitation applicability with the authority of the state of aircraft registration. (2) In accordance with sub-part 5-0, paragraph 1-G, it is herewith confirmed that the interval of the task mentioned in the above table may be adjusted in accordance with an operator's approved escalation practices or an approved reliability program, but the task content may not be changed or deleted without prior Primary Certification Authority (EASA) approval. (3) For aircraft that have operated with MOD 58019 embodied in isolation, the operational check of both Dual Flapper Check Valves for leaks shall also be performed at time of embodiment of MOD 58020.

A330 AIRWORTHINESS LIMITATIONS SECTION Sub-part 5-5: CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS

CDCCL REF.

1

2

3

CDCCL

REQUIREMENTS

REFERENCE

Air Gap between Fuel Quantity Indicator (FQI) probe and tank structure.

Critical to prevent spark generation during lightning strike conditions AMM and must not be compromised. 28-42-15-400 28-42-16-400 The gaps stated in the relevant maintenance procedure in the AMM 28-42-17-400 must be achieved during installation of a fuel quantity probe. 28-42-19-400 28-42-21-400

Separation of fuel quantity and level indicating system wiring from other wiring.

To prevent cross coupling of high voltage transients and thereby ESPM keep unsafe ignition energies from inside the tank. It is required that 20-10-00 operators obey the wire routing and separation standards given in the Electrical Standard Practices Manual (ESPM). 20-33-20 20-33-21 20-33-22

Direct bonding on items of Direct bonding is critical to prevent spark generation during AMM component failure and lightning strike conditions and must not be 28-11-33-400 equipment inside a fuel compromised. tank. 28-11-41-400 28-11-44-400 Direct Bonding in fuel tanks must be carried out during component installation to the appropriate bonding method and standard stated 28-12-41-400 within the installation procedure in the AMM. 28-12-45-400 28-12-48-400 28-12-51-400

LIMITATION APPLICABILITY

A330 – ALL series A330-200 A330 – ALL series A330-200 A330 – ALL series

A330 – ALL series A330 – ALL series A330 – ALL series A330 – ALL series

A330 – ALL series A330 – ALL series A330-200 A330 – ALL series A330 – ALL series A330 – ALL series A330 – ALL series

28-13-43-400

A330 – ALL series

28-17-51-400

A330 – ALL series

28-21-51-400 28-21-52-400 28-22-41-400

A330 – ALL series A330 – ALL series A330 – ALL series


CDCCL REF.

(3) (continuing)

CDCCL

REQUIREMENTS

REFERENCE


28-22-42-400 28-22-51-400 28-22-52-400

A330 – ALL series A330 – ALL series A330 – ALL series

28-25-42-400 28-25-43-400 28-25-44-400

A330 – ALL series A330 – ALL series A330-200

28-26-42-400 28-26-49-400 28-26-51-400

A330 – ALL series A330-200 A330-200

28-27-48-400 28-27-56-400

A330 – ALL series A330 – ALL series

28-42-18-400

A330 – ALL series

28-43-51-400 28-43-53-400

A330 – ALL series A330-200

57-27-11-400

A330 – ALL series


CDCCL REF.

4

CDCCL

REQUIREMENTS

REFERENCE

Safety critical features of fuel pumps.

These features must be maintained throughout the full life of the fuel CMM pump to avoid the possibility of generation of an ignition source by 28-20-40 overheating or sparks caused by arcing, friction etc. 28-21-50 Repair and overhaul of fuel pumps must be carried out in accordance 28-21-55 with the equipment manufacturer’s maintenance instructions or other maintenance instructions acceptable to the certifying authority. 28-22-11 28-22-12


A330 – ALL series A330 – ALL series A330 – ALL series A330 – ALL series A330 – ALL series

5

Centre fuel tank volume, ventilation and flow rate.

The volume of the Centre fuel tank and the flow rate of the ventilation N/A system must be maintained at values which, when used in the determination of the fuel tank flammability exposure, comply with the Flammability Reduction System (FRS) requirements.

A330-200 POST MOD 58723

6

Protective coating on fuel tank at the connection of fuel tank inerting system.

A protective coating (Finch paint) is necessary at the connection AMM between the centre fuel tank and the Dual Flapper Check Valves 47-20-43-400 (DFCV) housing of the Inert Gas Generating System (IGGS) to 47-21-43-700 prevent fuel or fuel vapour leaks into an area containing ignition sources. After maintenance of the DFCV the protective coating must be restored to the appropriate standard using the method stated within the maintenance procedure in the AMM.

A330-200 POST MOD 58019

7

Warning Placards for areas that may contain oxygen depleted atmospheres.

When a Flammability Reduction System is installed, the access doors and panels to the fuel tank(s) and any other enclosed areas that could contain hazardous atmosphere under either normal conditions or failure conditions must be permanently stencilled, marked, or placarded to warn of hazards. Warning placards must be installed in the appropriate positions to ensure maintenance personnel are aware of areas that may be hazardous because of possible oxygen depleted atmosphere.

A330-200 POST MOD 58723

AMM 25-52-00-000 25-52-00-400 28-12-52-000 28-12-52-400 57-17-11-000 57-17-00-400


CDCCL REF.

8

CDCCL

REQUIREMENTS

REFERENCE

Flammability Reduction System (FRS) design performance.

Flammability reduction system performance is dependent on airplane N/A descent times. Industry efforts to reduce descent time may result in Flammability Reduction System performance that does not meet FAA requirements. Fleet average flammability exposure for the fuel tanks with flammability reduction system of this airplane type must be maintained in accordance with 14 CFR Part 25, appendix M.


FAA only (1) A330-200 POST MOD 58723

Airbus will monitor descent statistics (including US descents) and, if necessary to maintain compliance, will publish service information. If Airbus publishes such service information, this CDCCL requires that Operators implement these FAA approved design changes to maintain compliance with 14 CFR Part 25, appendix M.

(1) “FAA only” term in the limitation applicability means that all aircraft operated under FAA registration or aircraft registered under an Airworthiness Authority which follow FAA rules, have to comply with this limitation. It is the operator’s responsibility to check the limitation applicability with the authority of the state of aircraft registration. Note: The CDCCL Ref. 8 does not require individual Operators to monitor descent rates of their fleets. Airbus will monitor descent statistics and provide any needed service instructions to Operators. To prevent increasing flammability exposure above permissible levels, this CDCCL requires Operators to incorporate future Airbus published service instructions denoted to maintain compliance with this CDCCL, or other approved actions, within the compliance times stated in the service instructions.


28

FUEL

Task Number

Zone

281800-02-1

190

Task Title

IGNITION PREVENTION

Task code

Threshold Interval

Ctrl

References

Eff

GVI

I

6 YE

N

AMM 281852-210-801 FAL 281800-00002-1-F

ALL

OP

I

4 000 FH

N

24 MO

AMM 281800-710-801 FAL 281800-00001-1-F

1256

I

DETAILED INSPECTION OF HEATSHIELDS BELOW THE CENTER TANK(SFAR88) Access panels :

192PB

193DB

Total access time :

0.00 Hrs

Skills :

0.60 MHrs

1 AF 120 210

281800-12-1

Issue No

:

Date

:

10 01/12/2013

IGNITION PREVENTION OPERATIONAL CHECK OF CENTER TANK FUEL PUMP GROUND FAULT INTERRUPTER (GFI)(SFAR88).

Amendment No Date

: 01 : 06/09/2014

Page : FAL - 28 [1 / 1] ATA

: 28

1266


47


Task Number

Zone

470000-03-1

191

Task Title

INERT GAS SYSTEM

Task code

OP

Threshold Interval

I

12 000 FH

N

OPERATIONAL CHECK OF DUAL FLOW SHUT OFF VALVE (DFSOV), DUAL FLAPPER CHECK VALVE (DFCV) AND NITROGEN-ENRICHED AIR (NEA) PIPELINE FOR LEAKS. 140 191

470000-04-1

Issue No

:

Date

:

10 01/12/2013

INERT GAS SYSTEM OPERATIONAL CHECK OF BOTH DUAL FLAPPER CHECK VALVES (DFCV) FOR LEAKS.

Amendment No Date

: 01 : 06/09/2014

OP

I

60 000 FH

References

Eff

AMM 472143-710-801 FAL 470000-00001-1-F

1256

AMM 472043-710-801 FAL 470000-00002-1-F

1256

Ctrl

N

Page : FAL - 47 [1 / 1] ATA

: 47

1266

1266


12

SERVICING (LUBRICATION)

Task Number

Zone

12-ECO-00

000

Task Title

AIRPLANE WET WASH

Task code

Threshold Interval

CLN

I

CLN

Check : 1C

30 DY

References

Eff

N

AMM 12-21-11-615-802

ALL

N

AMM 12-21-11-615-802

ALL

Ctrl

WASHING AIRCRAFT 000

12-ECO-10

AIRPLANE EXTERNAL CLEANING EXTERNAL CLEANING OF THE AIRCRAFT CLEANING OF THE WINDOWS CLEANING OF THE LANDING GEAR AND LANDING GEAR BAY

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ECO - 12 [1 / 1] ATA

: 12


72

ENGINE

Task Number

Zone

72-ECO-00

410 420

Issue No

:

Date

:

10 01/12/2013

Task Title

ENGINE CLEANING

Task code

CLN

Threshold Interval

I

1 200 FH

References

Eff

B1 AMM 72-00-00-100-806

ALL

Ctrl

CLEANING OF THE ENGINE GASPATH

Amendment No Date

: 01 : 06/09/2014

Page : ECO - 72 [1 / 1] ATA

: 72


PAGE

AMDT / ISSUE NO

TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

TITLE/CHAPTER/ZONE

PAGE

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ALI-52

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18

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43

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ISSUE 10 AMD 01


Page: 1


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TITLE/CHAPTER/ZONE

PAGE

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TITLE/CHAPTER/ZONE

PAGE

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ALI-54

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ISSUE 10 AMD 01


Page: 2


PAGE

AMDT / ISSUE NO

ALI-57

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PAGE

64

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65

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66

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67

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1

01/10


Page: 3


52

DOORS

Task Number

Zone

521103-01-2

831 841

Task Title

FWD PASSENGER/CREW DOOR

Task code

GVI

GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE

Threshold Interval

T

12 800 FC

I

12 800 CY

T

33 900 FC

I

15 500 CY

T

12 800 FC

I

12 800 CY

T

12 800 FC

I

12 800 CY

References

Ctrl

Eff

N

AMM 521100-210-801

ALL

N

ALI

ALL

N

AMM 521200-200-803

ALL

N

AMM 521300-200-803

ALL

Skills :

0.30 MHrs

1 AF 521105-01-1

521201-01-2

831 841


832 842

MID PASSENGER/CREW DOOR

DI

DETAILED INSPECTION OF TOP & BOTTOM CROSSBEAMS T8 & T1 ENDS AT FRAMES FR1 AND FR7 IN THEIR UNION TO DOOR STOP ASSEMBLIES, ON FORWARD PASSENGER/CREW DOOR, LH/RH. GVI

GENERAL VISUAL INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE

521105-01-01

Skills :

0.30 MHrs

1 AF 833 843

521301-01-2

GVI

AFT PASSENGER/CREW DOOR GENERAL VISUAL INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 52 [1 / 5] ATA

: 52


52

DOORS

Task Number

Zone

522201-01-2

834 844

Task code

Task Title

GVI

PASSENGER COMPARTMENT EMERGENCY EXIT GENERAL VISUAL INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE

Threshold Interval

T

12 800 FC

I

12 800 CY

T

15 800 FC

T

12 YE

I

3 300 CY

I

12 YE

T

10 600 FC

I

2 600 CY

References

Ctrl

Eff

N

AMM 522200-200-807

ALL

N

AMM 523100-220-802

ALL

N

AMM 523100-220-804

275

Skills :

2.00 MHrs

1 AF 132 821

523104-01-1

DI

FORWARD CARGO COMPARTMENT DOOR DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR HINGE ASSEMBLIES AT FR 20B TO FR25 (10 PLACES). note:CPCP Access panels :

132AR 132HR

132BR 132JR

Total access time :

132CR 132KR

132DR 132LR

132ER

132FR

132GR

0.00 Hrs

Skills :

2.00 MHrs

1 AF 821

523106-01-1

FORWARD CARGO COMPARTMENT DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR FR 20B, BETWEEN BEAM 3 AND BEAM 4.

DI

294 299 366

Access panels :

821CR Total access time :

0.60 Hrs

Skills :

0.50 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 52 [2 / 5] ATA

: 52


52

DOORS

Task Number

Zone

523204-01-1

152 822

Task code

Task Title

DI

AFT CARGO COMPARTMENT DOOR DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES) note:CPCP

Threshold Interval

T

15 800 FC

T

12 YE

I

3 300 CY

I

12 YE

T

10 300 FC

I

10 300 CY

T

20 000 FC

I

14 200 CY

References

Ctrl

Eff

N

AMM 523200-220-802

ALL

N

AMM 524111-200-801

ALL

N

AMM 524111-200-805

275

Access panels :

152AR 152HR

152BR 152JR

Total access time :

152CR 152KR

152DR 152LR

152ER

152FR

152GR

0.00 Hrs

Skills :

2.00 MHrs

1 AF 811

524101-01-2

AVIONICS COMP ACCESS DOOR

DI

DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER ACCESS DOOR SKIN, EXTERNAL SURFACE Skills :

0.50 MHrs

1 AF 121 122 811

524103-01-2

AVIONICS COMP ACCESS DOOR DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS PREP. : DOOR FLOOR PANEL; NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

DI

Access panels :


0.00 Hrs

Skills :

0.75 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 52 [3 / 5] ATA

: 52


52

DOORS

Task Number

Zone

524103-01-2S100

121 122 811

Task Title


Task code

DI

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS PREP. : DOOR FLOOR PANEL;

Threshold Interval

T

31 500 FC

I

14 200 CY

References

Ctrl

N

ALI 524103-01-02 AMM 524111-200-805

Eff 294 299 366

Skills :

0.75 MHrs

1 AF 734 744

528104-01-2

DI

MAIN GEAR DOORS DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, CENTER FITTING AND SURROUNDING AREA (300 MM AROUND), LH/RH NOTE: TPS APPLICATION REQUIRED ON FITTING ONLY note: CPCP

T

8 300 FC

T

6 YE

I

8 300 CY

I

6 YE

N

AMM 528100-200-804

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 52 [4 / 5] ATA

: 52

ALL


52

DOORS

Task Number

Zone

528203-01-1

713 714

Task Title

Task code

DI

NOSE GEAR DOORS DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON FUSELAGE, LH/RH note:CPCP

Threshold Interval

T

9 600 FC

T

6 YE

I

9 600 CY

I

6 YE

References

Ctrl

N

AMM 528200-200-803

Access panels :

713

714

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 52 [5 / 5] ATA

: 52

Eff ALL


53

FUSELAGE

Task Number

Zone

531106-01-4

200

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

10 000 CY

T

32 600 FC

I

10 000 CY

References

Ctrl

Eff

N

ALI 531106-01-04 AMM 531100-200-836

275

N

ALI 531106-01-04 AMM 531100-200-836

294

Skills :

1.00 MHrs

1 AF 531106-01-4S100

200

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.

299 366

Skills :

1.00 MHrs

1 AF 200

531110-02-2

FUSELAGE SKIN BTW FR 10 AND FR 13 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10 AND FR 13 FROM FLOOR LEVEL TO STR 9 FWD, EXTERNAL SURFACE, LH/RH

DI

T

18 500 FC

I

18 500 CY

N

AMM 531100-220-843

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [1 / 59] ATA

: 53

ALL


53

FUSELAGE

Task Number

Zone

531112-02-1

100 200

Task Title

Task code

DI

DOOR 1 CUTOUT DETAILED INSPECTION OF FUSELAGE STRUCTURE AROUND DOOR 1 (FORWARD PASSAGER / CREW DOOR), EXTERNAL SURFACE, BETWEEN FR 13 AND FR 18 FROM LATERAL LONGITUDINAL LAP JOINT TO STR 9 AFT, LH/RH

Threshold Interval

T

8 900 FC

I

8 900 CY

T

3 700 FC

I

3 700 CY

References

Ctrl

Eff

N

AMM 531100-220-805

ALL

N

AMM 531100-200-863

ALL

Access panels :

831

841

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 100

531118-01-1

GVI

NOSE FORWARD FUSELAGE GENERAL VISUAL INSPECTION OF GROUND SERVICES CONNECTION ACCESS DOORS CUTOUTS AND NOSE LANDING GEAR CUTOUT, BETWEEN FR 4 AND FR 19 ON LOWER FUSELAGE Access panels :

121AL

121EL

Total access time :

713 714 0.00 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [2 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531120-01-1

123

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF NLG BAY INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS NOTE:CPCP

Threshold Interval

T

3 900 FH

T

1 150 FC

References

Ctrl

Eff

N

AMM 531100/6 AMT 531100-210-801

ALL

N

AMM 531100-200-835

294

T

6 YE

I

3 900 FH

I

1 150 CY

I

6 YE

T

144 100 FH

T

26 300 CY

299

I

52 400 FH

366

I

9 200 CY

T

109 600 FH

T

20 000 CY

I

52 400 FH

I

9 200 CY

Access panels :

713

714

Total access time :

0.16 Hrs

Skills :

0.80 MHrs

1 AF 123

531124-01-4

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH Access panels :

713

714

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 531124-01-4S020

123

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

N

AMM 531100-200-835

Page : ALI - 53 [3 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

531125-01-4

121 122

Task Title

Task code

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH

Threshold Interval

T

21 400 FC

I

5 750 CY

References

Ctrl

N

AMM 531100-200-859

Eff 275 294 299 366

Access panels :

811

821

Total access time :

0.02 Hrs

Skills :

0.00 MHrs

1 NDT 123

531129-02-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

20 000 CY

I

4 750 CY

T

32 900 FC

I

4 750 CY

N

ALI 531129-02-02 AMM 531100-200-861

275

N

ALI 531129-02-02 AMM 531100-200-861

294

Access panels :

713

714

Total access time :

715 716 0.00 Hrs

Skills :

0.50 MHrs

1 NDT 531129-02-2S100

123

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING

366

Skills :

0.50 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [4 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531132-01-2

121 122

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 14 JOINT AREA BETWEEN STRINGERS 28 AND 30 LEVEL LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

12 900 CY

T

35 100 FC

I

12 900 CY

References

Ctrl

Eff

N

ALI 531132-01-02 AMM 531100-220-809

275

N

ALI 531132-01-02 AMM 531100-220-809

294

Skills :

0.40 MHrs

1 AF 531132-01-2S100

121 122

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 14 JOINT AREA BETWEEN STRINGERS 28 AND 30 LEVEL LH/RH.

299 366

Skills :

0.20 MHrs

1 AF 531134-01-3

531134-01-3S100

Issue No

:

Date

:

121 122

NOSE FORWARD FUSELAGE

121 122


10 01/12/2013

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.

Amendment No Date

: 01 : 06/09/2014

SDI

T

20 000 CY

I

3 700 CY

T

39 000 CY

I

3 700 CY

N

AMM 531100-250-802

275

N

AMM 531100-250-802

294 299 366

Page : ALI - 53 [5 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531135-01-2

200

Task Title

Task code

SDI

COCKPIT WINDOW FRAME SPECIAL DETAILED INSPECTION OF REAR LOWER CORNER OF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OF FR.10, EXTERNAL SURFACE, LH/RH.

Threshold Interval

T

4 850 FC

I

4 850 CY

T

20 000 FC

I

9 150 CY

T

34 700 FC

I

9 150 CY

References

Ctrl

Eff

N

AMM 531100-220-806

ALL

N

ALI 531138-01-02 AMM 531100-220-812

275

N

ALI 531138-01-02 AMM 531100-220-812

294

Skills :

0.80 MHrs

1 NDT 110

531138-01-2

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 ABOVE COCKPIT FLOOR LEVEL. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 Skills :

1.00 MHrs

1 AF 531138-01-2S100

110

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 ABOVE COCKPIT FLOOR LEVEL.

366

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [6 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531139-01-2

211 212

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND UPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT FLOOR LEVEL. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

9 150 CY

T

34 700 FC

I

9 150 CY

References

Ctrl

Eff

N

ALI 531139-01-02 AMM 531100-220-813

275

N

ALI 531139-01-02 AMM 531100-220-813

294

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF 531139-01-2S100

211 212

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND UPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT FLOOR LEVEL.

299 366

Skills :

1.00 MHrs

1 AF D

211 212

531142-01-2

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-02-2 NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

20 000 FC

I

5 200 CY

N

ALI 531142-01-02 AMM 531100-200-838

Skills :

1.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [7 / 59] ATA

: 53

275


D

53

FUSELAGE

Task Number

Zone

531142-01-2S100

211 212

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.

Threshold Interval

T

34 900 FC

I

5 200 CY

References

Ctrl

N

ALI 531142-01-02 AMM 531100-200-838

Eff 262 275 294 299 366

Skills :

1.00 MHrs

1 AF 211 212

531142-02-2

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-01-2 NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

20 000 FC

I

7 800 CY

T

34 900 FC

I

7 800 CY

N

ALI 531142-02-02 AMM 531100-200-848

275

N

ALI 531142-02-02 AMM 531100-200-848

294

Skills :

1.00 MHrs

1 NDT 531142-02-2S100

211 212

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.

366

Skills :

1.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [8 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531143-01-2

121 122

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING AT FR.14, LH/RH.

Threshold Interval

T

16 600 FC

I

3 900 CY

References

Ctrl

N

AMM 531100-220-837

Eff 275 294 299 366

Skills :

0.60 MHrs

1 AF 121 122

531144-01-2

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FRAME 14 AND CRUCIFORM FITTING, LH/RH. PREP. : INSULATION Z120;

T

16 600 FC

I

7 000 CY

N

AMM 531100-200-849

275 294 299 366

Skills :

0.60 MHrs

1 NDT R

531144-01-3S020

121 122

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FRAME 14 AND CRUCIFORM FITTING, LH/RH.

T

17 000 FC

I

7 000 CY

N

ALI 531144-01-03 AMM 531100-200-849

943 946 962 1019 1256 1266

Skills :

0.60 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [9 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531146-01-1

211 212

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 UPPER MEMBER, LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

8 750 CY

T

37 100 FC

I

8 750 CY

References

Ctrl

Eff

N

ALI 531146-01-01 AMM 531100-220-839

275

N

ALI 531146-01-01 AMM 531100-220-839

294

Skills :

0.60 MHrs

1 AF 531146-01-1S100

211 212

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 UPPER MEMBER, LH/RH.

299 366

Skills :

0.60 MHrs

1 AF 211 212

531149-01-1

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING TOP 3 NUTS ON CENTRE POST. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

20 000 FC

I

8 500 CY

N

AMM 531100-220-838

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [10 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

531149-01-1S100

211 212

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING TOP 3 NUTS ON CENTRE POST.

Threshold Interval

T

35 300 FC

I

8 500 CY

References

Ctrl

N

AMM 531100-220-838

Eff 294 299 366

Skills :

0.60 MHrs

1 AF 211 212

531154-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, INTERNAL STRUCTURE, LH/RH.

T

15 800 FC

I

8 100 CY

N

AMM 531100-200-857

275 294 299 366

Skills :

0.00 MHrs

1 AF R

531154-01-3S020

211 212

DI

MAIN STRUCTURE DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, INTERNAL STRUCTURE, LH/RH. PREP. : LINING; NOTE 1; SLIDING WINDOWS OPENED;

T

17 000 FC

I

8 100 CY

N

AMM 531100-200-857

946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : ALI - 53 [11 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531158-01-1

211 212

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 AND 9 UPPER MEMBERS, LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

15 500 CY

T

35 300 FC

I

15 500 CY

References

Ctrl

Eff

N

ALI 531158-01-01 AMM 531100-220-842

275

N

ALI 531158-01-01 AMM 531100-220-842

294

Skills :

0.60 MHrs

1 AF 531158-01-1S100

211 212

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 AND 9 UPPER MEMBERS, LH/RH.

299 366

Skills :

0.60 MHrs

1 AF 231 232

531175-01-3

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT STGR.14/18/22/24, LH/RH.

T

22 700 FC

I

7 900 CY

N

AMM 531100-200-840

294 299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : ALI - 53 [12 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531183-01-2

223 224

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH. PREP. : TOILETS, LINING, INSULATION TO BE DISPLACED, FASTENERS TO BEREMOVED;

Threshold Interval

T

28 700 FC

I

9 600 CY

References

Ctrl

N

ALI 531183-01-02 AMM 531100-250-821

Eff 275 294 299 366

Skills :

0.00 MHrs

1 NDT 223 224

531186-01-3

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH PREP. : DOOR FRAME LININGS Z220; INSULATION Z220; LAVATORIES Z220;

T

23 700 CY

I

9 600 CY

N

ALI 531186-01-03 AMM 531100-200-851

275 294 299 366

Skills :

0.20 MHrs

1 NDT 100 200

531188-01-3

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STRG.9 FWD LEVEL, LH/RH.

T

28 700 FC

I

7 000 CY

N

AMM 531100-200-868

299 366

Skills :

1.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : ALI - 53 [13 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531188-01-3S020

100 200

MAIN STRUCTURE

221 222

MAIN STRUCTURE

531189-01-2

Task Title

Task code

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STRG.9 FWD LEVEL, LH/RH. DI

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERON AT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B, LH/RH NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 CY

I

7 000 CY

T

20 000 FC

I

8 850 CY

T

29 300 FC

I

8 850 CY

References

Ctrl

Eff

N

AMM 531100-200-868

275

N

ALI 531189-01-02 AMM 531100-200-854

275

N

ALI 531189-01-02 AMM 531100-200-854

294

Skills :

0.00 MHrs

1 AF 531189-01-2S100

221 222

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERON AT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B, LH/RH

366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [14 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531192-01-3

221 222

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FR. 13 FORWARD FACE AND STRINGER 9 FORWARD AND FR. 13 AFT FACE AND STRINGER 12, LH/RH.

Threshold Interval

T

21 800 FC

I

8 100 CY

T

21 800 FC

I

8 100 CY

T

20 000 FC

I

8 850 CY

References

Ctrl

Eff

N

AMM 531100-200-842

ALL

N

AMM 531100-200-843

ALL

N

AMM 531100-200-844

275

Skills :

0.40 MHrs

1 AF 221 222

531194-01-3

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, MACHINED STIFFENERS 14 AND 22 BETWEEN FR. 17 AND FR. 18, LH/RH PREP. : DOOR FRAME LININGS Z220; INSULATION Z220; Skills :

0.00 MHrs

1 AF 121 122

531198-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [15 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

531198-01-2S100

121 122

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH

Threshold Interval

T

29 300 FC

I

8 850 CY

References

Ctrl

N

AMM 531100-200-844

Eff 294 299 366

Skills :

0.00 MHrs

1 AF D

100

532101-01-2

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-2.

T

2 200 CY

I

2 200 CY

T

6 900 FC

I

6 900 CY

N

AMM 532100-210-801

ALL

N

AMM 532100-220-827

ALL

Skills :

2.50 MHrs

1 AF R

100

532101-02-2

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-2.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

Page : ALI - 53 [16 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532115-01-1

132

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL FRAMES (FR 20A AND FR 25A) NOTE: CPCP

Threshold Interval

T

97 400 FH

T

14 300 CY

T

6 YE

I

97 400 FH

I

14 300 CY

I

6 YE

T

26 000 FC

I

7 300 CY

References

Ctrl

Eff

N

AMM 532100-200-812

ALL

N

AMM 532100-220-802

943

Access panels :


0.02 Hrs

Skills :

0.00 MHrs

1 AF R

100

532124-02-1

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH PREP. : SCUFF PLATES BELOW Z832/Z842;

946 962 1019 1256 1266

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [17 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532124-02-4

100 200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH PREP. : SCUFF PLATES BELOW Z832/Z842;

Threshold Interval

T

26 000 FC

I

8 800 CY

References

Ctrl

N

ALI 532124-02-04 AMM 532100-220-802

Eff 275 294 299 366

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

4.00 MHrs

1 NDT R

200

532125-01-1

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH

T

7 300 FC

I

7 300 CY

N

AMM 532100-220-803

943 946 962 1019 1256 1266

Skills :

1.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [18 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532125-01-4

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH

Threshold Interval

T

8 800 FC

I

8 800 CY

References

Ctrl

N

AMM 532100-220-803

Eff 275 294 299 366

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 200

532130-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROM STR 18 TO STR 22, LH/RH

N

AMM 532100-210-824

20 400 FC

I

26 100 FH

294

I

8 500 CY

299 366

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 53 [19 / 59] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

532138-01-1

100

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37 AND FR 37.1, FROM STR 53 TO STR 54, LH ONLY.

Threshold Interval

T

17 000 CY

I

10 000 CY

References

Ctrl

N

AMM 532100-210-825

Eff 943 946 962 1019 1256 1266

Access panels :

131AG

821

Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 AF 100

532138-01-3

MAIN STRUCTURE

DI

DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNA CUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTER LINE, EXTERNAL SURFACE 532138-01-3S100

100

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37 AND FR 37.1, FROM STR 53 TO STR 54, LH ONLY.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

T

20 000 CY

I

10 000 CY

T

26 500 CY

I

10 000 CY

N

AMM 532100-210-825

275

N

AMM 532100-210-825

294 299 366

Page : ALI - 53 [20 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532144-01-2

243 244

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FRAMES AND STRINGER COUPLING AREA, BETWEEN FR 32 AND FR 34, FROM STR 9 TO STR 13 LH/RH, INTERNAL STRUCTURE

Threshold Interval

T

20 000 FC

I

10 000 CY

T

20 600 FC

I

10 000 CY

T

23 200 FC

I

15 900 CY

References

Ctrl

Eff

N

AMM 532100-210-828

ALL

N

AMM 532100-210-831

ALL

N

AMM 532100-210-832

ALL

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF 131 132

532147-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OF CARGO FLOOR ATTACHMENTS FITTINGS FROM FR 20 TO FR 38 LH, FROM FR 26 TO FR 38 RH, BETWEEN STR 34 AND STR 43 Access panels :


0.02 Hrs

Skills :

4.00 MHrs

1 AF 200

532148-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREA AT FR 31 FROM STR 9 TO STR 15 LH/RH, EXTERNAL SURFACE Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [21 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532152-01-1

100 200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN AT SHEAR TIE ATTACHMENT BETWEEN FR 26 AND FR 37.1 FROM STR 13 TO STR 31 LH/RH, EXTERNAL SURFACE

Threshold Interval

T

22 600 CY

I

7 800 CY

T

13 900 FC

I

7 400 CY

References

Ctrl

Eff

N

ALI 532152-01-01 AMM 532100-210-846

ALL

N

AMM 532100-220-804

275

Skills :

2.00 MHrs

1 AF 100

532153-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32 AND FR 33, FROM STR 45 TO STR 49, LH ONLY

294 299 366

Skills :

0.00 MHrs

1 NDT R

100

532153-01-3

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32 AND FR 33, FROM STR 45 TO STR 49, LH ONLY

T

17 000 CY

I

30 000 CY

N

AMM 532100-220-804

943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [22 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532154-01-2

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AT SPOT LIGHT CUT-OUT, BETWEEN FR 27 AND FR 28 AND BETWEEN FR 30 AND FR 31, FROM STR 24 TO STR 26, LH/RH

Threshold Interval

T

25 900 FC

I

5 500 CY

References

Ctrl

N

AMM 532100-210-833

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 532154-01-2S020

200

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AT SPOT LIGHT CUT-OUT, BETWEEN FR 27 AND FR 28 AND BETWEEN FR 30 AND FR 31, FROM STR 24 TO STR 26, LH/RH

100

532155-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN AND DOUBLER AT PRESSURE RELIEF VALVE CUT-OUT, BETWEEN FR 24 AND FR 25, FROM STR 26 TO STR 30, LH ONLY

T

20 000 CY

I

5 500 CY

T

17 100 FC

I

5 300 CY

N

AMM 532100-210-833

275

N

AMM 532100-210-834

275 294 299 366

Skills :

0.00 MHrs

1 AF 200

532156-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH

N

AMM 532100-220-812

239 600 FH

T

35 200 CY

299

I

22 500 FH

366

I

3 700 CY

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

T

Page : ALI - 53 [23 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

532156-01-2S020

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

243 244

532157-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR 15, LH/RH PREP. : INSULATION Z240; SIDEWALL LININGS Z240;

Threshold Interval

T

60 000 FH

T

20 000 CY

I

22 500 FH

I

3 700 CY See note

T

38 800 CY

I

15 900 CY

References

Ctrl

Eff

N

AMM 532100-220-812

275

N

ALI 532157-01-02 AMM 532100-220-805

294 299 366

Access panels :

832

842

Total access time :

532157-01-2S020

Issue No

:

Date

:

243 244

10 01/12/2013

0.04 Hrs

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR 15, LH/RH PREP. : INSULATION SIDEWALL LINING

Amendment No Date

: 01 : 06/09/2014

SDI

T

20 000 CY

I

15 900 CY

N

AMM 532100-220-805

Page : ALI - 53 [24 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

532158-01-2

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH PREP. : CEILING PANELS; INSULATION;

Threshold Interval

References

Ctrl

N

AMM 532100-220-806

Eff 294

T

239 600 FH

T

35 200 CY

299

I

22 500 FH

366

I

3 700 CY

T

60 000 FH

T

20 000 CY

I

22 500 FH

I

3 700 CY

T

20 000 CY

I

3 400 CY

T

35 800 CY

I

3 400 CY

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

532158-01-2S020

200

MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH PREP. : CEILING PANELS; INSULATION; NOTE: THRESHOLD NEXT 4C CHECK 532165-02-2

532165-02-2S100

Issue No

:

Date

:

243 244 253 254

MAIN STRUCTURE

243 244 253 254

MAIN STRUCTURE

10 01/12/2013

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 38, LH/RH

SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 38, LH/RH

Amendment No Date

: 01 : 06/09/2014

SDI

N

AMM 532100-220-806

275

N

AMM 532100-220-819

275

N

AMM 532100-220-819

294 299 366

Page : ALI - 53 [25 / 59] ATA

: 53


D

53

FUSELAGE

Task Number

Zone

532166-01-3

200

Task code

Task Title

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO CROWN CENTER LINE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-3.

Threshold Interval

T

4 500 FC

I

4 500 CY

T

6 900 FC

I

6 900 CY

T

16 400 FC

I

4 800 CY

References

Ctrl

Eff

N

AMM 532100-210-853

ALL

N

AMM 532100-220-829

ALL

N

AMM 533100-220-813

ALL

Skills :

0.00 MHrs

1 AF 200

532166-02-3

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO CROWN CENTER LINE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-3.

191 192 197 198

533005-01-2

DI

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING SEALING LIP ATTACHMENT FROM FRAME 37.1 TO 38 AND FROM FRAME 53.6 TO 56 Access panels :

191AB 197AT

191AT 197FB

Total access time :

191BB 197GB

191CB 197HB

192AT 198AT

192BB 198GB

192CB 198HB

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [26 / 59] ATA

: 53


D

53

FUSELAGE

Task Number

Zone

533009-01-2

251 252 253 254

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 1 LH/RH NOTE : - ROTOTEST INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-2 PREP. : INSULATION Z250; OVERHEAD STOWAGE BINS Z250; NOTE: APPLY TASK: 533009-02-2

Threshold Interval

T

60 000 FH

T

20 000 CY

I

42 500 FH

I

12 100 CY See note

References

Ctrl

Eff

N

ALI 533009-01-02 AMM 533100-250-812

275

N

ALI 533009-01-02 AMM 533100-250-812

294

Check : NT

Skills :

0.00 MHrs

1 NDT D

533009-01-2S100

251 252 253 254

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 1 LH/RH NOTE : - ROTOTEST INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-2S100 PREP. : INSULATION Z250; OVERHEAD STOWAGE BINS Z250;

T

175 200 FH

T

26 900 CY

I

42 500 FH

I

12 100 CY

366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [27 / 59] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533009-02-2

251 252 253 254

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH NOTE : - X-RAY INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-2 PREP. : INSULATION Z250; OVERHEAD STOWAGE BINS Z250;

Threshold Interval

T

60 000 FH

T

20 000 FC

I

14 100 FH

I

4 050 CY See note

References

Ctrl

Eff

N

ALI 533009-02-02 AMM 533100-260-801

275

N

ALI 533009-02-02 AMM 533100-260-801

294

Check : NT

Skills :

16.00 MHrs

1 NDT 533009-02-2S100

251 252 253 254

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH NOTE : - X-RAY INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-2S100 PREP. : NOTE 1; OVERHEAD STOWAGE BINS;

T

175 200 FH

T

26 900 CY

I

14 100 FH

I

4 050 CY

366

Skills :

16.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 53 [28 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533010-01-2

200

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH NOTE: THRESHOLD NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

12 000 FH

I

3 400 CY See note

References

Ctrl

Eff

N

AMM 533100-250-804

275

N

AMM 533100-250-804

294

Check : NT Skills :

4.00 MHrs

1 NDT 533010-01-2S100

200

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH

T

175 200 FH

T

26 900 CY

299

I

12 000 FH

366

I

3 400 CY

T

60 000 FH

T

20 000 CY

I

16 700 FH

I

4 750 CY See note

Skills :

4.00 MHrs

1 NDT 200

533018-01-1

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

N

AMM 533100-250-810

Check : NT

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [29 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

533018-01-1S100

200

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-250-810

Eff 294

T

170 400 FH

T

26 200 CY

299

I

16 700 FH

366

I

4 750 CY

T

49 200 FH

T

7 550 FC

294

I

32 800 FH

299

I

5 050 CY

366

T

51 400 FH

T

7 800 FC

I

34 300 FH

962

5 200 CY

1019

Skills :

0.30 MHrs

1 NDT 734 744

533021-01-2

R

734 744

533021-01-3

MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 533021-02-2. MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.

I

N

N

AMM 533100-250-856

ALI

53-31-00-250-856

275

943 946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [30 / 59] ATA

: 53


D

53

FUSELAGE

Task Number

Zone

533021-02-2

147 148 149

147 148 149

533021-02-3

200

533106-01-3

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION (BORESCOPE) OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 AND Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR.53.2, LH. NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 533021-01-2. NOTE: APPLY TASK 533021-01-2.

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION (BORESCOPE) OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 AND Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR.53.2, LH. NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 533021-01-3.

DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

References

Ctrl

N

AMM 533100-290-809

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

49 200 FH

T

7 550 CY

294

I

32 800 FH

299

I

5 050 CY

366

T

51 400 FH

T

7 800 CY

962

I

34 300 FH

1019

I

5 200 CY

1256

N

AMM 533100-290-809

T

60 000 FH

T

20 000 CY

I

38 400 FH

N

ALI 533106-01-03 AMM 533100-220-850

I


2.00 MHrs

: 01 : 06/09/2014

275

T

Skills :

1 AF

Eff

943

1266

DI

CENTER FUSELAGE

Threshold Interval

Page : ALI - 53 [31 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

533106-01-3S100

200

Task Title

Task code

DI

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH

131 132 137 138

533107-01-4

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STRINGER 29 LEVEL, LH/RH

Threshold Interval

References

Ctrl

N

ALI 533106-01-03 AMM 533100-220-850

Eff 294

T

132 100 FH

T

37 700 FC

I

38 400 FH

I

10 900 CY See note

T

54 800 FH

T

15 600 FC

I

36 000 FH

299

I

10 200 CY

366

T

60 000 FH

T

17 000 CY

I

58 300 FH

962

8 600 CY

1019

299 366

N

ALI 533107-01-04 AMM 533100-200-852

275 294

Skills :

0.40 MHrs

1 NDT R

533107-01-7S020

131 132 137 138

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STRINGER 29 LEVEL, LH/RH PREP. : AIR CONDITIONING DUCTS IN Z137/138; AIR CONDITIONING DUCTS IN Z137/138;

I

N

AMM 533100-200-852

946

1256 1266

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : ALI - 53 [32 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533109-01-1

200

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22 FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARD AND AFT FRAME 45 LEVEL, LH/RH NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

20 000 FC

I

10 200 CY

T

33 800 FC

I

10 200 CY

References

Ctrl

Eff

N

AMM 533100-250-806

275

N

AMM 533100-250-806

294

Skills :

0.20 MHrs

1 NDT 533109-01-1S100

200

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22 FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARD AND AFT FRAME 45 LEVEL, LH/RH

299 366

Skills :

0.20 MHrs

1 NDT 200

533112-01-2

CENTER FUSELAGE SPECIAL DETAILED INSPECITON OF FUSELAGE EXTERNAL STRUCTURE, LONGITUDINAL JOINT AT STRINGER 39 AHEAD OF FRAME 53.2, LH/RH.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

SDI

N

ALI 533112-01-02 AMM 533100-270-825

275

T

116 800 FH

T

35 700 FC

I

5 200 FH

299

I

1 600 CY

366

Page : ALI - 53 [33 / 59] ATA

: 53

294


R

53

FUSELAGE

Task Number

Zone

533113-01-6

200

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-200-854

Eff 943

T

47 400 FH

T

7 000 FC

I

35 400 FH

962

5 200 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT 200

533113-01-8

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH

N

ALI 533113-01-08 AMM 533100-200-854

275

T

49 200 FH

T

14 000 FC

I

28 100 FH

299

I

8 000 CY

366

T

72 400 FH

T

20 600 FC

294

I

72 400 FH

299

I

20 600 CY

366

294

Skills :

0.20 MHrs

1 NDT 251 252

533114-01-6

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTION WITH STABILIZERS STRINGER 20 TO 23, LH/RH PREP. : NOTE 1;

N

AMM 533100-200-846

Access panels :

251XW

252XW

Total access time :

0.06 Hrs

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [34 / 59] ATA

: 53

275


R

53

FUSELAGE

Task Number

Zone

533115-01-7

251 252

Task Title

Task code

DI

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-220-816

Eff 943

T

84 800 FH

T

12 500 FC

I

27 500 FH

962

4 000 CY

1019

I

946

1256 1266

Skills :

0.40 MHrs

1 AF 251 252

533115-01-8

DI

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH PREP. : NOTE 1;

N

ALI 533115-01-08 AMM 533100-220-816

52 200 FH

T

14 900 FC

I

18 100 FH

299

I

5 150 CY

366

Access panels :

251XW

252XW

Total access time :

0.06 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 53 [35 / 59] ATA

: 53

294


53

FUSELAGE

Task Number

Zone

533125-01-1

147 148 149

Task Title

Task code

GVI

CENTER LANDING GEAR WELL GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2 PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF THE CLG TRUNNION FITTINGS NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED note:CPCP

Threshold Interval

T

1 500 FC

T

6 YE

I

1 500 CY

I

6 YE

T

13 200 FH

T

4 050 FC

T

6 YE

I

13 200 FH

I

4 050 CY

I

6 YE

References

Ctrl

Eff

N

AMM 533100/6 AMT 533100-200-832

ALL

N

ALI 533126-01-03 AMM 533100-200-833

275

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 147 148 149

533126-01-3

GVI

MLG AND CLG CUTOUT GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND CLG AND MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 note:CPCP

299 366

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.90 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : ALI - 53 [36 / 59] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533126-01-6

147 148 149

Task Title

Task code

DI

MLG AND CLG CUTOUT GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND CLG AND MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 note:CPCP

Threshold Interval

T

32 800 FH

T

5 000 FC

T

6 YE

References

Ctrl

N

AMM 533100-200-833

Eff 943 946 962 1019

I

32 800 FH

I

5 000 CY

I

6 YE

T

13 200 FH

T

4 050 FC

I

13 200 FH

299

I

4 050 CY

366

1256 1266

Skills :

0.90 MHrs

1 AF 191 192 193 195 196

533127-03-2

AIR CONDITIONING ACCESS CUTOUT DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE PREP. : FAIRING PANELS BETWEEN FR 39.1 AND FR 47;

DI

N

ALI 533127-03-02 AMM 533100-220-801

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [37 / 59] ATA

: 53

275 294


R

53

FUSELAGE

Task Number

Zone

533127-03-3

191 192 193 195 196

Task code

Task Title

GVI

AIR CONDITIONING ACCESS CUTOUT DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE PREP. : FAIRING PANELS BETWEEN FR 39.1 AND FR 47;

Threshold Interval

References

Ctrl

N

AMM 533100-220-801

Eff 943

T

32 800 FH

T

5 000 FC

I

32 800 FH

962

5 000 CY

1019

I

946

1256 1266

Access panels :

191KB 195DB

192PB 196BB

Total access time :

192SB 196EB

193AB 196GB

193BB 196HB

193DB

195CB

0.10 Hrs

Skills :

0.25 MHrs

1 AF 100 197 198

533145-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STRINGER 31 LEVEL FROM FRAME 53.3 TO FRAME 54, LH/RH NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

24 700 FC

I

6 150 CY

N

ALI 533145-01-04 AMM 533100-200-844

197HB

Total access time :

198AT

366

198HB

0.00 Hrs

Skills :

0.60 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294 299

Access panels :

197AT

275

Page : ALI - 53 [38 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533151-01-3

251 252

151 152

533152-02-2

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET FAIRING LEVEL, LH/RH. PREP. : LD-MCR IF INSTALLED;

Threshold Interval

T

67 300 FH

T

19 200 FC

I

41 700 FH

I

11 900 CY See note

T

24 700 CY

I

6 150 CY

References

Ctrl

Eff

N

ALI 533151-01-03 AMM 533100-220-932

ALL

N

ALI 533152-01-05 AMM 533100-270-811

275 294 299 366

Access panels :

151GW

152BX

Total access time :

0.68 Hrs

Skills :

0.00 MHrs

1 NDT 145 146

533154-01-5

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1, LH/RH

T

20 000 FC

I

13 300 CY

N

AMM 533100-220-819

294 299 366

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : ALI - 53 [39 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533155-01-1

145 146

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

41 700 FH

I

12 700 CY See note

References

Ctrl

Eff

N

AMM 533100-220-854

275

N

AMM 533100-220-854

294

Check : NT Access panels :

251FG

252FG

Total access time :

3.52 Hrs

Skills :

2.00 MHrs

1 AF 533155-01-1S100

145 146

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH

T

220 900 FH

T

33 900 CY

299

I

41 700 FH

366

I

12 600 CY

T

60 000 FH

T

20 000 CY

I

41 600 FH

I

7 300 CY See note

Skills :

2.00 MHrs

1 AF 151 152

533156-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. NOTE: THRESHOLD IS NEXT 4C CHECK

N

ALI 533156-01-02 AMM 533100-270-801

Check : NT Skills :

0.50 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [40 / 59] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

533156-01-2S100

151 152

147 148

533164-01-3

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH.

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959, LH/RH

Threshold Interval

References

Ctrl

N

ALI 533156-01-02 AMM 533100-270-801

Eff 294

T

216 000 FH

T

33 200 CY

I

24 500 FH

I

7 500 CY See note

T

106 300 FH

T

16 300 CY

I

69 300 FH

299

I

10 600 CY See note

366

T

60 000 FH

T

17 000 CY

I

84 200 FH

962

12 900 CY

1019

299 366

N

ALI 533164-01-03 AMM 533100-200-839

275 294

Skills :

2.00 MHrs

1 AF R

533164-01-4S020

147 148

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959, LH/RH

I

N

ALI 533164-01-04 AMM 533100-200-839

943 946

1256 1266

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [41 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533180-01-3

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS BETWEEN FR 53.6 AND FR 53.7,EXTERNAL SURFACE, LH/RH: - FROM STR 5 TO STR 13 (DOOR TYPE A) - FROM STR 5 TO STR 15 (DOOR TYPE 1)

Threshold Interval

References

Ctrl

N

AMM 533100-200-855

Eff 294

T

96 000 FH

T

27 300 CY

299

I

29 600 FH

366

I

8 400 CY

T

60 000 FH

T

20 000 CY

I

29 600 FH

Skills :

0.00 MHrs

1 AF 533180-01-3S020

200

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS BETWEEN FR 53.6 AND FR 53.7,EXTERNAL SURFACE, LH/RH: - FROM STR 5 TO STR 13 (DOOR TYPE A) - FROM STR 5 TO STR 15 (DOOR TYPE 1) NOTE: THRESHOLD IS NEXT 4C CHECK

200

533181-01-3

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH: - FROM STR 5 TO STR 13 (DOOR TYPE A) - FROM STR 5 TO STR 15 (DOOR TYPE 1)

AMM 533100-200-855

275

N

AMM 533100-200-848

294

I


SDI

MAIN STRUCTURE

N

T

97 300 FH

T

27 700 CY

299

I

49 800 FH

366

I

14 200 CY

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [42 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533181-01-3S020

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH: - FROM STR 5 TO STR 13 (DOOR TYPE A) - FROM STR 5 TO STR 15 (DOOR TYPE 1) NOTE: THRESHOLD IS NEXT 4C CHECK

R

200

533181-01-7

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH: - FROM STR 5 TO STR 13 (DOOR TYPE A) - FROM STR 5 TO STR 15 (DOOR TYPE 1)

Threshold Interval

References

Ctrl

Eff

N

AMM 533100-200-848

275

N

AMM 533100-200-848

943

T

60 000 FH

T

20 000 CY

I

49 800 FH

I

14 200 CY

T

60 000 FH

T

17 000 CY

I

86 400 FH

962

13 300 CY

1019

I

946

1256 1266

Skills :

1.00 MHrs

1 NDT 147 148

533187-01-1

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FR 48 AND FR 49, AT Y-1456 AND Y+1456.

T

159 000 FH

T

23 500 CY

I

8 500 CY

N

ALI 533187-01-01 AMM 533100-250-854

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

0.00 MHrs

: 01 : 06/09/2014

299 366

Skills :

1 NDT

294

Page : ALI - 53 [43 / 59] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533187-01-1S020

147 148

147 148

533187-01-4

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FR 48 AND FR 49, AT Y-1456 AND Y+1456. NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

8 500 CY See note

References

Ctrl

Eff

N

AMM 533100-250-854

275

N

AMM 533100-250-854

943

Check : NT

SDI

MAIN STRUCTURE

Threshold Interval

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FR 48 AND FR 49, AT Y-1456 AND Y+1456.

T

159 000 FH

T

23 500 CY

I

8 500 CY

946 962 1019 1256 1266

R

200

533194-01-2

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

N

AMM 533100-200-849

943

T

99 900 FH

T

14 700 FC

I

39 800 FH

962

5 800 CY

1019

I

946

1256 1266

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [44 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533194-01-9

200

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 533100-200-849

Eff 275

T

137 400 FH

T

20 300 FC

294

I

64 600 FH

299

I

9 500 CY

366

T

97 300 FH

T

14 300 FC

I

39 800 FH

962

5 800 CY

1019

Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

100

533195-02-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. PREP. : SCUFF PLATE

I

N

AMM 533100-200-850

943 946

1256 1266

Skills :

4.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [45 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

533195-02-9

100

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 533100-200-850

Eff 275

T

137 400 FH

T

20 300 CY

294

I

64 600 FH

299

I

9 500 CY

366

T

4 500 FC

I

4 500 CY

T

6 900 FC

I

6 900 CY

T

172 200 FH

T

28 000 CY

299

I

57 000 FH

366

I

19 000 CY

Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

4.00 MHrs

1 NDT D

200

533197-01-1

GVI

MAIN STRUCTURE

GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 53.3 AND FR 54 FROM STRINGER 6 LH TO STRINGER 6 RH, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-02-1 R

200

533197-02-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 53.3 AND FR 54 FROM STRINGER 6 LH TO STRINGER 6 RH, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-01-1

200

534105-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

N

ALI 533197-01-01 AMM 533100-210-819

ALL

N

ALI 533197-02-01 AMM 533100-220-931

ALL

N

AMM 534100-210-802

294

Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [46 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534105-01-4S020

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE. NOTE: THRESHOLD IS NEXT 4C CHECK

R

200

534105-01-6

DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

T

60 000 FH

T

20 000 CY

I

57 000 FH

I

19 000 CY See note

References

Ctrl

Eff

N

AMM 534100-210-802

275

N

AMM 534100-210-802

943

Check : NT

DI

MAIN STRUCTURE

Threshold Interval

T

60 000 FH

T

17 000 CY

I

87 400 FH

962

I

13 400 CY

1019

946

1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [47 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534107-01-2

263 264 273 274

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL SKIN SPLICE AT STR 7, AND STR 11 TO STR 13, AT JOINTS AND CIRCUMFERENTIAL SKIN PREP. : CEILING PANELS Z260; INSULATION Z260; OVERHEAD STOWAGE BINS Z260;

SPLICE PLATE AT FR 72, FROM STR 3 TO INTERSECTION OF LAP SPLICE, LH/RH

Threshold Interval

References

Ctrl

N

AMM 534100-220-802

Eff 294

T

183 200 FH

T

28 300 CY

299

I

49 900 FH

366

I

16 700 CY

T

60 000 FH

T

20 000 CY

I

49 900 FH

I

16 700 CY

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 534107-01-2S020

Issue No

:

Date

:

263 264 273 274

10 01/12/2013

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

SDI

N

AMM 534100-220-802

Page : ALI - 53 [48 / 59] ATA

: 53

275


R

53

FUSELAGE

Task Number

Zone

534107-01-4

263 264 273 274

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH PREP. : CEILING PANELS Z260; INSULATION Z260; OVERHEAD STOWAGE BINS Z260;

Threshold Interval

References

Ctrl

N

AMM 534100-220-802

Eff 943

T

60 000 FH

T

17 000 CY

I

73 000 FH

962

11 200 CY

1019

I

946

1256 1266

Skills :

0.80 MHrs

1 NDT R

200

534108-01-2

DI


T

185 600 FH

T

22 600 CY

I

146 300 FH

I

22 600 CY

N

ALI 534108-01-02 AMM 534100-210-842

275 943 946 962 1019 1256 1266

Skills :

0.40 MHrs

1 AF 534108-01-2S100

200


Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

N

AMM 534100-210-842

294

T

185 600 FH

T

28 500 CY

299

I

146 300 FH

366

I

22 600 CY

Page : ALI - 53 [49 / 59] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

534110-01-2

200 300

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM STRINGERS 6 TO 13 LH/RH, EXTERNAL SURFACE. NOTE: MSN 275 THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

17 000 CY

I

146 300 FH

I

22 600 CY

References

Ctrl

N

ALI 534110-01-02 AMM 534100-210-843

Eff 275 943 946 962 1019 1256 1266

Skills :

0.40 MHrs

1 AF 534110-01-2S100

R

200 300

200

534120-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM STR 6 TO STR 13 LH/RH, EXTERNAL SURFACE.

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PART OF WINDOW FORGINGS BETWEEN FR 53.8 AND FR 73 AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNAL SURFACE.

N

AMM 534100-210-843

294

T

185 600 FH

T

28 500 CY

299

I

146 300 FH

366

I

22 600 CY

T

106 900 FH

T

16 400 FC

I

106 900 FH

962

I

16 400 CY

1019

N

AMM 534100-210-844

943 946

1256 1266

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [50 / 59] ATA

: 53


D

53

FUSELAGE

Task Number

Zone

534126-01-2

100

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH TO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR 54 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-02-2.

Threshold Interval

T

2 200 FC

I

2 200 CY

T

6 900 FC

I

6 900 CY

References

Ctrl

Eff

N

AMM 534100-210-804

ALL

N

AMM 534100-200-822

ALL

Skills :

10.00 MHrs

1 AF 100

534126-02-2

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH TO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR 54 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-01-2.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

Page : ALI - 53 [51 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534131-01-2

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

Threshold Interval

References

Ctrl

N

AMM 534100-220-803

Eff 275

T

36 900 FH

T

10 500 FC

294

I

36 900 FH

299

I

10 500 CY

366

T

52 400 FH

T

8 000 FC

I

52 400 FH

962

8 000 CY

1019

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 NDT R

200

534131-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

I

N

AMM 534100-220-803

943 946

1256 1266

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [52 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534132-02-1

100 200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE LH/RH

Threshold Interval

T

22 800 FC

I

10 500 CY

T

52 100 FH

T

17 300 FC

T

6 YE

I

52 100 FH

I

17 300 CY

I

6 YE

References

Ctrl

Eff

N

AMM 534100-220-804

ALL

N

AMM 534100-210-847

ALL

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

4.00 MHrs

1 NDT 152

534139-01-3

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A AND FR 65). TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 note:CPCP Access panels :


0.00 Hrs

Skills :

0.25 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [53 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534140-02-1

152

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL FOR AFT BETWEEN TPS :

VISUAL INSPECTION OF LOCK FITTINGS AND BUSHES CARGO COMPARTMENT DOOR AT 10 POSITIONS FR 59A AND FR 65. APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

Threshold Interval

T

5 900 FC

References

Ctrl

Eff

N

AMM 534100-200-814

ALL

N

AMM 534100-210-806

275

T

6 YE

I

5 900 CY

I

6 YE

T

19 200 FH

T

5 500 FC

294

I

19 200 FH

299

I

5 500 CY

366

T

45 300 FH

T

6 900 FC

I

45 300 FH

962

I

6 900 CY

1019

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF 100

534143-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN OF BULK CARGO COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE.

Skills :

0.20 MHrs

1 AF R

100

534143-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN OF BULK CARGO COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE.

N

AMM 534100-210-806

943 946

1256 1266

Skills :

0.20 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [54 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534144-01-2

100

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE NOTE: REFFER TASK 534144-01-1 FOR LAST ACCOMPLISHMENT

Threshold Interval

References

Ctrl

N

AMM 534100-200-811

Eff 275

T

70 600 FH

T

23 400 FC

294

T

12 YE

299

I

16 100 FH

I

5 300 CY

I

6 YE

T

60 000 FH

T

17 000 CY

T

12 YE

366

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF R

100

534144-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE NOTE: CPCP

I

45 300 FH

I

6 900 CY

I

6 YE

N

AMM 534100-200-811

946 962 1019 1256 1266

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : ALI - 53 [55 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534149-01-1

162

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 67 AND FR 69) AS FAR AS VISIBLE note:CPCP

Threshold Interval

T

3 600 FC

T

6 YE

I

3 600 CY

I

6 YE

T

29 400 CY

I

12 700 CY

T

11 800 CY

I

9 700 CY

References

Ctrl

Eff

N

AMM 534100-200-815

ALL

N

ALI 534150-01-05 AMM 53-41-00-210-872

ALL

N

AMM 534100-210-851

ALL

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF 534150-02-5

534154-01-4

Issue No

:

Date

:

150 160

MAIN STRUCTURE

271 272

MAIN STRUCTURE

10 01/12/2013

DI

DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OF CARGO FLOOR ATTACHMENT FITTINGS, FROM FR 54 TO FR 64 LH AND FROM FR 54 TO FR 58 RH, BETWEEN STR 39 AND STR 45 FROM FR 65 TO FR 69 LH, BETWEEN STR 41 AND STR 50. DI

DETAILED INSPECTION OF INTERNAL STRUCTURE OF TORSION BOX, INCLUDING SKIN AND SPLICE PLATE, BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 AND FR 76, LH/RH. NOTE: THIS TASK REPLACE TASK 534154-01-2. USE LAST DONE OF TASK 534154-01-2 FOR CALCULATING THE NEXT DUE

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [56 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

534155-01-2

271 272

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF TORSION BOX LONGITUDINAL BEAM ADJACENT TO RUNOUT OF CORNER DOUBLER BETWEEN FR 73A AND FR 74, LH/RH.

Threshold Interval

References

Ctrl

Eff

N

AMM 534100-220-806

ALL

N

AMM 534100-200-809

275

T

20 000 FC

I

8 000 CY

T

30 600 FC

T

6 YE

294

I

30 600 CY

299

I

6 YE

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.50 MHrs

1 NDT 154

534156-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND 67, FROM CARGO FLOOR LEVEL TO STR 47 RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : BALL MATS Z150; CARGO FLOOR PANELS Z150; INSULATION Z150;

366

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 53 [57 / 59] ATA

: 53


D

53

FUSELAGE

Task Number

Zone

534177-01-3

200

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER LINE, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-3.

200

534177-02-3

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER LINE, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-01-3.

311 312

535103-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND CROWN CENTER LINE

Threshold Interval

T

4 500 FC

I

4 500 CY

T

6 900 FC

I

6 900 CY

T

16 500 FC

I

7 500 CY

References

Ctrl

N

AMM 534100-210-869

ALL

N

AMM 534100-220-819

ALL

N

AMM 535100-200-803

275 294 299 366

Access panels :


0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff

Page : ALI - 53 [58 / 59] ATA

: 53


53

FUSELAGE

Task Number

Zone

535104-02-1

311 312

Task Title

Task code

GVI

MAIN STRUCTURE

Threshold Interval

I

5 100 CY

References

Ctrl

N

AMM 535100-210-801

299 366

Access panels :

312AR 0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275 294

GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND BOTTOM CENTER LINE

Total access time :

Eff

Page : ALI - 53 [59 / 59] ATA

: 53


54

NACELLES / PYLONS

Task Number

Zone

545104-02-13

453 463

Task Title

Task code

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON PYRAMID ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB2 (2 FASTENER LOCATION/PYLON)

Threshold Interval

References

Ctrl

N

ALI 545104-02-13 AMM 545100-250-804

Eff 275

T

46 900 FH

T

13 400 FC

I

4 500 FH

299

I

1 300 CY

366

T

18 600 FH

T

6 100 CY

294

I

18 600 FH

299

I

6 100 CY

366

T

52 600 FH

T

8 100 CY

I

52 600 FH

962

8 100 CY

1019

294

Skills :

0.00 MHrs

1 NDT 453

545108-04-1

DI

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 TPS : TPS MUST NOT BE APPLIED NOTE: USE LAST DONE OF TASK 545108-04-2 FOR CALCULATING THE NEXT DUE

R

545108-04-12

453 463

DI

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 TPS : TPS MUST NOT BE APPLIED

I

N

N

AMM 545100-200-919

AMM 545100-200-919

275

943 946

1256 1266

R

453 463

545129-01-3

DI

PYLON BOX DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 ACCESS: 454DL 454DR 464DL 464DR

T

50 000 FH

T

17 000 CY

I

27 700 FH

I

8 500 CY

N

ALI 545129-01-03 AMM 545100-200-912 MRB 545129-01-3

275 943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 54 [1 / 9] ATA

: 54


R

D

54

NACELLES / PYLONS

Task Number

Zone

545129-01-3S100

453 463

400

545140-01-8

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 ACCESS: 454DL 454DR 464DL 464DR

DI

PYLON BOX DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-8 NOTE: THE ALI TASK SUPERSEDES THE AOT A330-54A3025. FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THE ALI INTERVAL (2930 FC OR 14680 FH).

R

545140-02-14

400

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

Threshold Interval

References

Ctrl

N

ALI 545129-01-03 AMM 545100-200-912

Eff 294

T

143 500 FH

T

21 200 CY

I

45 300 FH

I

6 700 CY See note

T

29 000 FH

T

8 300 FC

I

10 500 FH

299

I

3 000 CY

366

T

48 700 FH

T

7 500 FC

I

33 100 FH

962

5 100 CY

1019

I

299 366

N

N

ALI 545140-01-08 AMM 545100-200-915

AMM 545100-270-804

275 294

943 946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 54 [2 / 9] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545140-02-8

400

Task Title

Task code

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-8 NOTE: THE ALI TASK SUPERSEDES THE AOT A330-54A3025. FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THE ALI INTERVAL (5400 FC OR 27030 FH).

R

453 463

545142-02-7

DI

PYLON BOX DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14 note:CPCP

Threshold Interval

References

Ctrl

N

ALI 545140-02-08 AMM 545100-270-804

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

29 000 FH

T

8 300 FC

I

19 600 FH

299

I

5 600 CY

366

T

70 200 FH

T

10 800 FC

T

6 YE

I

70 200 FH

I

10 800 CY

I

6 YE

N

AMM 545100-200-920

294

943 946 962 1019 1256 1266

0.80 MHrs

: 01 : 06/09/2014

275

T

Skills :

1 AF

Eff

Page : ALI - 54 [3 / 9] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545142-02-9

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14 TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

Threshold Interval

T

25 900 FH

T

7 400 FC

T

6 YE

I

25 900 FH

I

7 400 CY

I

6 YE

T

182 600 FH

T

28 100 CY

I

38 500 FH

I

11 000 CY

References

Ctrl

N

ALI 545142-02-09 AMM 545100-200-920

Eff 275 294 299 366

Access panels :

453CL

453CR

Total access time :

463CL 463CR 0.00 Hrs

Skills :

0.80 MHrs

1 AF D

453 463

545146-03-7

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - HIGH FREQUENCY EDDY CURRENT INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-7 PREP. : AIR DUCT; PRE-COOLER; RODS;

N

ALI 545146-03-07 AMM 545100-250-808

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

0.00 MHrs

: 01 : 06/09/2014

299 366

Skills :

1 NDT

294

Page : ALI - 54 [4 / 9] ATA

: 54


D

54

NACELLES / PYLONS

Task Number

Zone

545146-03-7S020

453 463

453 463

545146-04-7

Task Title

Task code

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - HIGH FREQUENCY EDDY CURRENT INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-7S020 PREP. : AIR DUCT; PRE-COOLER; RODS; NOTE: THRESHOLD IS NEXT 4C CHECK

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - INSPECTION THROUGH FLEXIBLE BOROSCOPE - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-7 PREP. : AIR DUCT; PRE-COOLER; RODS;

T

60 000 FH

T

20 000 CY

I

38 500 FH

I

11 000 CY See note

References

Ctrl

N

AMM 545100-250-808

275

T

182 600 FH

N

ALI 545146-04-07 AMM 545100-200-917

294

T

28 100 CY

I

22 700 FH

I

6 500 CY

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

0.00 MHrs

: 01 : 06/09/2014

299 366

Skills :

1 NDT

Eff

Check : NT

SDI

PYLON BOX

Threshold Interval

Page : ALI - 54 [5 / 9] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545146-04-7S020

453 463

453 463

545150-02-11

Task Title

Task code

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - INSPECTION THROUGH FLEXIBLE BOROSCOPE - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-7S020 PREP. : AIR DUCT; PRE-COOLER; RODS; NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

22 700 FH

I

6 500 CY See note

References

Ctrl

Eff

N

AMM 545100-200-917

275

N

ALI 545150-02-11 AMM 545100-200-918

294

Check : NT

DI

PYLON BOX

Threshold Interval

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 PREP. : AIR DUCT; PRE-COOLER; RODS;

T

216 400 FH

T

33 300 CY

I

38 800 FH

I

11 100 CY

T

60 000 FH

T

20 000 CY

I

38 800 FH

299 366

Skills :

0.20 MHrs

1 AF 545150-02-11S020

Issue No

:

Date

:

453 463

10 01/12/2013

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 PREP. : AIR DUCT; PRE-COOLER; RODS; NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

N

AMM 545100-200-918

I


Page : ALI - 54 [6 / 9] ATA

: 54

275


R

R

54

NACELLES / PYLONS

Task Number

Zone

545150-02-2

453 463

454 464

545168-02-13

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 PREP. : AIR DUCT; PRE-COOLER; RODS;

DI

PYLON TO WING LINKS DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) NOTE: THRESHOLD IS NEXT 4C CHECK FOR MSN 275

Threshold Interval

References

Ctrl

N

ALI 545150-02-02 ALI 545150-02-2 AMM 545100-200-918

Eff 275

T

153 600 FH

T

24 100 FC

I

34 200 FH

I

5 400 CY

T

60 000 FH

T

17 000 CY

I

24 300 FH

946


1019

294 299 366

N

ALI 545168-02-13 AMM 545117-200-816

I

275 943

1256 1266

Access panels :

452CL 464BR

452CR

454BL

Total access time :

454BR

462CL

462CR

464BL

0.86 Hrs

Skills :

1.60 MHrs

1 AF R

545168-02-13S100

454 464

DI

PYLON TO WING LINKS DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON)

T

84 600 FH

T

25 900 FC

I

14 700 FH

I

4 500 CY

N

ALI 545168-02-13 AMM 545117-200-816

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

1.60 MHrs

: 01 : 06/09/2014

299 366

Skills :

1 AF

294

Page : ALI - 54 [7 / 9] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545174-02-5S100

454 464

Task code

Task Title

DI


Threshold Interval

References

Ctrl

N

Eff 943

T

100 000 FH

T

33 000 FC

I

65 600 FH

962

10 100 CY

1019

I

946

1256 1266

454 464

545174-02-9

DI


T

100 000 FH

T

20 700 CY

I

26 200 FH

I

7 500 CY

T

100 000 FH

T

33 000 FC

I

26 200 FH

I

7 500 CY

N

ALI 545174-02-09 AMM 545117-200-812

275

N

ALI 545174-02-09 AMM 545117-200-812

294

Access panels :

454KL 464MR

454KR

Total access time :

454ML

454MR

464KL

464KR

464ML

0.00 Hrs

Skills :

0.40 MHrs

1 AF 545174-02-9S100

454 464

DI


366

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 54 [8 / 9] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545180-04-6

454 464

Task Title

Task code

SDI

PYLON TO WING FITTING SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) PREP. : AFT SECONDARY STRUCTURE; ENGINE; LINKS; SLEEVES; NOTE: RII TASK

Threshold Interval

References

Ctrl

N

AMM 545117-230-801

Eff 275

T

92 300 FH

T

14 200 FC

294

I

73 400 FH

299

I

11 300 CY

366 943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 54 [9 / 9] ATA

: 54


R

55

STABILIZERS

Task Number

Zone

551019-01-4

311 312

Task Title

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO REAR SPAR WEB FROM RIB 3LH TO RIB 3RH

Task code

SDI

Threshold Interval

References

Ctrl

N

AMM 551100-200-809

Eff 943

T

60 000 FH

T

17 000 CY

I

20 200 FH

962

3 100 CY

1019

I

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 55 [1 / 1] ATA

: 55


57

WINGS

Task Number

Zone

571102-01-1

137 138

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 LEVEL, LH/RH PREP. : AIR CONDITIONING DUCTS; LINING; NOTE 1; NOTE: NEW TASK REPLACE TASK 571102-01-4

Threshold Interval

References

Ctrl

N

ALI 571102-01-01 AMM 571100-220-806

Eff 275

T

75 400 FH

T

15 000 FC

I

25 100 FH

299

I

5 000 CY

366

T

60 000 FH

T

17 000 FC

I

25 700 FH

962

5 140 CY

1019

294

Access panels :


0.02 Hrs

Skills :

0.20 MHrs

1 AF R

571102-01-6S020

137 138

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 LEVEL, LH/RH PREP. : AIR CONDITIONING DUCTS LINING

I

N

AMM 571100-220-806

946

1256 1266

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : ALI - 57 [1 / 72] ATA

: 57


D

57

WINGS

Task Number

Zone

571103-01-4

137 138

137 138

571103-02-4

130 190

571104-01-4

Issue No

:

Date

:

10 01/12/2013

Task Title

MAIN STRUCTURE

Task code

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH NOTES : - ROTOTEST INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-4 PREP. : AIR CONDITIONING DUCTS FASTENER (2 POSITIONS) LINING MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH NOTES : - HIGH FREQUENCY EDDY CURRENT INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-4 PREP. : AIR CONDITIONING DUCTS LINING; NOTE 1; NOTE: REFER TASK 571103-01-4 MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENERS BETWEEN STR 38 AND 39, LH/RH

Amendment No Date

: 01 : 06/09/2014

SDI

Threshold Interval

References

Ctrl

N

AMM 571100-280-801

Eff 275

T

72 000 FH

T

14 400 FC

294

I

30 200 FH

299

I

6 000 CY

366

T

72 000 FH

T

14 400 FC

I

4 650 FH

299

I

930 CY

366

T

97 800 FH

T

19 500 FC

I

28 000 FH

299

I

5 600 CY

366

N

N

ALI 571103-02-04 AMM 571100-200-817

ALI 571104-01-04 AMM 571100-250-810

Page : ALI - 57 [2 / 72] ATA

: 57

275 294

275 294


57

WINGS

Task Number

Zone

571107-01-1

195 196

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & 21, LH/RH

Threshold Interval

T

50 000 FH

T

20 000 FC

I

20 400 FH

I

5 850 CY

T

123 400 FH

T

35 200 FC

I

20 400 FH

I

5 850 CY

References

Ctrl

Eff

N

ALI 571107-01-01 AMM 571100-200-830

275

N

ALI 571107-01-01 AMM 571100-200-830

294

Access panels :

191QB

192QB

Total access time :

5.56 Hrs

Skills :

0.40 MHrs

1 NDT 571107-01-1S100

195 196

SDI


366

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [3 / 72] ATA

: 57


57

WINGS

Task Number

Zone

571108-01-6

141 142

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. PREP. : FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

28 800 FH

I

8 200 CY See note

References

Ctrl

Eff

N

ALI 571108-01-06 AMM 571100-200-813

275

N

ALI 571108-01-06 AMM 571100-200-813

294


147AZ

148AZ

Total access time :

734

744

0.00 Hrs

Skills :

0.00 MHrs

1 AF 571108-01-6S100

141 142

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS.

T

135 300 FH

T

38 600 FC

I

28 800 FH

I

8 200 CY

366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [4 / 72] ATA

: 57


57

WINGS

Task Number

Zone

571114-01-6

141 142

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. (20 DRAIN HOLES LOCATIONS)

Threshold Interval

T

60 000 FH

T

20 000 CY

I

42 000 FH

I

12 000 CY

T

91 500 FH

T

26 100 FC

I

42 000 FH

I

12 000 CY

T

60 000 FH

T

20 000 CY

I

20 400 FH

I

5 800 CY

References

Ctrl

Eff

N

ALI 571114-01-06 AMM 571100-200-832

275

N

ALI 571114-01-06 AMM 571100-200-832

294

Access panels :

147AZ

148AZ

Total access time :

734 744 0.00 Hrs

Skills :

0.00 MHrs

1 NDT 571114-01-6S100

141 142

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. (20 DRAIN HOLES LOCATIONS)

299 366

Skills :

0.00 MHrs

1 NDT 193

571116-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN STRINGERS 21 & 22, AT Y =-567.5

N

ALI 571116-01-02 AMM 571100-200-834

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [5 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

571116-01-2S100

193

Task Title

Task code

SDI


Threshold Interval

T

123 400 FH

T

35 200 FC

I

20 400 FH

I

5 800 CY

T

60 000 FH

T

20 000 CY

I

20 400 FH

I

5 800 CY

T

123 400 FH

T

35 200 FC

I

20 400 FH

I

5 800 CY

References

Ctrl

N

ALI 571116-01-02 AMM 571100-200-834

Eff 294 299 366

Skills :

0.20 MHrs

1 NDT 143 195

571118-01-6

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEEN STRINGERS 27 & 28.. PREP. : FAIRING PANELS BETWEEN FR 44 AND FR 47;

N

ALI 571118-01-06 AMM 571100-200-833

275

N

ALI 571118-01-06 AMM 571100-200-833

294

Skills :

0.20 MHrs

1 NDT 571118-01-6S100

143 195

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEEN STRINGERS 27 & 28.. PREP. : FAIRING PANELS BETWEEN FR 44 AND FR 47;

366

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [6 / 72] ATA

: 57


57

WINGS

Task Number

Zone

571119-01-1

145 146

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LONGITUDINAL BEAMS ABOVE CWB, WEB HOLE AREA BETWEEN FRAMES 41 AND 42 FROM Y=-1456 TO Y=1456. (7 BEAMS TO BE INSPECTED)

Threshold Interval

T

20 000 FC

I

3 100 CY

T

33 000 FC

I

3 100 CY

References

Ctrl

Eff

N

AMM 571100-250-802

275

N

ALI 571119-01-01 AMM 571100-250-802

294

Skills :

0.00 MHrs

1 NDT 571119-01-1S100

145 146

147 148

571121-01-3

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LONGITUDINAL BEAMS ABOVE CWB, WEB HOLE AREA BETWEEN FRAMES 41 AND 42 FROM Y=-1456 TO Y=1456. (7 BEAMS TO BE INSPECTED)

366

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1959. (9 ASSY TO BE INSPECTED)

T

116 800 FH

T

18 700 CY

I

116 800 FH

I

18 700 CY

N

ALI 571121-01-03 AMM 571100-200-818

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [7 / 72] ATA

: 57

275


R

57

WINGS

Task Number

Zone

571121-01-3S100

147 148

571121-01-5S020

147 148

Task Title

Task code

SDI


SDI


Threshold Interval

References

Ctrl

N

ALI 571121-01-03 AMM 571100-200-818

Eff 294

T

152 800 FH

T

24 500 CY

I

116 800 FH

I

18 700 CY

T

60 000 FH

T

17 000 CY

I

121 900 FH

962

I

18 700 CY

1019

299 366

N

ALI 571121-01-05 AMM 571100-200-818

943 946

1256 1266

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

1.20 MHrs

1 NDT 145 146

571123-01-3

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH. PREP. : NOTE 1;

Amendment No Date

: 01 : 06/09/2014

SDI

N

AMM 571100-200-820

294

T

80 400 FH

T

22 900 CY

299

I

29 100 FH

366

I

8 300 CY

Page : ALI - 57 [8 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

571123-01-3S020

145 146

191 192 195 196

571123-01-5

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH. PREP. : INSULATION Z250; LOWER SIDEWALL PANELS Z250; NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

29 100 FH

I

8 300 CY See note

References

Ctrl

Eff

N

AMM 571100-200-820

275

N

ALI 571123-01-05 AMM 571100-200-820

943

Check : NT

SDI

MAIN STRUCTURE

Threshold Interval

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH. CABIN FLOOR PANELS NOTE 1

T

60 000 FH

T

17 000 CY

I

34 400 FH

962

5 200 CY

1019

I

946

1256 1266

147 148

571125-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND FRAME 47 LOWER CORNER FITTING, LH/RH. NOTE: MSN 275 BECOME SAMPLE A/C THRESHOLD IS 18000 FC OR 72000 FH

N

AMM 571100-200-825

78 300 FH

T

22 300 CY

294

I

14 700 FH

299

I

4 200 CY

366

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 57 [9 / 72] ATA

: 57


57

WINGS

Task Number

Zone

571126-01-4

147

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR SPARE WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 FC

I

40 200 FH

I

11 500 CY See note

References

Ctrl

Eff

N

AMM 571100-200-826

275

N

AMM 571100-200-826

294



0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

571126-01-4S100

147

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR SPARE WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER.

T

96 400 FH

T

27 500 FC

299

I

40 200 FH

366

I

11 500 CY

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [10 / 72] ATA

: 57


57

WINGS

Task Number

Zone

571130-01-4

141 142 147 148

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

23 900 FH

I

7 300 CY See note

References

Ctrl

Eff

N

ALI 571130-01-04 AMM 571100-200-827

275

N

ALI 571130-01-04 AMM 571100-200-827

294


147AZ

148AZ

Total access time :

734

744

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 571130-01-4S100

141 142 147 148

141 142

571133-01-1

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE

SDI

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES).

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES). PREP. : FUEL TANK DRAINED AND VENTED;

Amendment No Date

: 01 : 06/09/2014

DI

T

122 600 FH

T

37 500 FC

I

23 900 FH

I

7 300 CY See note

T

112 100 FH

T

32 600 CY

299

I

54 900 FH

366

I

15 900 CY

299 366

N

AMM 571100-200-815

Page : ALI - 57 [11 / 72] ATA

: 57

294


57

WINGS

Task Number

Zone

571133-01-1S020

141 142

141 142

571145-01-3

Task Title

Task code

DI


SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

77 600 FH

T

20 000 CY

I

54 900 FH

I

15 900 CY

T

60 000 FH

T

20 000 CY

I

29 500 FH

References

Ctrl

Eff

N

AMM 571100-200-815

275

N

ALI 571145-01-03 AMM 571100-270-803

275

N

ALI 571145-01-03 AMM 571100-270-803

294

I


Access panels :

147AZ

148AZ

Total access time :

734 744 0.00 Hrs

Skills :

0.00 MHrs

1 NDT 571145-01-3S100

141 142

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.

T

110 300 FH

T

31 500 FC

I

29 500 FH

I

8 400 CY

366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [12 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

571145-01-5S020

141 142

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.

Threshold Interval

References

Ctrl

N

ALI 571145-01-05 AMM 571100-270-803

Eff 943

T

60 000 FH

T

17 000 CY

I

42 400 FH

962

6 500 CY

1019

I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734

744

1.08 Hrs

Skills :

0.80 MHrs

1 NDT 191 192 195 196

571146-02-5

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

29 200 FH

N

AMM 571100-270-804

I


Access panels :

191HB

191QB

Total access time :

192HB 192QB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [13 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

571146-02-5S100

191 192 195 196

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH

Threshold Interval

References

Ctrl

N

AMM 571100-270-804

Eff 294

T

101 700 FH

T

29 000 FC

299

I

29 200 FH

366

I

8 300 CY

T

60 000 FH

T

17 000 CY

I

43 500 FH

962

6 600 CY

1019

Skills :

0.00 MHrs

1 NDT R

571146-02-7S020

191 192 195 196

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH

I

N

AMM 571100-270-804

943 946

1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [14 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

571153-01-2S100

141 142

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH PREP. : SEALANT TO BE REMOVED;

Threshold Interval

References

Ctrl

N

AMM 571100-250-809

Eff 943

T

107 900 FH

T

16 600 FC

I

74 800 FH

962

11 500 CY

1019

I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734 744 1.08 Hrs

Skills :

0.50 MHrs

1 NDT 141 142

571153-01-6

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH PREP. : SEALANT TO BE REMOVED;

N

ALI 571153-01-06 AMM 571100-250-809

63 800 FH

T

18 200 FC

I

49 800 FH

299

I

14 200 CY

366

Access panels :

147AZ

148AZ

Total access time :

734 744 1.08 Hrs

Skills :

0.50 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 57 [15 / 72] ATA

: 57

294


57

WINGS

Task Number

Zone

571159-01-4

145 146

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPARE VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

30 000 FH

I

9 200 CY See note

References

Ctrl

Eff

N

ALI 571159-01-04 AMM 571100-200-823

275

N

ALI 571159-01-04 AMM 571100-200-823

294

Check : NT Skills :

0.00 MHrs

1 NDT 571159-01-4S100

145 146

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPARE VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS)

T

91 700 FH

T

28 000 FC

I

30 000 FH

I

9 200 CY

T

35 600 FH

T

10 900 FC

I

17 100 FH

I

5 250 CY

299 366

Skills :

0.00 MHrs

1 NDT 191 192

571163-01-2

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FRAME 40 NODE, FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAM FITTING AND LOWER PANEL, LH/RH. NOTE: TASK APPLICABLE BEFORE

Amendment No Date

: 01 : 06/09/2014

SDI

N

ALI 571163-01-02 AMM 571100-270-815

275 294 299

Page : ALI - 57 [16 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

571164-01-2

191 192

Task Title

MAIN STRUCTURE

Task code

DI

DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, KEEL BEAM FITTING ANGLE AND DOUBLER AT FR 40, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 571100-220-814

Eff 943

T

106 900 FH

T

16 400 CY

I

44 900 FH

962

6 900 CY

1019

I

946

1256 1266

541 641

572004-02-1

572004-02-1S020

Issue No

:

Date

:

541 641

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING PREP. : FUEL PUMP FAIRINGS

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING PREP. : FUEL PUMP FAIRINGS NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

N

AMM 572000-210-822

294

T

117 300 FH

T

33 500 FC

299

I

20 600 FH

366

I

5 800 CY

T

60 000 FH

T

20 000 CY

I

20 600 FH

N

AMM 572000-210-822

I


Page : ALI - 57 [17 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

572005-01-7

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SK FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR SPAR. PREP. : AIRCRAFT JACKING; FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

Eff

N

ALI 572005-01-07 AMM 572000-220-851

275

N

ALI 572005-01-07 AMM 572000-220-851

294

T

60 000 FH

T

20 000 CY

I

15 300 FH

I

4 300 CY See note

T

100 000 FH

T

28 500 FC

I

15 300 FH

I

4 300 CY See note

T

124 100 FH

T

35 400 FC

I

26 400 FH

299

I

7 500 CY

366

Access panels :

541CB

641CB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 572005-01-7S100

541 641

500 600

572006-02-9

Issue No

:

Date

:

10 01/12/2013

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR SPAR.

GVI

OUTER WING DETAILED INSPECTION OF OUTER WING LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE

Amendment No Date

: 01 : 06/09/2014

299 366

N

ALI 572006-02-09 AMM 572000-210-829

Page : ALI - 57 [18 / 72] ATA

: 57

275 294


57

WINGS

Task Number

Zone

572009-01-4

540 640

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 PREP. : FIXED FLAP TRACK FAIRING Z531; FUEL PUMP FAIRINGS Z500; FIXED FLAP TRACK FAIRING Z631; FUEL PUMP FAIRINGS Z600;

Threshold Interval

T

60 000 FH

T

20 000 CY

I

20 200 FH

I

5 700 CY

T

101 900 FH

T

29 100 FC

I

20 200 FH

I

5 700 CY See note

References

Ctrl

Eff

N

AMM 572000-210-807

275

N

ALI 572009-01-04 AMM 572000-210-807

294

Access panels :

454GL

454GR

Total access time :

464GL 464GR 0.00 Hrs

531AB

631AB

Skills :

0.00 MHrs

1 AF 572009-01-4S100

Issue No

:

Date

:

531 631

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT ""5400 FC OR 21700 FH "" FROM APPROVE DATE"

Amendment No Date

: 01 : 06/09/2014

299 366

Check : NT

Page : ALI - 57 [19 / 72] ATA

: 57


D

57

WINGS

Task Number

Zone

572009-02-4

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: APPLY TASK 572009-01-4

Threshold Interval

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

15 000 CY See note

References

Ctrl

Eff

N

ALI 572009-02-04 AMM 572000-210-823

275

N

ALI 572009-02-04 AMM 572000-210-823

294

Check : NT

Access panels :

454GL

454GR

Total access time :

464GL 464GR 0.00 Hrs

Skills :

0.00 MHrs

1 NDT D

572009-02-4S100

Issue No

:

Date

:

541 641

10 01/12/2013

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4S100 PREP. : FIXED FLAP TRACK FAIRING Z531; FUEL PUMP FAIRINGS Z500; FIXED FLAP TRACK FAIRING Z631; FUEL PUMP FAIRINGS Z600;

Amendment No Date

: 01 : 06/09/2014

T

101 900 FH

T

29 100 FC

I

50 000 FH

I

15 000 CY

299 366

Page : ALI - 57 [20 / 72] ATA

: 57


57

Task Number

Zone

572012-02-1

500 600

572012-02-1S100

R

WINGS

572016-02-9S020

500 600

500 600

Task Title

Task code

DI

WING BOTTOM SKIN DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING PLATE. PREP. : FUEL PUMP FAIRINGS

DI


SDI

OUTER WING SPECIAL VISIBLE AND RIB PREP. :

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 4. FUEL PUMP FAIRINGS

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-826

275

N

AMM 572000-210-826

294

T

60 000 FH

T

20 000 CY

I

19 900 FH

I

5 600 CY

T

122 700 FH

T

35 000 FC

299

I

19 900 FH

366

I

5 600 CY

T

60 000 FH

T

17 000 CY

I

34 400 FH

962

5 300 CY

1019

I

N

ALI 572016-02-09 AMM 572000-210-813

943 946

1256 1266

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [21 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572019-01-5

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS UPPER SURFACE BETWEEN FRONT SPAR AND STRINGER 8 AND BOTTOM STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING STRINGERS 15 & 18 AND BUTTSTRAPS STRINGERS 13 & 20. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-841

275

N

AMM 572000-210-841

294

T

60 000 FH

T

20 000 CY

I

27 800 FH

I

7 900 CY See note

T

127 000 FH

T

36 200 FC

299

I

27 800 FH

366

I

7 900 CY

Access panels :

541EB

541FB

Total access time :

541GB 641EB 0.00 Hrs

641FB

641GB

Skills :

2.00 MHrs

2 AF 572019-01-5S100

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 20. PREP. : FUEL TANK DRAINED AND VENTED; Skills :

2.00 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [22 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572023-02-3

500 600

Task Title

BOTTOM SKIN AT STGR ATTACHMENTS

Task code

DI

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-832

275

N

AMM 572000-210-832

294

T

60 000 FH

T

20 000 CY

I

13 900 FH

I

3 900 CY

T

110 200 FH

T

31 500 FC

299

I

13 900 FH

366

I

3 900 CY

Skills :

0.00 MHrs

1 AF 572023-02-3S100

500 600

BOTTOM SKIN AT STGR ATTACHMENTS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.

DI

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [23 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572027-01-5

541 641

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. PREP. : FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 FC

I

28 300 FH

I

6 200 CY See note

References

Ctrl

Eff

N

ALI 572027-01-05 AMM 572000-220-855

275

N

ALI 572027-01-05 AMM 572000-220-855

294

Check : NT

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :

541BB 541BZ 541FZ 641AB 641DB 641DZ 0.00 Hrs

541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

Skills :

0.00 MHrs

1 NDT 572027-01-5S100

541 641

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9.

T

127 500 FH

T

36 400 FC

I

28 300 FH

I

6 200 CY

366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [24 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572032-01-4

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

Threshold Interval

References

Ctrl

N

AMM 572000-210-849

Eff 275

T

54 700 FH

T

15 600 CY

294

I

36 000 FH

299

I

10 300 CY See note

366

T

62 900 FH

T

9 600 FC

I

45 500 FH

962

7 000 CY

1019

Skills :

0.80 MHrs

1 AF R

572032-01-9S100

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

I

N

AMM 572000-210-849

943 946

1256 1266

Skills :

0.80 MHrs

1 AF 500 600

572033-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR.

N

ALI 572033-01-04 AMM 572000-210-850

78 500 FH

T

22 400 CY

I

24 400 FH

299

I

6 900 CY

366

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 57 [25 / 72] ATA

: 57

294


R

57

WINGS

Task Number

Zone

572033-01-9S020

500 600

Task code

Task Title

DI


Threshold Interval

References

Ctrl

N

ALI 572033-01-09 AMM 572000-210-850

Eff 943

T

60 000 FH

T

17 000 CY

I

36 800 FH

962

5 600 CY

1019

I

946

1256 1266

Skills :

0.60 MHrs

1 AF 541 641

572046-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. PREP. : FUEL TANK DRAINED AND VENTED;

T

60 000 FH

T

20 000 CY

I

25 000 FH

I

7 100 CY See note

N

AMM 572000-220-849

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 541DB 641DB 641EB 6.00 Hrs

541EB 641FB

541FB

641AB

Skills :

1.60 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [26 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

572046-01-4S100

541 641

Task code

Task Title

DI


Threshold Interval

References

Ctrl

N

AMM 572000-220-849

Eff 294

T

106 200 FH

T

30 300 FC

299

I

25 000 FH

366

I

7 100 CY

T

60 000 FH

T

17 000 CY

I

34 600 FH

962

5 300 CY

1019

Skills :

1.60 MHrs

2 AF R

572046-01-9S020

541 641

DI


I

N

AMM 572000-220-849

943 946

1256 1266

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 541DB 641DB 641EB 6.00 Hrs

541EB 641FB

541FB

641AB

Skills :

1.60 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [27 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572047-01-3

541 641

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING BOLTING AREAS) AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.

Threshold Interval

T

111 700 FH

T

31 900 CY

I

50 000 FH

I

20 000 CY

T

60 000 FH

T

20 000 CY

I

50 000 FH

References

Ctrl

N

ALI 572047-01-3 AMM 572000-220-856

Eff 294 299 366

Access panels :

541AB 641BZ

541BB 641CB

Total access time :

541BZ 641CZ

541CB

541CZ

641AB

641BB

3.00 Hrs

Skills :

0.40 MHrs

1 NDT 572047-01-3S020

541 641

500 600

572049-01-4

Issue No

:

Date

:

10 01/12/2013

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING BOLTING AREAS) AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THRESHOLD IS NEXT 4C CHECK

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

AMM 572000-220-856

275

N

AMM 572000-220-857

275

I


DI

OUTER WING

N

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

16 200 CY See note

Page : ALI - 57 [28 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

572049-01-4S100

500 600

572049-01-9S020

500 600

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.

Threshold Interval

References

Ctrl

N

AMM 572000-220-857

Eff 294

T

103 000 FH

T

29 400 FC

299

I

50 000 FH

366

I

16 200 CY

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

8 100 CY

1019

I

N

ALI 572049-01-09 AMM 572000-220-857

943 946

1256 1266

Skills :

0.40 MHrs

1 NDT 571 573 671 673

572050-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. PREP. : FLAPS EXTENDED

N

AMM 572000-210-859

123 100 FH

T

35 100 FC

299

I

34 700 FH

366

I

9 900 CY

Skills :

0.32 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

T

Page : ALI - 57 [29 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

572050-01-4S020

571 573 671 673

572050-01-8S020

571 573 671 673

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. PREP. : FLAPS EXTENDED NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 FC

I

34 700 FH

I

9 900 CY See note

References

Ctrl

Eff

N

AMM 572000-210-859

275

N

ALI 572050-01-12 AMM 572000-210-859

943

Check : NT

DI

OUTER WING

Threshold Interval

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. PREP. : FLAPS EXTENDED

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

I

17 000 CY

1019

946

1256 1266

Access panels :

573DB

673DB

Total access time :

0.52 Hrs

Skills :

0.32 MHrs

1 AF R

572051-01-10

571 671

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. PREP. : FLAPS EXTENDED;

N

ALI 572051-01-10 AMM 572000-220-858

943

T

60 000 FH

T

17 000 CY

I

29 100 FH

962

I

4 400 CY

1019

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [30 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572051-01-5

571 671

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. PREP. : FLAPS EXTENDED;

Threshold Interval

References

Ctrl

N

AMM 572000-220-858

Eff 275

T

83 400 FH

T

23 800 FC

294

I

18 700 FH

299

I

5 300 CY

366

T

96 500 FH

T

20 900 FC

294

I

34 500 FH

299

I

9 800 CY

366

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

I

8 300 CY

1019

Skills :

0.00 MHrs

1 NDT 541 641

572052-03-1

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE PREP. : SEALANT REMOVAL AS PER NTM;

N

AMM 572000-220-873

275

Skills :

1.40 MHrs

1 NDT R

572052-03-8S020

541 641

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE PREP. : SEALANT REMOVAL AS PER NTM;

N

AMM 572000-220-873

943 946

1256 1266

Access panels :

541BB

541CB

Total access time :

641BB 641CB 2.00 Hrs

Skills :

1.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [31 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

572054-01-1S100

571 671

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. PREP. : FLAPS EXTENDED;

Threshold Interval

References

Ctrl

N

AMM 572000-220-860

Eff 943

T

89 400 FH

T

13 700 FC

I

39 800 FH

962

6 100 CY

1019

I

946

1256 1266

Skills :

0.40 MHrs

1 NDT 571 671

572054-01-5

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT WIRE HARNESS SLOT BETWEEN RIBS 4 & 5. PREP. : FLAPS EXTENDED;

N

AMM 572000-220-860

70 100 FH

T

20 000 FC

294

I

27 900 FH

299

I

7 900 CY

366

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : ALI - 57 [32 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572068-01-4

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. PREP. : FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

20 000 CY See note

T

132 100 FH

T

37 700 FC

I

50 000 FH

I

20 000 CY See note

References

Ctrl

Eff

N

ALI 572068-01-04 AMM 572000-220-848

275

N

ALI 572068-01-04 AMM 572000-220-848

294

Access panels :

541CB 641FZ

541DB

Total access time :

541EZ

541FZ

641CB

641DB

641EZ

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572068-01-4S100

Issue No

:

Date

:

541 641

10 01/12/2013

SDI

OUTER WING DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

Amendment No Date

: 01 : 06/09/2014

299 366

Page : ALI - 57 [33 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

572069-01-10S020

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

Threshold Interval

References

Ctrl

N

ALI 572069-01-12 AMM 572000-210-865

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

14 500 CY

1019

I

946

1256 1266

Access panels :

541DB

541FZ

Total access time :

641DB

641FZ

2.00 Hrs

Skills :

0.00 MHrs

1 AF 541 641

572069-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

50 000 FH

N

ALI 572069-01-04 AMM 572000-210-865

I


Access panels :

541DB

541FZ

Total access time :

641DB 641FZ 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [34 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

572069-01-4S100

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

Threshold Interval

T

95 100 FH

T

27 100 FC

I

50 000 FH

I

20 000 CY

T

117 500 FH

T

18 000 CY

T

12 YE

References

Ctrl

N

ALI 572069-01-04 AMM 572000-210-865

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

572081-01-14

541 641

541 641

572081-01-5

Issue No

:

Date

:

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED;

I

101 300 FH

I

15 500 CY

I

12 YE

DI

T

79 700 FH

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE OR 21300 FC OR 98300 FH"" OR NEXT ""12 YE OR 10300 FC OR 47700 FH"" FROM APPROVE DATE"

T

22 700 FC

OUTER WING

Amendment No Date

: 01 : 06/09/2014

T

12 YE

I

43 000 FH

I

12 300 CY

I

12 YE

N

AMM 572000-210-817

943 946 962 1019 1256 1266

N

AMM 572000-210-817

See note Check : NT

Page : ALI - 57 [35 / 72] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572081-01-5S100

541 641

572082-01-1S020

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

DI

OUTER WING DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-817

541AZ 541FB 641DZ

Total access time :

541BB 541CB 541FZ 641AB 641EB 641EZ 9.72 Hrs

541DB 641AZ 641FB

541DZ 641BB 641FZ

79 700 FH

T

22 700 FC

299

T

24 YE

366

I

43 000 FH

I

12 300 CY

I

12 YE

T

60 000 FH

T

17 000 CY

I

33 500 FH

962

5 100 CY

1019

I

N

AMM 572000-210-870

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

1256 1266

541EB 641CB

2.00 MHrs

: 01 : 06/09/2014

943 946

Skills :

1 AF

294

T

Access panels :

541AB 541EZ 641DB

Eff

Page : ALI - 57 [36 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572084-01-3

541 641

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-220-871

275

N

AMM 572000-220-871

294

T

60 000 FH

T

20 000 CY

I

38 400 FH

I

11 800 CY

T

77 600 FH

T

24 000 FC

299

I

38 400 FH

366

I

11 800 CY

T

60 000 FH

T

17 000 CY

I

59 300 FH

962

9 100 CY

1019

Access panels :

541AB

541AZ

Total access time :

541BZ 641AB 2.72 Hrs

641AZ

641BZ

Skills :

0.00 MHrs

1 NDT 572084-01-3S100

541 641

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH. Skills :

0.00 MHrs

1 NDT R

572084-01-5S020

541 641

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.

I

N

AMM 572000-220-871

943 946

1256 1266

Skills :

0.80 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [37 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572092-01-4

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

T

60 000 FH

T

20 000 CY

I

36 200 FH

I

9 000 CY

T

100 700 FH

T

28 700 FC

I

37 800 FH

I

10 800 CY See note

T

60 000 FH

T

20 000 FC

I

49 000 FH

References

Ctrl

Eff

N

ALI 572092-01-04 AMM 572000-210-872

275

N

ALI 572092-01-04 AMM 572000-210-872

294

Access panels :

541EB

541FB

Total access time :

641EB 641FB 2.00 Hrs

Skills :

0.60 MHrs

2 AF 572092-01-4S100

541 641

500 600

572110-01-4

DI


DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. NOTE: THRESHOLD IS NEXT 4C CHECK

366

N

ALI 572110-01-04 AMM 572100-210-848

I


Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [38 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

572110-01-4S100

500 600

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

Threshold Interval

References

Ctrl

N

ALI 572110-01-04 AMM 572100-210-848

Eff 294

T

100 100 FH

T

28 600 FC

I

49 000 FH

I

14 000 CY

T

69 600 FH

T

19 800 FC

I

39 800 FH

299

I

11 300 CY

366

T

60 000 FH

T

17 000 CY

I

31 800 FH

962

I

4 800 CY

1019

299 366

Skills :

0.80 MHrs

1 AF 532 533 534 632 633 634

572111-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

N

ALI 572111-01-04 AMM 572100-210-849

275 294

Access panels :

532AB 632CB

532CB 633AB

Total access time :

533AB 533CB 633CB 634AB 0.00 Hrs

534AB 634CB

534CB

632AB

Skills :

0.60 MHrs

1 AF R

572111-01-9S020

532 533 534 632 633 634

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

N

ALI 572111-01-09 AMM 572100-210-849

943 946

1256 1266

Skills :

0.60 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [39 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

572116-02-1

500 600

500 600

572119-02-5

572121-01-4S100

541 641

Task Title

Task code

GVI

OUTER WING GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. WING BOTTOM SKIN AT HOLES

DI

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLES AFT OF FRON SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 12 AND 23. TPS : TPS MUST NOT BE APPLIED note:CPCP DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

Threshold Interval

References

Ctrl

N

ALI 572116-02-01 AMM 572100-210-861

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

133 400 FH

T

38 100 FC

I

18 400 FH

299

I

5 200 CY

366

T

60 000 FH

T

17 000 CY

T

6 YE

N

ALI 572119-02-05 AMM 572100-210-822

294

943 946 962 1019

I

48 800 FH

I

7 500 CY

I

6 YE

T

85 200 FH

T

24 300 FC

I

30 700 FH

299

I

8 700 CY

366

1256 1266

N

ALI 572121-01-04 AMM 572100-210-856

0.60 MHrs

: 01 : 06/09/2014

275

T

Skills :

1 AF

Eff

Page : ALI - 57 [40 / 72] ATA

: 57

275 294


57

WINGS

Task Number

Zone

572125-01-6

542 642

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-4 NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS NEXT 12 YE OR 9900 FC OR 45200 FH FROM APPROVE DATE OF AMS A330 I09 A00

Threshold Interval

T

60 000 FH

T

20 000 CY

T

12 YE

I

39 400 FH

I

11 200 CY

I

12 YE

T

95 700 FH

T

27 300 FC

T

24 YE

I

39 400 FH

I

11 200 CY

I

12 YE

References

Ctrl

Eff

N

ALI 572125-01-06 AMM 572100-210-805

275

N

ALI 572125-01-06 AMM 572100-210-805

294

Access panels :

542DB

542EB

Total access time :

642DB 642EB 3.00 Hrs

Skills :

0.00 MHrs

1 AF 572125-01-6S100

542 642

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-4S100

366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [41 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572125-02-4

542 642

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-6 PREP. : SEALANT REMOVAL AS PER NTM NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

39 400 FH

I

11 200 CY See note

References

Ctrl

Eff

N

ALI 572125-02-04 AMM 572100-210-823

275

N

ALI 572125-02-04 AMM 572100-210-823

294

Check : NT

Access panels :

542DB

542EB

Total access time :

642DB 642EB 3.00 Hrs

Skills :

0.80 MHrs

1 NDT 572125-02-4S100

542 642

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-6S100 PREP. : SEALANT REMOVAL AS PER NTM

T

95 700 FH

T

27 300 FC

I

39 400 FH

I

11 200 CY

366

Skills :

0.80 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [42 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572133-01-4

500 600

Task Title

Task code

DI


Threshold Interval

T

60 000 FH

T

20 000 CY

I

23 300 FH

I

6 600 CY

T

125 600 FH

T

35 900 FC

I

23 300 FH

I

6 600 CY

T

60 000 FH

T

20 000 CY

T

12 YE

I

40 600 FH

I

11 600 CY

I

12 YE

References

Ctrl

Eff

N

ALI 572133-01-04 AMM 572100-210-835

275

N

ALI 572133-01-04 AMM 572100-210-835

294

Skills :

2.00 MHrs

1 AF 572133-01-4S100

500 600

DI


299 366

Skills :

2.00 MHrs

1 AF 574 575 674 675

572153-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE JOINT PLATE AT RIB 27. NOTE: CPCP

N

ALI 572153-01-04 AMM 572100-210-810

Access panels :

574AT

674AT

Total access time :

0.84 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [43 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

572153-01-4S100

574 575 674 675

Task Title

Task code

DI


Threshold Interval

T

134 900 FH

T

38 500 CY

T

24 YE

I

40 600 FH

I

11 600 CY

I

12 YE

References

Ctrl

N

ALI 572153-01-04 AMM 572100-210-810

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

0.40 MHrs

: 01 : 06/09/2014

294 299 366

Skills :

1 AF

Eff

Page : ALI - 57 [44 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572154-01-4

541 542 641 642

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

65 200 FH

T

18 600 CY

T

12 YE

I

43 100 FH

I

12 300 CY

I

References

Ctrl

N

ALI 572154-01-04 AMM 572100-210-811

12 YE See note


541FB 541NB 542CB 641JB 641RB 642GB

541GB 541PB 542DB 641KB 641SB

Total access time :

541HB 541QB 542EB 641LB 642AB

541JB 541RB 542GB 641MB 642BB

541KB 541SB 641FB 641NB 642CB

541LB 542AB 641GB 641PB 642DB

541MB 542BB 641HB 641QB 642EB

20.00 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [45 / 72] ATA

: 57

Eff 275


57

WINGS

Task Number

Zone

572154-01-4S100

541 542 641 642

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

Threshold Interval

T

65 200 FH

T

18 600 FC

T

24 YE

I

43 100 FH

I

12 300 CY

I

12 YE

T

79 900 FH

T

12 200 CY

T

12 YE

References

Ctrl

N

ALI 572154-01-04 AMM 572100-210-811

Eff 294 299 366

Skills :

3.00 MHrs

1 AF R

541 542 641 642

572154-01-9

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. TPS : TPS MUST NOT BE APPLIED PREP. : FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED;

Amendment No Date

: 01 : 06/09/2014

DI

I

37 100 FH

I

5 700 CY

I

12 YE

N

AMM 572100-210-811

943 946 962 1019 1256 1266

Page : ALI - 57 [46 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572158-01-5

541 641

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23.

Threshold Interval

T

60 000 FH

T

20 000 CY

I

25 200 FH

I

7 200 CY See note

References

Ctrl

Eff

N

ALI 572158-01-05 AMM 572100-210-826

275

N

ALI 572158-01-05 AMM 572100-210-826

294


541GB 541PB 641KB 641SB

541HB 541QB 641LB

Total access time :

541JB 541RB 641MB

541KB 541SB 641NB

541LB 641GB 641PB

541MB 641HB 641QB

541NB 641JB 641RB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572158-01-5S100

541 641

DI


T

101 600 FH

T

29 000 FC

I

25 200 FH

I

7 200 CY

366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [47 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572164-01-5

541 542 641 642

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. TPS : TPS MUST NOT BE APPLIED note:CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

T

12 YE

I

22 900 FH

I

6 500 CY

I

References

Ctrl

Eff

N

ALI 572164-01-05 AMM 572100-210-816

275

N

ALI 572164-01-05 AMM 572100-210-816

294

12 YE See note


541GB 541PB 542DB 641NB 642CB

541HB 541QB 641GB 641PB 642DB

Total access time :

541JB 541RB 641HB 641QB

541KB 541SB 641JB 641RB

541LB 542AB 641KB 641SB

541MB 542BB 641LB 642AB

541NB 542CB 641MB 642BB

15.00 Hrs

Skills :

2.00 MHrs

1 AF 572164-01-5S100

541 542 641 642

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. TPS : TPS MUST NOT BE APPLIED note:CPCP

T

131 000 FH

T

37 400 CY

T

24 YE

I

22 900 FH

I

6 500 CY

I

12 YE

366

Skills :

2.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [48 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572180-01-4S100

541 641

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

Threshold Interval

References

Ctrl

N

ALI 572180-01-04 AMM 572100-210-840

Eff 275

T

71 300 FH

T

20 300 FC

I

55 800 FH

299

I

15 900 CY

366

T

60 000 FH

T

17 000 CY

I

29 700 FH

962

4 500 CY

1019

294

Skills :

0.80 MHrs

1 AF R

572180-01-9S020

541 641

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. PREP. : FUEL TANK DRAINED AND VENTED;

I

N

AMM 572100-210-840

943 946

1256 1266

Access panels :

541GB 541PB 641KB 641SB

541HB 541QB 641LB

Total access time :

541JB 541RB 641MB

541KB 541SB 641NB

541LB 641GB 641PB

541MB 641HB 641QB

541NB 641JB 641RB

11.00 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [49 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572183-01-4

542 642

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-4

Threshold Interval

References

Ctrl

N

ALI 572183-01-04 AMM 572100-210-865

Eff 275

T

78 000 FH

T

22 300 CY

I

28 000 FH

299

I

8 000 CY See note

366

T

60 000 FH

T

17 000 CY

I

32 300 FH

962

4 900 CY

1019

294

Access panels :

542DB

542EB

Total access time :

642DB 642EB 0.00 Hrs

Skills :

0.60 MHrs

1 AF R

572183-01-8S020

542 642

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-8S020

I

N

ALI 572183-01-08 AMM 572100-210-865

542EB

Total access time :

642DB

1266

642EB

3.00 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

946

1256

Access panels :

542DB

943

Page : ALI - 57 [50 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572183-02-4

542 642

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-4

Threshold Interval

References

Ctrl

N

ALI 572183-02-04 AMM 572100-220-805

Eff 275

T

78 000 FH

T

22 300 CY

I

28 000 FH

299

I

8 000 CY See note

366

T

60 000 FH

T

17 000 CY

I

32 300 FH

962

4 900 CY

1019

294

Access panels :

542DB

542EB

Total access time :

642DB 642EB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

572183-02-8S020

542 642

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-8S020 PREP. : SEALANT REMOVAL AS PER NTM

I

N

ALI 572183-02-08 AMM 572100-220-805

542EB

Total access time :

1266

642DB 642EB 3.00 Hrs

Skills :

0.60 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

946

1256

Access panels :

542DB

943

Page : ALI - 57 [51 / 72] ATA

: 57


57

WINGS

Task Number

Zone

572606-01-3

532 533 534 632 633 634

FITTINGS

532 533 534 632 633 634

FITTINGS

572606-01-3S020

Issue No

:

Date

:

10 01/12/2013

Task Title

Task code

DI

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. PREP. : MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634; DI

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. PREP. : MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634; NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

Threshold Interval

References

Ctrl

N

AMM 572600-210-815

Eff 294

T

101 300 FH

T

28 900 FC

299

I

50 000 FH

366

I

17 600 CY

T

60 000 FH

T

20 000 CY

I

50 000 FH

N

AMM 572600-210-815

I


Page : ALI - 57 [52 / 72] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572606-01-8

532 533 534 632 633 634

572607-01-7

572607-01-7S020

Issue No

:

Date

:

Task Title

DI

FITTINGS DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. PREP. : MOVABLE FLAP TRACK FAIRING Z532; MOVABLE FLAP TRACK FAIRING Z533; MOVABLE FLAP TRACK FAIRING Z534; MOVABLE FLAP TRACK FAIRING Z632; MOVABLE FLAP TRACK FAIRING Z633; MOVABLE FLAP TRACK FAIRING Z634;

531 532 533 534 631 632 633 634

FITTINGS

531 532 533 534 631 632 633 634

FITTINGS

10 01/12/2013

Task code

Threshold Interval

References

Ctrl

N

AMM 572600-210-815

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

12 500 CY

1019

I

946

1256 1266

DI

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. note:CPCP

T

115 500 FH

T

33 000 CY

T

24 YE

I

50 000 FH

I

20 000 CY

I

N

ALI 572607-01-07 AMM 572600-210-802

294 299 366

12 YE See note

DI

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. note:CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

T

12 YE

I

50 000 FH

I

20 000 CY

I

12 YE

N

AMM 572600-210-802

See note Check : NT

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [53 / 72] ATA

: 57

275


57

WINGS

Task Number

Zone

573001-01-5

550 650

Task Title

Task code

DI

WING TIP SPECIAL DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTO SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AN BUTTSTRAPS. PREP. : WINGTIP LEADING EDGE ASSY; WINGTIP NAVIGATION LIGHT; WINGTIP STROBE LIGHT;

Threshold Interval

T

84 600 FH

T

24 100 CY

T

12 YE

I

20 700 FH

I

5 900 CY

I

12 YE

T

84 600 FH

T

24 100 CY

T

24 YE

I

20 700 FH

I

5 900 CY

I

12 YE

References

Ctrl

Eff

N

ALI 573001-01-05 AMM 573000-210-801

275

N

ALI 573001-01-05 AMM 573000-210-801

294

Skills :

1.20 MHrs

1 AF 573001-01-5S100

550 650

DI

WING TIP SPECIAL DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. PREP. : WINGTIP LEADING EDGE ASSY; WINGTIP NAVIGATION LIGHT; WINGTIP STROBE LIGHT; NOTE: CPCP

366

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [54 / 72] ATA

: 57


57

WINGS

Task Number

Zone

573002-01-5

500 600

Task Title

Task code

DI

WING TIP DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE.

Threshold Interval

References

Ctrl

N

ALI 573002-01-05 AMM 573000-210-806

Eff 275

T

84 600 FH

T

24 100 CY

I

20 700 FH

299

I

5 900 CY See note

366

T

60 000 FH

T

20 000 CY

I

21 100 FH

I

6 000 CY

T

102 900 FH

T

29 400 FC

I

21 100 FH

I

6 000 CY

294

Skills :

0.30 MHrs

1 AF 535 635

573003-02-4

SDI

WING TIP SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). PREP. : WINGLET

N

ALI 573003-02-04 AMM 573000-220-806

275

N

ALI 573003-02-04 AMM 573000-220-806

294

Skills :

0.80 MHrs

1 NDT 573003-02-4S100

535 635

SDI


366

Skills :

0.80 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [55 / 72] ATA

: 57


57

WINGS

Task Number

Zone

574106-01-4

521 522 523 621 622 623

Task code

Task Title

DI

INBOARD LEADING EDGE

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: MSN 255-SAMPLE A/C FOUND CORROSION, 100% THRESHOLD CHANGE TO SAMPLE THRESHOLD; NEXT DUE IS NEXT STRUCTURE CHECK 4C (6 YEAR) FROM APPROVED DATE OF AMS A330 I09 A00

Threshold Interval

T

84 300 FH

T

24 000 CY

T

12 YE

I

84 300 FH

I

24 000 CY

I

12 YE

References

Ctrl

N

ALI 574106-01-04 AMM 574100-210-806

Access panels :

521BB 521JB 522GB 522PB 523GB 523PB 621HB 622FB 622NB 623FB 623NB

521CB 522AB 522HB 522RB 523HB 621BB 621JB 622GB 622PB 623GB 623PB

Total access time :

521DB 522BB 522JB 522SB 523JB 621CB 622AB 622HB 622RB 623HB

521EB 522CB 522KB 523CB 523KB 621DB 622BB 622JB 622SB 623JB

521FB 522DB 522LB 523DB 523LB 621EB 622CB 622KB 623CB 623KB

521GB 522EB 522MB 523EB 523MB 621FB 622DB 622LB 623DB 623LB

521HB 522FB 522NB 523FB 523NB 621GB 622EB 622MB 623EB 623MB

1.88 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [56 / 72] ATA

: 57

Eff 275


57

WINGS

Task Number

Zone

574106-01-4S100

521 522 523 621 622 623

Task Title

Task code

DI


DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: MSN 255-SAMPLE A/C FOUND CORROSION, 100% THRESHOLD CHANGE TO SAMPLE THRESHOLD; NEXT DUE IS NEXT STRUCTURE CHECK 4C (6 YEAR) FROM APPROVED DATE OF AMS A330 I09 A00

Threshold Interval

T

84 300 FH

T

24 000 CY

T

24 YE

I

84 300 FH

I

24 000 CY

I

References

Ctrl

N

ALI 574106-01-04 AMM 574100-210-806

Eff 294 299 366

12 YE See note

Skills :

3.00 MHrs

1 AF R

574106-01-7S020

521 522 523 621 622 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. . . . note:CPCP .

T

60 000 FH

T

17 000 CY

T

12 YE

I

50 000 FH

I

17 000 CY

I

12 YE

N

ALI 574106-01-07 AMM 574100-210-806

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

962 1256 1266

3.00 MHrs

: 01 : 06/09/2014

946 1019

Skills :

1 AF

943

Page : ALI - 57 [57 / 72] ATA

: 57


57

WINGS

Task Number

Zone

574107-02-4

521 522 523 621 622 623

Task code

Task Title

SDI

INBOARD LEADING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

15 500 CY See note

References

Ctrl

Eff

N

ALI 574107-02-04 AMM 574100-210-812

275

N

ALI 574107-02-04 AMM 574100-210-812

294


521FB 522DB 522LB 523CB 622AB 622HB 622QB

521GB 522EB 522MB 523DB 622BB 622JB 622RB

Total access time :

521HB 522FB 522NB 523EB 622CB 622KB 622SB

521JB 522GB 522PB 621FB 622DB 622LB 623CB

522AB 522HB 522QB 621GB 622EB 622MB 623DB

522BB 522JB 522RB 621HB 622FB 622NB 623EB

522CB 522KB 522SB 621JB 622GB 622PB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 574107-02-4S100

521 522 523 621 622 623

SDI

INBOARD LEADING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

T

119 300 FH

T

34 100 FC

I

50 000 FH

I

15 500 CY

366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [58 / 72] ATA

: 57


57

WINGS

Task Number

Zone

574109-02-1S100

521 522 523 621 622 623

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. . . note:CPCP

Threshold Interval

T

47 500 FH

T

13 500 CY

T

12 YE

I

22 700 FH

I

6 500 CY

I

12 YE

T

80 900 FH

T

12 400 CY

T

12 YE

References

Ctrl

N

ALI 574109-02-01 AMM 574100-210-814

Eff 275 294 299 366

Skills :

0.60 MHrs

1 AF R

574109-02-5S020

521 522 523 621 622 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. . . note:CPCP .

I

38 700 FH

I

5 900 CY

I

12 YE

N

AMM 574100-210-814

946 962 1019 1256 1266

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : ALI - 57 [59 / 72] ATA

: 57


57

WINGS

Task Number

Zone

574110-02-1

500 600

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

Threshold Interval

T

60 000 FH

T

20 000 CY

T

6 YE

I

50 000 FH

I

18 900 CY

I

6 YE

T

60 000 FH

T

20 000 CY

I

50 000 FH

References

Ctrl

N

ALI 574110-02-01 AMM 574100-210-813

Eff 275 294 299 366

Skills :

0.00 MHrs

1 AF 500 600

574114-03-1

574114-03-1S100

Issue No

:

Date

:

500 600

10 01/12/2013


DI

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26 TO RIB 39. NOTE: THRESHOLD IS NEXT 4C CHECK

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26 TO RIB 39.

Amendment No Date

: 01 : 06/09/2014

N

ALI 574114-03-01 AMM 574100-210-830

275

N

ALI 574114-03-01 AMM 574100-210-830

294

I


DI

T

106 900 FH

T

30 500 CY

I

50 000 FH

I

14 600 CY

299 366

Page : ALI - 57 [60 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

574115-02-1S100

522 622

515 615

574704-02-3

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11 AND RIB 24 TO RIB 26. note:CPCP

DI

SLAT 5 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT ""6600 FC OR 23300 FH "" FROM APPROVE DATE"

Threshold Interval

T

58 000 FH

T

16 500 CY

T

12 YE

I

25 300 FH

I

7 200 CY

I

12 YE

T

60 000 FH

T

17 000 FC

T

12 YE

I

23 300 FH

I

6 600 CY

I

12 YE

References

Ctrl

N

ALI 574115-02-01 AMM 574100-210-844

Eff 275 294 299 366

N

ALI 574704-02-03 AMM 574700-210-804

275 943 946 962 1019 1256 1266

See note Check : NT Skills :

0.00 MHrs

1 AF 574704-02-3S100

515 615

DI

SLAT 5 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED;

T

109 000 FH

T

31 100 CY

T

24 YE

I

23 300 FH

I

6 600 CY

I

N

ALI 574704-02-03 AMM 574700-210-804

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299 366

12 YE See note

Issue No

294

Page : ALI - 57 [61 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

574704-03-1

515 615

Task Title

Task code

DI

SLAT 5

SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

References

Ctrl

N

AMM 574700-250-802

Eff 275

T

60 000 FH

T

17 000 CY

943

I

23 300 FH

946

I

6 600 CY See note

1019

962 1256

Check : NT

1266

Skills :

0.00 MHrs

1 NDT 574704-03-1S100

515 615

DI

SLAT 5 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

N

AMM 574700-250-802

294

T

109 000 FH

T

31 100 CY

299

I

23 300 FH

366

I

6 600 CY

T

22 500 FH

Skills :

0.00 MHrs

1 NDT 516 616

574804-01-2

Issue No

:

Date

:

10 01/12/2013

SDI

SLAT 6 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH.

Amendment No Date

: 01 : 06/09/2014

T

6 100 CY

I

15 400 FH

I

4 400 CY

N

AMM 574800-250-804

Page : ALI - 57 [62 / 72] ATA

: 57

ALL


57

WINGS

Task Number

Zone

574804-02-5S020

516 616

500 600

575011-01-4

Task Title

Task code

DI


TRAILING EDGE AND TRAILING EDGE DEVICE

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

21 500 FH

T

6 100 CY

T

12 YE

I

15 400 FH

I

4 400 CY

I

12 YE

T

60 000 FH

T

20 000 FC

I

60 000 FH

I

20 000 CY

T

133 000 FH

T

38 000 FC

I

50 000 FH

I

20 000 CY

References

Ctrl

Eff

N

ALI 574804-02-05 AMM 574800-210-804

ALL

N

ALI 575011-01-04 AMM 575000-210-828

275

N

ALI 575011-01-04 AMM 575000-210-828

294

Skills :

0.00 MHrs

1 AF 575011-01-4S100

500 600

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

DI

366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

299

Page : ALI - 57 [63 / 72] ATA

: 57


57

WINGS

Task Number

Zone

575012-01-2

500 600

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

Threshold Interval

References

Ctrl

N

ALI 575012-01-02 AMM 575000-210-809

Eff 275

T

76 700 FH

T

21 900 CY

I

19 700 FH

299

I

5 600 CY See note

366

T

81 900 FH

T

23 400 CY

I

81 900 FH

299

I

23 400 CY See note

366

294

Skills :

0.00 MHrs

1 AF 572 672

575018-01-3

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. PREP. : FLAPS EXTENDED

DI

N

ALI 575018-01-03 AMM 575000-210-832

Access panels :

147AT

148AT

Total access time :

191CT

192CT

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [64 / 72] ATA

: 57

275 294


R

57

WINGS

Task Number

Zone

575018-01-8S020

572 672

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. PREP. : FLAPS EXTENDED

Threshold Interval

References

Ctrl

N

AMM 575000-210-832

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

17 000 CY

1019

I

946

1256 1266

Access panels :

147AT

148AT

Total access time :

191CT

192CT

5.12 Hrs

Skills :

0.40 MHrs

1 AF 575022-01-1S100

575 675

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL. NOTE: CPCP

DI

T

50 400 FH

T

14 400 CY

T

12 YE

I

37 200 FH

I

10 600 CY

I

12 YE

N

ALI 575022-01-01 AMM 575000-210-814

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

366

1.00 MHrs

: 01 : 06/09/2014

294 299

Skills :

1 AF

275

Page : ALI - 57 [65 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

575022-01-4

575 675

500 600

575025-01-4

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL. TRAILING EDGE AND TRAILING EDGE DEVICE

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

Threshold Interval

T

57 500 FH

T

8 800 CY

T

12 YE

References

Ctrl

N

AMM 575000-210-814

Eff 943 946 962 1019

I

57 500 FH

I

8 800 CY

I

12 YE

T

69 000 FH

T

19 700 CY

I

31 000 FH

I

8 800 CY See note

T

50 000 FH

T

14 300 FC

I

30 300 FH

962

I

4 600 CY

1019

1256 1266

N

ALI 575025-01-04 AMM 575000-210-835 MRB 575025-01-4

275 294 299 366

Access panels :

531AB

631AB

Total access time :

6.12 Hrs

Skills :

0.00 MHrs

1 AF R

575025-01-8S100

500 600

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

DI

N

AMM 575000-210-835

943 946

1256 1266

Skills :

0.20 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [66 / 72] ATA

: 57


57

WINGS

Task Number

Zone

575051-01-1

147 148

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS. PREP. : FLAPS EXTENDED;

Threshold Interval

T

35 600 CY

I

8 000 CY

References

Ctrl

N

ALI 575051-01-01 AMM 575000-210-836

Eff 294 299 366

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 575051-01-1S020

Issue No

:

Date

:

147 148

10 01/12/2013

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS. PREP. : FLAPS EXTENDED;

Amendment No Date

: 01 : 06/09/2014

DI

T

17 000 CY

I

8 000 CY

N

AMM 575000-210-836

Page : ALI - 57 [67 / 72] ATA

: 57

275


R

57

WINGS

Task Number

Zone

575067-01-2

531 532 533 534 631 632 633 634

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, EXTERNAL STRUCTURE. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-02-2 PREP. : FIXED FLAP TRACK FAIRING Z531; FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z631; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634;

Threshold Interval

T

60 000 FH

T

17 000 CY

T

12 YE

I

25 500 FH

References

Ctrl

N

ALI 575067-01-02 AMM 575000-210-821

Eff 275 943 946 962 1019

I

8 500 CY

I

12 YE

T

109 200 FH

T

18 200 CY

299

T

24 YE

366

I

38 400 FH

I

6 400 CY

I

12 YE

1256 1266

Skills :

0.00 MHrs

1 AF R

575067-01-2S100

Issue No

:

Date

:

531 532 533 534 631 632 633 634

10 01/12/2013

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, EXTERNAL STRUCTURE. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-02-2 PREP. : FIXED FLAP TRACK FAIRING Z531; FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z631; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634;

Amendment No Date

: 01 : 06/09/2014

DI

N

AMM 575000-210-821

Page : ALI - 57 [68 / 72] ATA

: 57

294


R

57

WINGS

Task Number

Zone

575067-02-2

531 532 533 534 631 632 633 634

Task Title


Task code

SDI

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, INTERNAL STRUCTURE. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-01-2 TPS : TPS MUST NOT BE APPLIED PREP. : FS BOLT; FWD FLAP TRACK FAIRINGS;

Threshold Interval

T

60 000 FH

T

17 000 CY

T

12 YE

I

25 500 FH

References

Ctrl

N

ALI 575067-02-02 AMM 575000-210-822

Eff 275 943 946 962 1019

I

8 500 CY

I

12 YE

T

109 200 FH

T

18 200 CY

299

T

24 YE

366

I

38 400 FH

I

6 400 CY

I

12 YE

T

9 000 FH

T

3 000 CY

I

9 000 FH

I

3 000 CY

1256 1266

Skills :

0.00 MHrs

1 NDT R

575067-02-2S100

575401-01-2

Issue No

:

Date

:

531 532 533 534 631 632 633 634


500 600

INBOARD FLAP

10 01/12/2013

SDI

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, INTERNAL STRUCTURE. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-01-2S100 TPS : TPS MUST NOT BE APPLIED PREP. : FS BOLT; FWD FLAP TRACK FAIRINGS;

GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL SURFACE OF UPPER AND LOWER SKIN NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575401-02-1 PREP. : FLAPS EXTENDED

Amendment No Date

: 01 : 06/09/2014

GVI

N

N

AMM 575000-210-822

ALI 575401-01-02 AMM 575400-210-801

Page : ALI - 57 [69 / 72] ATA

: 57

294

ALL


D

57

WINGS

Task Number

Zone

575401-02-1

500 600

Task Title

Task code

DI

INBOARD FLAP GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL SURFACE OF UPPER AND LOWER SKIN NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 575401-01-2 PREP. : FLAPS EXTENDED

Threshold Interval

References

Ctrl

N

ALI 575401-02-01 AMM 575400-210-802

Eff 275

T

17 700 FH

T

5 900 FC

I

17 700 FH

299

I

5 900 CY

366

T

70 400 FH

T

10 700 FC

I

70 400 FH

962

10 700 CY

1019

294

Skills :

0.40 MHrs

1 AF R

592 692

576105-01-1

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1. PREP. : FAIRING PANELS Z592; FAIRING PANELS Z692;

I

N

ALI 576105-01-01 AMM 576100-250-801

943 946

1256 1266

Skills :

0.00 MHrs

1 NDT R

592 692

576108-01-1

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. PREP. : FAIRING PANELS Z592; FAIRING PANELS Z692;

SDI

N

ALI 576108-01-01 AMM 576100-250-802

943

T

137 900 FH

T

21 000 CY

I

137 900 FH

962

I

21 000 CY

1019

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [70 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

576114-02-1

591 691

Task Title

Task code

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE OF OUTER JACK FITTING. PREP. : JACK FITTING FAIRING; NOTE: MSN 275 THRESHOLD IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

N

ALI 576114-02-01 AMM 576100-200-811

Eff 275

T

60 000 FH

T

17 000 CY

I

56 200 FH

946

I

6 400 CY See note

1019

943 962 1256

Check : NT

1266

Skills :

0.00 MHrs

1 NDT 576114-02-1S100

R

591 691

591 691

576115-01-1

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE OF OUTER JACK FITTING. PREP. : JACK FITTING FAIRING;

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1. PREP. : FAIRING PANELS Z591; FAIRING PANELS Z691;

N

AMM 576100-200-811

275

T

195 500 FH

T

30 000 CY

I

56 200 FH

I

6 400 CY

T

143 000 FH

T

21 900 FC

I

143 000 FH

962

I

21 900 CY

1019

943

N

ALI 576115-01-01 AMM 576100-250-803

943 946

1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [71 / 72] ATA

: 57


R

57

WINGS

Task Number

Zone

576117-01-1

591 691

Task Title

Task code

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACK FITTING. PREP. : FAIRING PANELS Z591; FAIRING PANELS Z691;

Threshold Interval

References

Ctrl

N

ALI 576117-01-01 AMM 576100-250-804

Eff 943

T

78 000 FH

T

11 900 FC

I

89 300 FH

962

9 400 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT R

591 691

576118-01-1

SDI

AILERON MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. PREP. : FAIRING PANELS Z591; FAIRING PANELS Z691;

N

ALI 576118-01-01 AMM 576100-250-805

943

T

94 500 FH

T

13 900 FC

I

94 500 FH

962

13 900 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ALI - 57 [72 / 72] ATA

: 57


71


Task Number

Zone

711301-02-2

415 416 425 426

Task code

Task Title

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

Threshold Interval

T

8 000 FC

T

3 YE

I

8 000 CY

I

3 YE

T

8 000 FC

T

3 YE

I

8 000 CY

I

3 YE

References

Ctrl

Eff

N

ALI 711301-02-02 AMM 711300-210-804

ALL

N

AMM 711300-210-805

ALL

Access panels :

415AL 426BR

415BL

Total access time :

415 416 425 426

711302-02-2

Issue No

:

Date

:

10 01/12/2013

416AR

416BR

425AL

425BL

426AR

0.16 Hrs

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCHES FITTINGS).

Amendment No Date

: 01 : 06/09/2014

GVI

Page : ALI - 71 [1 / 1] ATA

: 71


R

78

ENGINE EXHAUST

Task Number

Zone

783201-04-1

417 418 427 428

MAIN STRUCTURE

417 418 427 428

MAIN STRUCTURE

783202-02-2

Task code

Task Title

GVI

GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND GVI

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS). PREP. : LATCH ACCESS DOOR;

Threshold Interval

T

8 000 FC

I

8 000 CY

T

8 000 FC

I

8 000 CY

References

Ctrl

N

AMM 783200-210-807

ALL

N

AMM 783000-210-805

ALL

Access panels :

415AL 428AR

416AR

Total access time :

417AL

418AR

425AL

426AR

427AL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff

Page : ALI - 78 [1 / 1] ATA

: 78


PAGE

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Page: 5


32

LANDING GEAR

Task Number

Zone

321101-01-1

731 741

Task Title

Task code

DI

MAIN GEAR DETAILED INSPECTION OF MLG MAIN FITTING EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 321100-210-805

ALL

N

AMM 321100-210-806

ALL

N

AMM 321100-220-821

ALL

Skills :

0.40 MHrs

1 AF 731 741

321102-01-1

DI

MAIN GEAR DETAILED INSPECTION OF MLG SLIDING PISTON EXTERNAL SURFACES, EXCEPT WHERE COVERED BY MAIN FITTING AND BUSH FLANGES. PREP. : AIRCRAFT JACKING; note:CPCP Skills :

1.00 MHrs

1 AF 731 741

321104-02-1

Issue No

:

Date

:

10 01/12/2013

DI

MAIN GEAR DETAILED INSPECTION OF MLG BOGIE BEAM, BOGIE BEAM PIVOT PIN, BRAKE RODS AND BRAKE ROD PINS EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, BUSH FLANGES AND STONE CHIP PROTECTIVE SEALANT. note: CPCP

Amendment No Date

: 01 : 06/09/2014

Page : STR - 32 [1 / 7] ATA

: 32


32

LANDING GEAR

Task Number

Zone

321105-01-1

731 741

Task Title

Task code

DI

MAIN GEAR DETAILED INSPECTION OF MLG PITCH TRIMMER EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. PREP. : MLG PITCH TRIMMER EXTENDED; note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 321100-210-808

ALL

N

AMM 321100-220-822

ALL

N

AMM 321100-220-823

275

Skills :

0.40 MHrs

1 AF 321106-02-1

321107-02-1

Issue No

:

Date

:

731 741

MAIN GEAR

731 741

MAIN GEAR

10 01/12/2013

DI

DETAILED INSPECTION OF MLG UPPER & LOWER SIDE STAY, UPPER PIN, LOWER PIN, CENTER PIN, UPPER CARDAN PIN & NUT, LOWER CARDAN PIN & NUT, UPPER & LOWER SIDE STAY SPRING BRACKETS, PIVOT LINK BRACKET, PIVOT LINK, CONNECTING LINK, UPPER & LOWER SPRING BRACKET BOLTS, PIVOT LINK BRACKET BOLTS, PIVOT LINK CENTER PIN, LOCK LINK/SIDE STAY PIN, CONNECTING LINK/LOCK LINK/UPPER SPRING PIN, CONNECTING LINK/PIVOT LINK PIN, LOWER SPRING/PIVOT LINK PIN, CARDAN LINK, CARDAN LINK PIN, LOCK LINK CENTER PIN & LOCK LINK UPPER PIN EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, BUSH FLANGES AND FITTINGS. note:CPCP DI

DETAILED INSPECTION OF MLG UPPER & LOWER LOCK LINKS EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. note:CPCP Amendment No Date

: 01 : 06/09/2014

294 299 366

Page : STR - 32 [2 / 7] ATA

: 32


LANDING GEAR

Task Number

Zone

321109-02-1

731 741

MAIN GEAR

731 741

MAIN GEAR

321110-02-1

R

32

731 741

321112-01-1

Task Title

Task code

DI

DETAILED INSPECTION OF MLG UPPER & LOWER TORQUE LINKS, UPPER PIN, LOWER PIN, APEX PIN & APEX PIN NUT EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. note:CPCP DI

DETAILED INSPECTION OF MLG UPPER ARTICULATION LINK EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. note:CPCP

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 321100-220-824

ALL

N

AMM 321100-220-825

275 294 299 366

DI

MAIN GEAR

Threshold Interval

DETAILED INSPECTION OF MLG AXLES EXTERNAL SURFACES, EXCEPT WHERE COVERED BY BOGIE BEAM.

T

6 YE

I

6 YE

N

AMM 321100-220-826

943 946 962 1019 1256 1266

731 741

321124-02-1

Issue No

:

Date

:

10 01/12/2013

DI

MAIN GEAR DETAILED INSPECTION OF MLG LOCK STAY/UNLOCK ACTUATOR & ATTACHMENT PINS EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. note:CPCP

Amendment No Date

: 01 : 06/09/2014

T

6 YE

I

6 YE

N

AMM 321100-220-827

Page : STR - 32 [3 / 7] ATA

: 32

ALL


32

LANDING GEAR

Task Number

Zone

321128-01-1

731 741

731 741

321129-01-1

731 741

321129-02-1

731 741

321136-01-1

Issue No

:

Date

:

10 01/12/2013

Task Title

Task code

DI

MAIN GEAR DETAILED INSPECTION OF MLG BOGIE BEAM UNDER BOGIE STOP PAD.

24 MO

I

2 500 CY

I

24 MO

: 01 : 06/09/2014

EAD 2011-0211 SIL 32-3248

ALL

N

EAD 2012-0015 ISB 32-3225

275 294

I

26 MO

N

EAD 2012-0053 ISB 32-3240

ALL

N

AMM 321100-220-828

ALL

Check : NT

DI

DETAILED INSPECTION OF MLG RETRACTION LINK, TURNBUCKLE LINK, BELLCRACNK LINK, FORWARD PINTLE PIN, FORWARD PINTLE PIN LOCK BOLT & PINS SM2, SM7, W, W1, W2 & P EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES.

N

See note

DETAILED INSPECTION OF MLG BOGIE PIVOT PIN. NOTE: - REFER TO EASA AD 2012-0053 FOR 100% THRESHOLD. MAIN GEAR

See note

Eff

299

DI

MAIN GEAR

2 500 FC

T

References

Ctrl

Check : NT

DETAILED INSPECTION OF BOGIE BEAM INTERNAL DIAMETER FOR CORROSION OR PAINT DAMAGE. NOTE: - REFER TO EASA AD 2012-0015 FOR 100% THRESHOLD AND 100% INTERVAL.

Date

T

DI

MAIN GEAR

Amendment No

Threshold Interval

T

6 YE

I

6 YE

Page : STR - 32 [4 / 7] ATA

: 32


R

32

LANDING GEAR

Task Number

Zone

321142-01-1

731 741

MAIN GEAR

570 670

MAIN GEAR

731 741

MAIN GEAR

711

NOSE GEAR

321146-01-1

321148-01-1

322101-02-1

Task Title

DI

DETAILED INSPECTION OF MLG RETRACTION ACTUATOR EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. DI

DETAILED INSPECTION OF MLG AFT PINTLE PIN, AFT PINTLE NUT, SHORTENING MECHANISM ECCENTRIC EARTHING PIN & SHORTENING MECHANISM EARTHING PIN EXTERNAL SURFACES, EXCEPT WHERE COVERED BY MAIN FITTING AND PINTLE BEARING. DI

DETAILED INSPECTION OF MLG LOWER ARTICULATING LINK & PINS SL1, SL2, SL3, SL4 & SL5 EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. DI

DETAILED INSPECTION OF NLG MAIN FITTING, TURNING SLEEVE, UPPER FLANGE, LOWER FLANGE, LEVER, MAIN FITTING HINGE PINS, UPPER & LOWER FLANGE ATTACHMENT PINS AND STEERING ACTUATOR PISTON ROD ATTACHMENT PINS EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP

Issue No

:

Date

:

10 01/12/2013

Task code

Amendment No Date

: 01 : 06/09/2014

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 321100-220-829

ALL

N

AMM 321100-220-830

ALL

N

AMM 321100-220-831

ALL

N

AMM 322100-220-813

ALL

Page : STR - 32 [5 / 7] ATA

: 32


32

LANDING GEAR

Task Number

Zone

322102-02-1

711

Task Title

Task code

DI

NOSE GEAR DETAILED INSPECTION OF NLG SLIDING TUBE INCLUDING AXLE, EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP

711

322103-02-1

DI

NOSE GEAR DETAILED INSPECTION OF NLG UPPER & LOWER TORQUE LINKS AND TORQUE LINK UPPER, LOWER & APEX PINS, EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP

322104-02-1

322105-02-1

123 711

NOSE GEAR

711

NOSE GEAR

DI

DETAILED INSPECTION OF NLG DRAG STAY UPPER ARM, DRAG STAY UPPER PIN, CENTER PINS & PINTLE PIN EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP DI

DETAILED INSPECTION OF NLG DRAG STAY LOWER ARM AND DRAG STAY LOWER ARM TO MAIN FITTING EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 322100-220-814

ALL

N

AMM 322100-220-815

ALL

N

AMM 322100-220-816

ALL

N

AMM 322100-220-817

ALL

Page : STR - 32 [6 / 7] ATA

: 32


32

LANDING GEAR

Task Number

Zone

322106-02-1

711

Task Title

Task code

DI

NOSE GEAR DETAILED INSPECTION OF NLG UPPER & LOWER LOCK LINKS, LOCK LINK CENTER PIN AND LOCK LINK UPPER ARM TO MAIN FITTING PIN EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP

322109-01-1

322119-01-1

123 711

NOSE LANDING GEAR

123

NOSE GEAR

DETAILED INSPECTION OF NLG RETRACTION ACTUATOR AND ATTACHMENT PINS EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS, FITTINGS AND BUSH FLANGES. note:CPCP DI

DETAILED INSPECTION OF NLG RETRACTION ACTUATOR PIN (AIRFRAME). NOTE 9

Issue No

:

Date

:

10 01/12/2013

DI

Amendment No Date

: 01 : 06/09/2014

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

10 YE

I

10 YE

References

Ctrl

Eff

N

AMM 322100-220-818

ALL

N

AMM 322100-220-819

ALL

N

AMM 322100-220-820

ALL

Page : STR - 32 [7 / 7] ATA

: 32


52

DOORS

Task Number

Zone

521104-01-1

831 841

Task Title


Task code

DI

DETAILED INSPECTION OF DOOR 1 (FORWARD PASSENGER/CREW DOOR), INTERNAL STRUCTURE note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 521100-200-801

ALL

N

AMM 521200-200-801

ALL

Access panels :

831

841

Total access time :

0.04 Hrs

Skills :

1.20 MHrs

1 AF 832 842

521202-01-1

DI

MID PASSENGER/CREW DOOR DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR), INTERNAL STRUCTURE TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : DOOR LINING; DOOR INSULATION; ESCAPE SLIDE; note:CPCP Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

8.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [1 / 8] ATA

: 52


52

DOORS

Task Number

Zone

521302-01-1

833 843

Task Title

Task code

DI

AFT PASSENGER/CREW DOOR DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR), INTERNAL STRUCTURE note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 521300-200-801

ALL

N

AMM 522200-200-802

ALL

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

8.00 MHrs

1 AF 834 844

522202-01-1

PASSENGER COMPARTMENT EMERGENCY EXIT DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR), INTERNAL STRUCTURE note:CPCP

DI

Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

8.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [2 / 8] ATA

: 52


52

DOORS

Task Number

Zone

523102-01-1

821

Task Title

FORWARD CARGO COMPARTMENT DOOR

Task code

DI

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 000 FC

I

4 400 CY

References

Ctrl

Eff

N

AMM 523100-220-801

ALL

N

AMM 523100-220-803

ALL

Access panels :

821AR

821BR

Total access time :

821CR 821DR 0.00 Hrs

Skills :

4.00 MHrs

1 AF 821

523103-01-1

FORWARD CARGO COMPARTMENT DOOR DETAILED INSPECTION OF LATCHING HOOKS OF FORWARD CARGO COMPARTMENT DOOR (10 PLACES)

DI

Access panels :

821

821AR

Total access time :

821BR 0.02 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [3 / 8] ATA

: 52


52

DOORS

Task Number

Zone

523105-01-1

821

Task Title


Task code

SDI

SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A

Threshold Interval

T

6 000 CY

I

6 000 CY

T

10 600 FC

I

800 CY

References

Ctrl

Eff

N

AMM 523100-250-801

ALL

N

AOT A330-A52L003-12 EAD 2012-0274

ALL

Access panels :


0.02 Hrs

Skills :

0.60 MHrs

1 NDT 821

523107-01-1

FORWARD CARGO COMPARTMENT DETAILED VISUAL INSPECTION OF OUTER SKIN RIVETS AND WHOLE INNER FORKS AT THE FRAME FORK END OF FR21 AND FR20B OF THE FORWARD CARGO DOOR. NOTE: - LESS THAN 18400 FC: 100 FC AFTER THE EFFECTIVE DATE OF EASA AD 2012-0274 (WHICHEVER OCCURS LATER). - EQUAL OR MORE THAN 18400 FC: 50 FC AFTER THE EFFECTIVE DATE OF EASA AD 2012-0274.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

Page : STR - 52 [4 / 8] ATA

: 52


52

DOORS

Task Number

Zone

523202-01-1

822

Task Title


Task code

DI

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 000 FC

I

4 400 CY

References

Ctrl

Eff

N

AMM 523200-220-801

ALL

N

AMM 523200-220-804

ALL

Access panels :

822AR

822BR

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 822

523203-01-1

AFT CARGO COMPARTMENT DOOR DETAILED INSPECTION OF LATCHING HOOKS OF AFT CARGO COMPARTMENT DOOR (10 PLACES)

DI

Access panels :

822

822AR

Total access time :

822BR 0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [5 / 8] ATA

: 52


52

DOORS

Task Number

Zone

523205-01-1

822

Task Title


Task code

SDI

SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A

Threshold Interval

T

6 000 FC

I

6 000 CY

T

12 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 523200-250-801

ALL

N

AMM 523300-220-801

ALL

N

AMM 523300-220-802

ALL

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 NDT 823

523302-01-1


DI

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE note:CPCP Skills :

4.00 MHrs

1 AF 823

523303-01-1

BULK CARGO COMPARTMENT DOOR DETAILED INSPECTION OF STOP FITTINGS ON BULK CARGO COMPARTMENT DOOR note:CPCP

DI

Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [6 / 8] ATA

: 52


52

DOORS

Task Number

Zone

524102-01-1

121 122 811

Task Title


Task code

DI

DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS AND HINGE FITTINGS ON FUSELAGE TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : DOOR FLOOR PANEL; note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

28 200 CY

I

14 200 CY

References

Ctrl

Eff

N

AMM 524111-200-803

ALL

N

AMM 524111-200-805

943

Access panels :


0.00 Hrs

Skills :

1.20 MHrs

1 AF R

524103-01-3S020

121 122 811

AVIONICS COMP ACCESS DOOR DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS PREP. : DOOR FLOOR PANEL;

DI

946 962 1019 1256 1266

Access panels :


0.02 Hrs

Skills :

0.75 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [7 / 8] ATA

: 52


52

DOORS

Task Number

Zone

528103-01-1

734 744

Task Title

Task code

DI

MAIN GEAR DOORS DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, FORWARD AND AFT FITTINGS, LH/RH note:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 528100-200-803

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 52 [8 / 8] ATA

: 52

Eff ALL


53

FUSELAGE

Task Number

Zone

531101-01-1

110

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE BULKHEAD ATTACHED TO FR 1 note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 531100-200-801

ALL

N

AMM 531100-220-802

ALL

N

AMM 531100-200-804

ALL

Access panels :


0.00 Hrs

Skills :

0.80 MHrs

1 AF 200

531102-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL VISIBLE PORTIONS OF FRAMEWORK BETWEEN FR 3 AND FR 10, LH/RH note:CPCP Skills :

0.75 MHrs

1 AF 200

531104-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL PORTIONS OF FRAMEWORK COVERED BY RETAINERS PREP. : RETAINERS; note:CPCP Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [1 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531105-01-1

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL VISIBLE PORTIONS OF RETAINERS note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

17 000 CY

I

10 000 CY

References

Ctrl

Eff

N

AMM 531100-200-805

ALL

N

AMM 531100-200-836

943

Skills :

0.40 MHrs

1 AF R

531106-01-5S020

200

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.

946 962 1019 1256 1266

Skills :

1.00 MHrs

1 AF 200

531111-01-3

NOSE FORWARD FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 10 AND FR 18 FROM STR 9 (FWD AND AFT) TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

GVI

T

11 400 CY

I

11 400 CY

N

AMM 531100-210-817

Page : STR - 53 [2 / 74] ATA

: 53

ALL


53

FUSELAGE

Task Number

Zone

531113-01-1

221 222

100

531115-01-2

Task Title

Task code

DI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE OF THE UPPER SIDE OF THE FR 12A STIFFENER FITTING AT FLOOR CROSS BEAM ATTACHMENT LEVEL, LH/RH. PREP. : CABIN ATTENDANT SEATS (IF INSTALLED) CREW REST ROOM IF INSTALLED FLOOR PANELS FROM FR 10 TO FR 13 GALLEYS LAVATORY IF INSTALLED NOTE 1 STOWAGE (IF INSTALLED) VIDEO CONTROL CENTER (IF INSTALLED)

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN AND FAIL SAFE RING, WHERE INSTALLED, OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RH NOTE: CPCP

Threshold Interval

T

13 000 FC

I

10 000 CY

T

12 YE

I

6 YE

References

Ctrl

N

N

AMM EAD FAD ISB

531100-250-822 F-2003-205 2005-03-12 53-3135

275

AMM 531100-200-812

ALL

Skills :

1.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff

Page : STR - 53 [3 / 74] ATA

: 53

294 299 366


53

FUSELAGE

Task Number

Zone

531117-01-1

121 122

Task Title

Task code

GVI

AVIONICS COMPARTMENT GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 1 AND FR 20 FROM CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL INCLUDING CABIN FLOOR SUPPORT STRUCTURE AND NLG BAY PANELS AND BEAMS NOTE: TPS APPLICATION REQUIRED ONLY BETWEEN FR 10 AND FR 20, EXCLUDING NLG BAY PANELS TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : AVIONIC BAY FLOOR PANELS . note:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 531100-210-805

ALL

N

AMM 531100-220-803

ALL

Check : C8

Skills :

5.00 MHrs

1 AF 121 122

531121-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 10 AND FR 20 BELOW AVIONICS COMPARTMENT FLOOR LEVEL TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : AVIONICS BAY FLOOR PANEL; NOTE:CPCP

T

12 YE

I

12 YE

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [4 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531122-01-1

121 122

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 1 AND FR 10 BELOW AVIONICS COMPARTMENT FLOOR LEVEL NOTE:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 531100-210-802

ALL

N

AMM 531100-220-804

ALL

Check : C8

Skills :

1.40 MHrs

1 AF 121 122

531123-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW GALLEYS AND TOILETS FROM CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL BETWEEN FR 10 AND FR 13A, LH/RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : NOTE 1; NOTE: CPCP

T

6 YE

I

6 YE

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [5 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

531124-01-6S020

123

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH

Threshold Interval

References

Ctrl

N

AMM 531100-200-835

Eff 943

T

93 100 FH

T

17 000 CY

I

93 100 FH

962

17 000 CY

1019

I

946

1256 1266

Access panels :

713

714

Total access time :

0.16 Hrs

Skills :

0.50 MHrs

1 AF R

531125-01-5S020

121 122

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH

T

17 000 FC

I

17 000 CY

N

AMM 531100-200-859

943 946 962 1019 1256 1266

Skills :

1.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [6 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531126-01-1

123

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF NOSE LANDING GEAR AFT SIDE PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, LH/RH note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 531100-200-817

ALL

N

AMM 531100-200-819

ALL

Access panels :

713

714

Total access time :

715 716 0.00 Hrs

Skills :

0.50 MHrs

1 AF 123

531129-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : BOLTS; NLG ACTUATORS DISCONNECTED; note:CPCP Access panels :

713

714

Total access time :

715 716 0.00 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [7 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

531129-02-3S020

123

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING PREP. : BOLTS; NLG ACTUATORS DISCONNECTED;

Threshold Interval

T

28 200 CY

I

11 500 CY

References

Ctrl

N

AMM 531100-200-861

Eff 943 946 962 1019 1256 1266

Access panels :

713

714

715

Total access time :

716

0.36 Hrs

Skills :

0.75 MHrs

1 NDT R

121 122

531130-01-3


SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 16A AT CABIN FLOOR LEVEL, LH/RH. PREP. : INSULATION Z220;

T

30 500 CY

I

10 700 CY

N

AMM 531100-200-845

275 943 946 962 1019 1256 1266

R

121 122

531131-01-3

Issue No

:

Date

:

10 01/12/2013

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 16A, JOINT AREA BETWEEN STRINGERS 28 AND 30, LH/RH. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 531131-02-3. PREP. : INSULATION Z220;

Amendment No Date

: 01 : 06/09/2014

DI

T

24 800 CY

I

24 000 CY

N

AMM 531100-220-808

275 943 946 962 1019 1256 1266

Page : STR - 53 [8 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

531131-02-3

121 122

221 222

531136-01-3

Task Title

Task code

SDI

NOSE FORWARD FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 16A JOINT AREA BETWEEN STRINGERS 28 AND 30, LH/RH. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 531131-01-3. PREP. : INSULATION Z220;

T

24 800 CY

I

24 000 CY

References

Ctrl

N

AMM 531100-250-803

Eff 275 943 946 962 1019 1256 1266

DI


Threshold Interval

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 12 AND 13 DOUBLER AREA AT CROWN CENTERLINE PREP. : CEILING PANELS Z220; INSULATION Z220;

T

24 500 CY

I

10 100 CY

N

AMM 531100-220-811

275 943 946 962 1019 1256 1266

123

531137-01-1

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF NOSE LANDING GEAR DRAG STRUT FITTING ATTACHMENTS TO UPPER AND FORWARD CANTED PANEL note:CPCP

T

12 YE

I

12 YE

N

AMM 531100-220-836

Access panels :

713

714

715

Total access time :

716

0.00 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [9 / 74] ATA

: 53

ALL


R

53

FUSELAGE

Task Number

Zone

531143-01-3S020

121 122

Task Title

Task code

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING AT FR.14, LH/RH. PREP. : AIR DUCTS; NOTE 1; VACUUM PIPES;

Threshold Interval

T

17 000 CY

I

3 900 CY

References

Ctrl

N

AMM 531100-220-837

Eff 943 946 962 1019 1256 1266

Skills :

0.60 MHrs

1 AF R

531149-01-2S020

211 212

DI

NOSE FORWARD FUSELAGE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING TOP 3 NUTS ON CENTRE POST.

T

28 400 CY

I

8 500 CY

N

AMM 531100-220-838

943 946 962 1019 1256 1266

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [10 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531150-01-1

211 212

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE BULKHEAD ABOVE FLOOR LEVEL, INCLUDING FR 1, AS FAR AS VISIBLE. NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THE PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETE AFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED AND ELECTRONIC DEVICE REMOVED. PREP. : ACCESS BETWEEN FR1 AND FR2 FROM AVIONIC BAY; INSULATION PANELS; NOTE 1; NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 531100-200-820

Access panels :

311VU

312VU

Total access time :

313VU 314VU 0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [11 / 74] ATA

: 53

Eff ALL


53

FUSELAGE

Task Number

Zone

531151-01-1

121 122

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR PANELS, INCLUDING FR 1 AND STRINGER CONNECTIONS. NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THE PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETE AFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED AND ELECTRONIC DEVICE REMOVED. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : AVIONICS FORWARD FLOOR PANELS; INSULATION PANELS; WIRING BUNDLES DISPLACED; NOTE: CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 531100-200-829

ALL

N

AMM 531100-200-821

275

Skills :

1.00 MHrs

1 AF R

211 212

531152-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND FORWARD). note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

943 946

See note

962

Check : NT

1019 1256 1266

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [12 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531152-01-1S100

211 212

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND FORWARD). note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 531100-200-821

Eff 294 299 366

Skills :

1.00 MHrs

1 AF R

531158-01-2S020

211 212

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 AND 9 UPPER MEMBERS, LH/RH. PREP. : LINING; NOTE 1;

T

17 000 CY

I

15 500 CY

N

AMM 531100-220-842

946 962 1019 1256 1266

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 53 [13 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531159-01-1

221 222

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AROUND DOOR 1 (FORWARD PASSENGER/CREW DOOR), BETWEEN FR 13A AND FR 17 AND BETWEEN FLOOR LEVEL AND STR 9 (AFT), LH/RH. TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : LAVATORY IF INSTALLED; LINING; NOTE 1; note:CPCP

Threshold Interval

References

Ctrl

Eff

N

AMM 531100-200-823

ALL

N

AMM 531100-200-839

275

N

AMM 531100-270-809

943

T

12 YE

I

6 YE

T

38 000 CY

I

38 000 CY

T

79 500 FH

T

17 000 CY

I

60 000 FH

962

16 600 CY

1019

Skills :

1.00 MHrs

1 AF 531161-01-3

R

531165-01-1

233 234

MAIN STRUCTURE

120 123

MAIN STRUCTURE

DI

DETAILED INSPECTION OF PAX / CREW DOOR UPPER KEEL FITTING AT FR.18 FORWARD AND AFT FACE, AT STR.12 LEVEL, INTERNAL STRUCTURE, LH/RH. PREP. : DOOR FRAME LINING Z220;

SPECIAL DETAILED INSPECTION OF FRAME 17 INNER FLANGE FASTENER HOLE AT Y+/- 750, JUNCTION WITH THE FITTING, LH/RH

SDI

I

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [14 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531171-01-1

210 220

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 17 TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : CABIN FLOOR PANELS; note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

5 YE

I

5 YE

References

Ctrl

Eff

N

AMM 531100-210-803

ALL

N

AMM 531100-200-865 SIL 53-091

275

Skills :

0.00 MHrs

1 AF 210 220

531172-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING DOORS ENTRANCE AREA FROM FR 10 TO FR 17 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE NOT INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : CABIN FLOOR PANELS; FCRC (IF INSTALLED); GALLEYS AND TOILETS; NOTE: CPCP

299 366

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 53 [15 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

531172-02-1

210 220

121 122

531173-01-1

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING DOORS ENTRANCE AREA FROM FR 10 TO FR 17 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : CABIN FLOOR PANELS; FCRC (IF INSTALLED); GALLEYS AND TOILETS; NOTE: CPCP

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL, BETWEEN FR 13A AND FR 17, LH/RH note:CPCP

T

6 YE

I

6 YE

References

Ctrl

N

AMM 531100-200-865 SIL 53-091

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

946

1256 1266

T

6 YE

I

6 YE

N

AMM 531100-200-826

Check : C4

0.60 MHrs

: 01 : 06/09/2014

943 962

Skills :

1 AF

Eff

1019

DI

MAIN STRUCTURE

Threshold Interval

Page : STR - 53 [16 / 74] ATA

: 53

ALL


R

53

FUSELAGE

Task Number

Zone

531175-01-4S020

231 232

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT STGR.14/18/22/24, LH/RH.

Threshold Interval

T

18 800 CY

I

7 950 CY

References

Ctrl

N

AMM 531100-200-840

Eff 943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF R

121

531176-01-1

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE BELOW BATTERIES BETWEEN FR 10A AND 11A AND BETWEEN STR 41 AND STR 43, LH note:CPCP

T

6 YE

I

6 YE

N

AMM 531100-210-804

ALL

N

AMM 531100-250-821

275

Check : C4

Skills :

0.10 MHrs

1 AF 223 224

531183-01-4

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH. PREP. : TOILETS, LINING, INSULATION TO BE DISPLACED, FASTENERS TO BEREMOVED;

Amendment No Date

: 01 : 06/09/2014

SDI

T

23 700 CY

I

9 600 CY

Page : STR - 53 [17 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

531184-01-1

200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A AND FROM FR.14 TO FR.16A, LH/RH.

Threshold Interval

T

35 700 CY

I

11 100 CY

T

20 000 FC

I

8 850 CY

T

23 700 CY

I

9 600 CY

References

Ctrl

Eff

N

AMM 531100-250-806

275

N

AMM 531100-200-841

275

N

AMM 531100-200-851

943

Skills :

0.40 MHrs

1 NDT 531185-01-2

R

531186-01-1

Issue No

:

Date

:

221 222

MAIN STRUCTURE

223 224

MAIN STRUCTURE

10 01/12/2013

DI

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PASSENGER / CREW DOOR CUTOUT AFT UPPER CORNER, JUNCTION OF INTERNAL PLATE ON FR. 17, BETWEEN STR.12 AND 13, LH/RH. PREP. : LINING NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH PREP. : DOOR FRAME LININGS Z220; INSULATION Z220; LAVATORIES Z220;

Amendment No Date

: 01 : 06/09/2014

SDI

946 962 1019 1256 1266

Page : STR - 53 [18 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

531188-01-5

100 200

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9 FWD LEVEL, LH/RH.

Threshold Interval

T

22 200 CY

I

7 050 CY

References

Ctrl

N

AMM 531100-200-868

Eff 943 946 962 1019 1256 1266

R

531189-01-3S020

221 222

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERO AT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B, LH/RH PREP. : DOOR FRAME LININGS Z220; INSULATION Z220;

T

25 100 CY

I

15 100 CY

N

AMM 531100-200-854

943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF R

531198-01-3S020

121 122

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH PREP. : INSULATION Z120;

T

25 100 CY

I

15 100 CY

N

AMM 531100-200-844

943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [19 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532102-01-1

133 134

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 20 AND FR 39.1 BELOW CARGO COMPARTMENT FLOOR PANELS note:CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 532100-210-821

ALL

N

AMM 532100-200-810

ALL

Check : C4

Access panels :


0.02 Hrs

Skills :

5.00 MHrs

1 AF 131 132

532104-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE FROM PASSENGER CABIN FLOOR TO CARGO COMPARTMENT FLOOR, BELOW AND 0,75 M FWD AND AFT OF GALLEYS AND TOILETS, FROM FR 20 TO FR 39.1, LH/RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : CARGO COMPARTMENT LINING; NOTE 1; NOTE: CPCP

T

6 YE

I

6 YE

Check : C4

Access panels :


0.02 Hrs

Skills :

4.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [20 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532105-01-1

134

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 19 AND FR 26 FROM CARGO COMPARTMENT FLOOR TO STR 46 RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : BALLMATS; NOTE :CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 532100-200-801

Check : C4

Access panels :


0.02 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [21 / 74] ATA

: 53

Eff ALL


53

FUSELAGE

Task Number

Zone

532107-01-1

134

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR 25 (10 PLACES) TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

Threshold Interval

References

Ctrl

N

AMM 532100-200-811

Eff 275

T

7 400 CY

T

6 YE

294

I

7 400 CY

299

I

6 YE

366 943 946 962 1019 1256 1266

Access panels :


0.02 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [22 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

532107-02-1

134

Task Title

Task code

Threshold Interval

DI

T

6 YE

DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND FR 25 PREP. : ECCENTRIC BOLTS; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 THRESHOLD IS NEXT 4C CHECK FROM APPROVE DATE

I

6 YE

MAIN STRUCTURE

References

Ctrl

N

AMM 532100-220-816

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AF 532107-02-1S100

134

DI

MAIN STRUCTURE DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND FR 25 PREP. : ECCENTRIC BOLTS; note:CPCP

T

24 YE

I

6 YE

N

AMM 532100-220-816

299 366

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 53 [23 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532108-01-1

122 132

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AROUND FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 19 AND FR 26 FROM STR 26 RH TO CARGO COMPARTMENT FLOOR LEVEL note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

20 000 FC

I

2 200 CY

T

17 000 CY

I

2 200 CY

References

Ctrl

Eff

N

AMM 532100-200-804

ALL

N

AMM 532100-210-803

ALL

N

AMM 532100-210-803

943

Access panels :


0.02 Hrs

Skills :

2.00 MHrs

1 AF D

200

532117-01-3

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-3. Skills :

4.00 MHrs

1 AF 200

532117-01-5

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-5.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

GVI

962 1019 1256 1266

Page : STR - 53 [24 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532117-02-3

200

Task Title

MAIN STRUCTURE

Task code

DI

DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-3. R

200

532117-02-5

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, LH/RH. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-5.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

Threshold Interval

T

20 000 FC

I

6 900 CY

T

17 000 CY

I

6 900 CY

References

Ctrl

Eff

N

AMM 532100-220-830

ALL

N

AMM 532100-220-830

943 946 962 1019 1256 1266

Page : STR - 53 [25 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532122-01-1

131 132

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT BETWEEN FR 32 AND FR 36, FROM CABIN FLOOR DOWN TO STR 30, LH/RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : AIR CONDITIONING DUCTS; NOTE 1; SIDEWALL LINING; NOTE: CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 532100-200-802

Access panels :


0.02 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [26 / 74] ATA

: 53

Eff ALL


53

FUSELAGE

Task Number

Zone

532123-01-1

241 242 243 244

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUTOUT BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOOR UP TO STR 9, LH/RH. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : NOTE 1; SIDEWALL/DOOR FRAME LINING; NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

6 YE

References

Ctrl

Eff

N

AMM 532100-200-808

ALL

N

AMM 532100-200-809

ALL

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 100

532124-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH PREP. : SCUFF PLATES BELOW Z832/Z842; note:CPCP Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [27 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532129-01-2

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 37.1 FROM FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE

Threshold Interval

T

128 300 FH

References

Ctrl

Eff

N

AMM 532100-210-823

275

N

AMM 532100-210-823

943

T

18 800 CY

I

106 600 FH

I

17 700 CY

T

137 000 FH

T

20 100 CY

I

86 200 FH

962

14 300 CY

1019

Skills :

2.00 MHrs

1 AF R

200

532129-01-3

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 37.1 FROM FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE

I

946

1256 1266

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [28 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532134-01-1

231 232 241 242

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING DOORS ENTRANCE AREAS, FROM FR 17 TO FR 36 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE NOT INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS; GALLEYS; TOILETS; NOTE: CPCP

Threshold Interval

T

5 YE

I

5 YE

References

Ctrl

N

AMM 532100-200-803 SIL 53-091

0.00 Hrs

Skills :

8.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294 366

841

Total access time :

275 299

Access panels :

831

Eff

Page : STR - 53 [29 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

532134-02-1

231 232 241 242

200

532142-01-2

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.5 M AROUND GALLEYS AND TOILETS, FROM FR 17 TO FR 36 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD SECTION 7 ARE INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS GALLEYS TOILETS NOTE: CPCP

T

6 YE

I

6 YE

References

Ctrl

N

AMM 532100-210-851

Eff 943 946 962 1019 1256 1266

DI

MAIN STRUCTURE

Threshold Interval

DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNA CUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTER LINE, EXTERNAL SURFACE

T

37 600 CY

I

18 800 CY

T

32 300 CY

I

18 800 CY

N

AMM 532100-210-826

275

N

AMM 532100-210-830

ALL

Skills :

0.10 MHrs

1 AF 200

532146-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 26 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [30 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532149-01-2

231 232 233 234

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR 26, FROM STR 4 TO STR 6 STR 12 TO STR 14 AND STR 21 TO STR 22, LH/RH PREP. : CEILING PANELS Z230; INSULATION Z230; SIDEWALL PANELS Z230;

Threshold Interval

References

Ctrl

Eff

N

AMM 532100-220-810

ALL

N

AMM 532100-220-811

275

N

AMM 532100-220-812

943

T

32 300 CY

I

18 800 CY

T

23 400 CY

I

15 300 CY

T

137 000 FH

T

20 100 CY

I

88 800 FH

962

I

13 900 CY

1019

Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 200

532150-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 37.1. Skills :

0.00 MHrs

1 NDT R

200

532156-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH

946

1256 1266

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [31 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

532157-01-3

243 244

532162-01-2

533006-01-1

Task code

Task Title

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR 15, LH/RH PREP. : INSULATION Z240; SIDEWALL LININGS Z240;

233 234

MAIN STRUCTURE

147 148 149 197 198

CENTER FUSELAGE

Threshold Interval

T

19 400 CY

I

15 900 CY

References

Ctrl

N

AMM 532100-220-805

946 962 1256 1266

DI

DI

DETAILED INSPECTION OF BELLY FAIRING SUPPORT STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB.

T

36 800 CY

I

23 600 CY

T

3 YE

I

3 YE

N

AMM 532100-210-838

275

N

AMM 533100-220-805

275 294 299 366

Access panels :

147BT 197FB 198HB

Total access time :

148BB 197GB 734

148BT 197HB 744

197AB 198AT 753

197AT 198BB 754

197BB 198EB

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

1019

DETAILED INSPECTION OF SKIN AROUND SATCOM (45 DEG) ANTENNA CUT-OUT BETWEEN FR 26.1 AND FR 26.3 AND BETWEEN STR 12 AND STR 13, LH/RH, EXTERNAL SURFACE

147BB 197EB 198GB

Eff

Page : STR - 53 [32 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533006-01-2

147 148 149 197 198

Task Title

Task code

DI

CENTER FUSELAGE DETAILED INSPECTION OF BELLY FAIRING SUPPORT STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB.

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 533100-220-805

Eff 943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 190

533008-01-1

DI

CENTER FUSELAGE DETAILED INSPECTION OF BELLY FAIRING PANELS AND FASTENERS AT WING UPPER SURFACE TO FUSELAGE JUNCTION, FROM WING LEADING EDGE TO TRAILING EDGE, LH/RH

N

AMM 533100-220-808

ALL

N

AMM 533100-290-805

275

T

3 YE

I

3 YE

T

149 900 FH

T

23 000 CY

294

I

131 700 FH

299

I

20 200 CY

366

Skills :

1.50 MHrs

1 AF 263 264

533012-01-3

Issue No

:

Date

:

10 01/12/2013

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO 5, LH/RH. NOTE : - ROTOTEST INSPECTION 1MM - THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-3 PREP. : INSULATION Z260; OVERHEAD STOWAGE BINS Z260;

Amendment No Date

: 01 : 06/09/2014

SDI

Page : STR - 53 [33 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533012-02-3

263 264

145 146

533013-01-2

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO 5, LH/RH. NOTE : - X-RAY INSPECTION 5 MM - THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-3 PREP. : INSULATION Z260; OVERHEAD STOWAGE BINS Z260;

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH NOTE: MSN 275 BECOME SAMPLE A/C THRESHOLD IS 26600 FC OR 173200 FH

Threshold Interval

References

Ctrl

N

AMM 533100-260-803

Eff 275

T

149 900 FH

T

23 000 CY

294

I

37 400 FH

299

I

5 750 CY

366

T

173 200 FH

T

26 600 CY

I

47 800 FH

I

7 350 CY

T

185 100 FH

T

27 300 CY

I

49 900 FH

962

7 550 CY

1019

N

AMM 533100-250-805

275

N

AMM 533100-250-805

943

Skills :

0.00 MHrs

1 NDT R

145 146

533013-01-5

Issue No

:

Date

:

10 01/12/2013

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH PREP. : FLOOR PANELS Z250; INSULATION Z250; SEATS AND FURNISHINGS Z250;

Amendment No Date

: 01 : 06/09/2014

SDI

I

946

1256 1266

Page : STR - 53 [34 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533014-01-3

147 148

147 148

533015-01-1

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF FRAME 47 DATUM, LH/RH

DI

CENTER FUSELAGE DETAILED INSPECTION OF MAIN LANDING GEAR BAY, LOWER FLANGE OF GANTRY Y=1959 AT FRAME 48 LEVEL, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-250-807

Eff 275

T

230 000 FH

T

35 300 CY

294

I

206 500 FH

299

I

31 700 CY

366

T

144 700 FH

T

21 800 CY

I

97 900 FH

I

15 000 CY

T

60 000 FH

T

17 000 CY

I

26 100 FH

962

3 850 CY

1019

N

AMM 533100-220-851

275

N

AMM 533100-250-808

943

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF R

533016-01-4S020

200

SDI


I

946

1256 1266

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [35 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533016-01-5

200

Task Title

Task code

SDI


200

533019-01-1

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM CENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 AND STRG5) LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-250-808

Eff 275

T

123 200 FH

T

18 200 CY

294

I

34 700 FH

299

I

5 100 CY

366

T

60 000 FH

T

20 000 CY

I

143 600 FH

I

21 200 CY

T

60 000 FH

T

17 000 CY

I

143 900 FH

962

21 200 CY

1019

N

AMM 533100-250-836

275

N

AMM 533100-250-836

943

Skills :

0.00 MHrs

1 NDT R

533019-01-2S020

200

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM CENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 AND STRG5) LH/RH

I

946

1256 1266

Skills :

0.30 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [36 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533035-01-1

190

Task Title

Task code

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH. TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FAIRING PANELS Z191; FAIRING PANELS Z192; FAIRING PANELS Z193; FAIRING PANELS Z195; NOTE: CPCP

Threshold Interval

T

30 MO

I

30 MO

References

Ctrl

N

AMM 533100-200-860

Eff 275 294 299 366

Skills :

2.00 MHrs

1 AF R

190

533035-01-2

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELL FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37. AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH. TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FAIRING PANELS Z191; FAIRING PANELS Z192; FAIRING PANELS Z193; FAIRING PANELS Z195;

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

GVI

T

6 YE

I

6 YE

N

943 946 962 1019 1256 1266

Page : STR - 53 [37 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533036-01-1

190

Task code

Task Title

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE BETWEEN FR 47 AND FR 56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH. note:CPCP

Threshold Interval

T

5 YE

I

5 YE

References

Ctrl

N

AMM 533100-200-862

Eff 275 294 299 366

Access panels :

147AB 148BT 197HB

147AT 197AB 198AT

Total access time :

147BB 197AT 198BB

147BT 197BB 198EB

148AB 197EB 198GB

148AT 197FB 198HB

148BB 197GB

1.70 Hrs

Skills :

0.00 MHrs

1 AF R

190

533036-01-2

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE BETWEEN FR 47 AND FR 56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH. TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

GVI

T

6 YE

I

6 YE

N

943 946 962 1019 1256 1266

Page : STR - 53 [38 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533037-01-1

190

Task Title

Task code

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 AND FR.56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE, EXCLUDING AREA FROM Y=-2390 TO Y=2390, LH/RH. TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FAIRING PANELS Z147; FAIRING PANELS Z148; FAIRING PANELS Z191; FAIRING PANELS Z192; FAIRING PANELS Z197; FAIRING PANELS Z198; NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

T

60 000 FH

T

20 000 CY

I

46 000 FH

I

7 250 CY

References

Ctrl

Eff

N

AMM 533100-210-817

ALL

N

AMM 533100-210-805

275

Skills :

0.50 MHrs

1 AF 100 200

533101-01-6

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO STRINGER 6, EXTERNAL SURFACE, LH/RH Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [39 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533101-01-9S020

100 200

Task Title

Task code

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO STRINGER 6, EXTERNAL SURFACE, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-210-805

Eff 943

T

60 000 FH

T

17 000 CY

I

50 600 FH

962

7 750 CY

1019

I

946

1256 1266

Skills :

3.00 MHrs

1 AF N

200

533104-02-6

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND - UPPER BEACON LIGHT CUTOUTS BETWEEN FR.40.3 AND FR.41 - OBTURATOR CUTOUT BETWEEN FR.42 AND FR.43 - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN STRINGER 1 LH AND STRINGER 1 RH - AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND FR.40.1 PREP. : ANTICOLLISION LIGHTS, ANTENNAS AND OBTURATORS WHERE INSTALLED;

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

DI

T

128 200 FH

T

18 900 CY

I

7 400 CY

N

AMM 533100-220-923

Page : STR - 53 [40 / 74] ATA

: 53

946


R

53

FUSELAGE

Task Number

Zone

533106-01-5S020

200

Task Title

Task code

DI

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-220-850

Eff 943

T

77 900 FH

T

11 500 CY

I

56 600 FH

962

8 350 CY

1019

I

946

1256 1266

Skills :

2.00 MHrs

1 AF R

533109-01-2S020

200

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22 FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARD AND AFT FRAME 45 LEVEL, LH/RH

T

17 000 FC

I

10 200 CY

N

AMM 533100-250-806

946 962 1019 1256 1266

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 53 [41 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533114-01-5S020

251 252

Task Title

Task code

SDI

CENTER FUSELAGE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTION WITH STABILIZERS STRINGER 20 TO 23, LH/RH

Threshold Interval

References

Ctrl

N

AMM 533100-200-846

Eff 943

T

103 200 FH

T

14 700 CY

I

100 000 FH

962

14 700 CY

1019

I

946

1256 1266

Access panels :

251XW

252XW

Total access time :

0.06 Hrs

Skills :

0.30 MHrs

1 NDT 191 192 193

533117-01-1

DI

FR40 BULKHEAD DETAILED INSPECTION OF FR.40 PRESSURE BULKHEAD, AFT FACE BELOW CENTER WING BOX TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : RH ONLY:AIR CONDITIONING PACK; note:CPCP

T

12 YE

I

12 YE

N

AMM 533100-200-803

Access panels :

191KB

192PB

Total access time :

193BB 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [42 / 74] ATA

: 53

ALL


53

FUSELAGE

Task Number

Zone

533122-01-1

149

Task Title

Task code

GVI

CENTER LANDING GEAR WELL GENERAL VISUAL INSPECTION OF CLG WELL; KEEL BEAM INTERNAL STRUCTURE AND PANELS BETWEEN FR 47 AND FR 53.2 NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA. NOTE: CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 533100-200-830

ALL

N

AMM 533100-200-831

ALL

Skills :

1.00 MHrs

1 AF 147 148

533123-01-1

DI

MAIN LANDING GEAR BAY DETAILED INSPECTION OF MAIN LANDING GEAR BAY, PRESSURE DIAPHRAGMS AND PRESSURIZED FLOORS LOWER SURFACE, BETWEEN FR.47 AND FR.53.2 note:CPCP Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [43 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533124-01-2

147 148 149

Task code

Task Title

DI

CENTER LANDING GEAR WELL DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT CLG DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

21 300 FC

I

21 300 CY

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 533100-220-814

275

N

AMM 533100-200-834

ALL

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 191 192 193 195 196

533127-02-1

GVI

AIR CONDITIONING ACCESS CUTOUT GENERAL VISUAL INSPECTION OF AREA AROUND AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE note:CPCP Access panels :

191KB

192PB

Total access time :

193BB 193DB 0.00 Hrs

195AB

196AB

Skills :

2.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [44 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533129-01-1

143 149 191 192 193 195 196

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF KEEL BEAM INTERNAL AND EXTERNAL STRUCTURE SKIN AND ADJACENT FUSELAGE STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE PREP. : FAIRING PANELS BETWEEN FR 40 AND FR 47; note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 533100-220-804

ALL

N

AMM 533100-200-813

ALL

Access panels :

191KB

193BB

Total access time :

193DB 195AB 0.00 Hrs

734

744

Skills :

0.00 MHrs

1 AF 147 148 149

533135-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF CLG AND MLG DOOR HINGE FITTINGS NO 1 THROUGH NO 6, DOOR ACTUATOR FITTINGS AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED note:CPCP Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [45 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533141-01-1

151 152

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND CARGO COMPARTMENT FLOOR LEVEL PREP. : CARGO FLOOR PANELS; LD-MCR IF INSTALLED OR POST 46678 LDL TOILETS AND FURNISHINGS; LINING; NOTE :CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 533100-200-814

ALL

N

AMM 533100-200-815

ALL

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF 137 138

533142-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE AND STR 40, FROM AFT FACE OF CARGO COMPARTMENT REAR PANEL note:CPCP Access panels :


0.02 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [46 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533143-01-1

153 154

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR LEVEL note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 533100-220-802

ALL

N

AMM 533100-220-803

ALL

N

AMM 533100-200-819

275

Skills :

0.40 MHrs

1 AF 137 138

533144-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE INTERNAL STRUCTURE BELOW STR 40, FROM FR 39.1 TO FR 40 note:CPCP Skills :

0.80 MHrs

1 AF 145 146

533150-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF PRESSURIZED FLOORS AND PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE FITTED ABOVE THIS AREA. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : CABIN FLOOR PANELS Z250; GALLEYS Z250; LAVATORIES Z250; NOTE: CPCP

294 299 366

Skills :

1.40 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [47 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533150-02-1

145 146

533154-01-6S020

145 146

Task Title

Task code

DI

MAIN STRUCTURE

12 YE

N

AMM 533100-200-836

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

1256 1266

T

31 700 CY

I

31 700 CY

N

AMM 533100-220-819

943 946 962 1019 1256 1266

2.00 MHrs

: 01 : 06/09/2014

943 962

Skills :

1 AF

Eff

1019

DI

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1, LH/RH PREP. : CABIN FLOOR PANELS; GALLEYS; TOILETS;

T

References

Ctrl

Check : 8C

DETAILED INSPECTION OF PRESSURIZED FLOORS AND PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2 NOTE: - IF NO GALLEYS/TOILETS ARE INSTALLED TPS APPLICATION MAY BE LIMITED TO PRESSURIZED FLOORS AND PRESSURE DIAPHRAGM. - TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT FITTED ABOVE THIS AREA. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : CABIN FLOOR PANELS Z250; NOTE: CPCP MAIN STRUCTURE

Threshold Interval

Page : STR - 53 [48 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533156-01-3

151 152

250

533170-01-1

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. PREP. : LD-MCR IF INSTALLED; LINING; NOTE 1;

DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 AND FR 53.5 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE NOT INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS Z250; GALLEYS Z250; LAVATORIES Z250; NOTE: CPCP

References

Ctrl

N

AMM 533100-270-801

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

T

29 700 CY

I

46 100 FH

962

7 100 CY

1019

946

1256 1266

T

5 YE

I

5 YE

N

AMM 533100-200-825 SIL 53-091

275 294 299 366

1.00 MHrs

: 01 : 06/09/2014

943

193 500 FH

Skills :

1 CA

Eff

T

I

DI

MAIN STRUCTURE

Threshold Interval

Page : STR - 53 [49 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

533170-02-1

250

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 AND FR 53.5 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS Z250; GALLEYS Z250; LAVATORIES Z250;

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 533100-200-866 SIL 53-091

Eff 943 946 962 1019 1256 1266

Skills :

1.00 MHrs

1 CA 250

533171-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 AND FR 53.5 TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : FLOOR PANELS Z250;

T

12 YE

I

12 YE

N

AMM 533100-200-826

Skills :

1.00 MHrs

1 CA

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [50 / 74] ATA

: 53

ALL


53

FUSELAGE

Task Number

Zone

533189-01-1

137 138

261 262

533190-01-1

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF FWD LOWER SHELL PANEL BTW STR 35 AND STR 36, LHS, FROM FR 39.2 TO FR 40 AT INERTING SYSTEM CROSSING AREA. PREP. : LININGS FROM FR 39.2 TO FR 40 AROUND STR 35; SIDEWALL PANELS Z130;

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR 53.4 AND 53.8 FROM CABIN FLOOR LEVEL TO STR 9, LH/RH note:CPCP

Threshold Interval

T

60 000 FH

T

17 000 CY

I

31 800 FH

I

4 700 CY

T

12 YE

I

6 YE

References

Ctrl

N

AMM 533100-250-862

N

AMM 533100-200-827

844

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

1256 1266

Access panels :

834

Eff

Page : STR - 53 [51 / 74] ATA

: 53

ALL


53

FUSELAGE

Task Number

Zone

533191-01-1

151 152

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW DOOR3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR 53.4 AND 53.8 FROM CABIN FLOOR DOWN TO CARGO FLOOR LEVEL, LH/RH note:CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 533100-200-828

ALL

N

AMM 533100-200-835

ALL

N

AMM 533100-220-933

ALL

Check : C4

Access panels :

151EW

151GW

Total access time :

152EW 152GW 0.00 Hrs

822

Skills :

0.50 MHrs

1 AF 100 200

533193-01-1

GVI

CENTER FUSELAGE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN (INCLUDING DOOR 3 CUT-OUT) BETWEEN FR 53.3 AND FR 54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTER LINE LH/RH, EXTERNAL SURFACE

T

17 000 FC

I

2 200 CY

T

17 000 CY

I

6 900 CY

Skills :

1.00 MHrs

1 AF D

100 200

533193-02-1

Issue No

:

Date

:

10 01/12/2013

CENTER FUSELAGE DETAILED INSPECTION OF FUSELAGE SKIN (INCLUDING DOOR 3 CUTOUT) BETWEEN FR 53.3 AND FR 54 FROM UPPER EDGE OF BELLY FAIRING TO STR 6 LH/RH, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ATERNATIVE TASK TO 533193-01-1. NOTE: APPLY TASK 533193-01-1

Amendment No Date

: 01 : 06/09/2014

DI

Page : STR - 53 [52 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

533195-01-1

100

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

45 300 FH

References

Ctrl

Eff

N

AMM 533100-200-829

ALL

N

AMM 533100-210-820

ALL

N

AMM 534100-210-801

275

Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

4.00 MHrs

1 AF 200

533199-01-2

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 38 AND FR 53.3 FROM STR 6 TO CROWN CENTER LINE, EXTERNAL SURFACE, LH/RH.

200

534102-01-4

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 58 FROM STRINGERS 13 TO CROWN CENTER LINE, EXTERNAL SURFACE, LH/RH.

T

7 250 CY

I

45 300 FH

I

7 250 CY

T

90 000 FH

T

25 800 CY

I

36 100 FH

I

10 300 CY

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [53 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

534102-01-5

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 58 FROM STRINGERS 13 TO CROWN CENTER LINE, EXTERNAL SURFACE, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 534100-210-801

Eff 943

T

60 000 FH

T

17 000 CY

I

43 800 FH

962

6 700 CY

1019

I

946

1256 1266

Skills :

0.40 MHrs

1 AF R

263 264

534104-01-6

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS 4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22, LH/RH PREP. : CEILING PANELS Z260; INSULATION Z260; OVERHEAD STOWAGE BINS Z260;

N

AMM 534100-220-801

943

T

60 000 FH

T

17 000 CY

I

55 200 FH

962

8 500 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT 263 264

534104-01-9

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS 4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22, LH/RH PREP. : CEILING PANELS; INSULATION; OVERHEAD STOWAGE BINS;

Amendment No Date

: 01 : 06/09/2014

SDI

N

AMM 534100-220-801

275

T

21 500 CY

I

74 600 FH

294

I

11 500 CY

299 366

Page : STR - 53 [54 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534120-01-2

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PAR OF WINDOW FORGINGS BETWEEN FR 53.8 AND FR 73 AND BETWEEN STR 18 AND STR 22 LH/RH, EXTERNAL SURFACE.

Threshold Interval

T

145 800 FH

T

24 200 CY

I

53 600 FH

I

8 100 CY

T

20 000 FC

I

2 200 CY

T

20 000 FC

I

6 900 CY

References

Ctrl

Eff

N

AMM 534100-210-844

275

N

AMM 534100-210-803

ALL

N

AMM 534100-220-823

ALL

Skills :

1.50 MHrs

1 AF 200

534124-01-2

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-02-2. Skills :

10.00 MHrs

1 AF D

200

534124-02-2

GVI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-01-2. Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [55 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534127-01-1

153 154 163 164

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 53.2 AND 73 BELOW CARGO COMPARTMENT FLOOR PANELS. NOTE : IF LDL INSTALLED, INSPECTION AREA BETWEEN FR 54A AND FR 73 TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : CARGO COMPARTMENT FLOOR PANELS INSULATION LD-MCR-IF INSTALLED NOTE:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 534100-200-812

ALL

N

AMM 534100-200-813

ALL

Access panels :


0.00 Hrs

Skills :

12.00 MHrs

1 AF 171 172

534128-01-1

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN FR 73 AND FR 80 BELOW CABIN FLOOR INCLUDING CABIN FLOOR STRUCTURE note:CPCP Access panels :

162AZ

822

Total access time :

0.00 Hrs

Skills :

6.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [56 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534132-01-1

100

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CRE DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE LH/RH PREP. : SCUFF PLATES BELOW Z833/Z843; note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 534100-200-807

ALL

N

AMM 534100-200-804

ALL

Skills :

2.00 MHrs

1 AF 271 272

534133-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR 4 (AFT PASSENGER/ CREW DOOR) BETWEEN FR 72 AND FR 77 FROM CABIN FLOOR LEVEL TO STR 9 LH/RH note:CPCP Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [57 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534134-01-1

171 172

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR 73 AND 76 FROM CABIN FLOOR LEVEL TO STR 30 LH/RH note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 534100-200-806

ALL

N

AMM 534100-200-808

ALL

Access panels :

162AZ

823

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 152

534138-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND 66, FROM STR 26 RH TO CARGO FLOOR LEVEL note:CPCP Access panels :


0.00 Hrs

Skills :

1.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [58 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

534140-01-1

152

Task Title

Task code

Threshold Interval

DI

T

6 YE

DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR59A AND FR65 note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00 THRESHOLD IS NEXT 4C CHECK FROM APPROVE DATE

I

6 YE

MAIN STRUCTURE

References

Ctrl

N

AMM 534100-200-802

Eff 275 943 946 962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AF 534140-01-1S100

152

DI

MAIN STRUCTURE DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR59A AND FR65 note:CPCP

T

24 YE

I

6 YE

N

AMM 534100-200-802

299 366

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 53 [59 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534145-01-1

162

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 66 AND 70 FROM STR 31 TO STR 48, RH note:CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 534100-200-803

ALL

N

AMM 534100-200-817

ALL

Check : C4

Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AF 162

534146-01-1

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR STOP FITTINGS AT 10 POSITIONS AT FR 67 AND 69 TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

T

6 YE

I

6 YE

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [60 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534148-01-3

200

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA CUT-OUT BETWEEN FR 56 AND FR 57 FROM STRINGERS 2 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

Threshold Interval

T

178 100 FH

T

26 300 CY

I

155 700 FH

I

23 900 CY

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 534100-210-849

275

N

AMM 534100-200-809

943

Skills :

0.20 MHrs

1 AF R

154

534156-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND FR 67, FROM CARGO FLOOR LEVEL TO STR 47 RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : BALL MATS Z150; CARGO FLOOR PANELS Z150; INSULATION Z150; note:CPCP

946 962 1019 1256 1266

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [61 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534158-01-1

151 152 161 162

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND CARGO COMPARTMENT FLOOR FROM FR 53.2 TO FR 73, INCLUDING MAIN DECK FLOOR STRUCTURE. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : CEILING PANELS Z150; INSULATION Z150; LDL (IF INSTALLED); LDMCR (IF INSTALLED); SIDEWALL LININGS Z150; NOTE:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 534100-200-818

Access panels :

822

823

Total access time :

0.00 Hrs

Skills :

6.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [62 / 74] ATA

: 53

Eff ALL


53

FUSELAGE

Task Number

Zone

534159-01-1

261 262 271 272

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND TOILETS AND GALLEYS FROM FR 53.5 TO FR 80 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE NOT INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS; GALLEYS; TOILLETS; NOTE: CPCP

Threshold Interval

T

5 YE

I

5 YE

References

Ctrl

N

AMM 534100-200-810 SIL 53-091

0.00 Hrs

Skills :

7.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294 366

843

Total access time :

275 299

Access panels :

833

Eff

Page : STR - 53 [63 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

534159-02-1

261 262 271 272

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW AND 0.75 M AROUND TOILETS AND GALLEYS FROM FR 53.5 TO FR 80 NOTE: - TASK APPLICABLE IF IMPROVEMENTS AS STATED IN NOTE 7 OF MPD STRUCTURE SECTION ARE NOT INCORPORATED - REFER TO SIL 53-091 FOR FURTHER INSTRUCTIONS TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : FLOOR PANELS; GALLEYS; TOILLETS; NOTE: CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 534100-210-865

962 1019 1256 1266

843

Total access time :

0.04 Hrs

Skills :

10.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943 946

Access panels :

833

Eff

Page : STR - 53 [64 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

534162-01-1

151 152 161 162 171 172

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE FROM MAIN DECK FLOOR TO CARGO COMPARTMENT FLOOR, BELOW AND 0.75 M FWD AND AFT OF UPPER DECK GALLEYS AND TOILETS, FROM FR 53.5 TO FR 80 LH/RH TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 PREP. : ACT IF INSTALLED; CARGO COMPARTMENT CEILING PANELS; LD-MCR-IF INSTALLED; LDL TOILETS AND FURNISHING-IF INSTALLED; LINING; NOTE 1;

Threshold Interval

T

6 YE

I

6 YE

T

34 000 CY

I

4 700 CY

References

Ctrl

Eff

N

AMM 534100-200-816

ALL

N

AMM 534100-220-807

275

Access panels :

822

823

Total access time :

0.00 Hrs

Skills :

3.00 MHrs

1 AF 150

534166-01-2

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF SKIN AROUND VHF2 ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 56 TO STR 57, RH. PREP. : VHF2 ANTENNA; Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [65 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

535101-01-1

270

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD FACE ABOVE CABIN FLOOR LEVEL INCLUDING FR 80/82, RIM ANGLE AND ATTACHMENT TO SKIN PREP. : INSULATION TOILETS AND GALLEYS note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; YE"

Threshold Interval

T

20 YE

I

12 YE

References

Ctrl

Eff

N

AMM 535100-200-808

275

N

AMM 535100-200-808

294

See note Check : NT

THRESHOLD IS "20

Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AF 535101-01-1S100

270

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD FACE ABOVE CABIN FLOOR LEVEL INCLUDING FR 80/82, RIM ANGLE AND ATTACHMENT TO SKIN PREP. : INSULATION TOILETS AND GALLEYS note:CPCP

T

20 YE

I

12 YE

299 366

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [66 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

535102-01-1

170

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD FACE BELOW CABIN FLOOR LEVEL INCLUDING FR 80/82, RIM ANGLE ATTACHMENT AND ATTACHMENT TO SKIN TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 535100-200-801

Eff 275 294 299 366

Access panels :


0.00 Hrs

Skills :

0.50 MHrs

1 AF 311 312

535103-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND CROWN CENTER LINE note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; YE"

T I

24 YE

N

AMM 535100-200-803

12 YE See note

Check : NT

THRESHOLD IS "24

Access panels :


0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [67 / 74] ATA

: 53

275


53

FUSELAGE

Task Number

Zone

535103-01-1S100

311 312

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND CROWN CENTER LINE note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 535100-200-803

Eff 294 299 366

Skills :

2.00 MHrs

1 AF 311 312

535104-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND BOTTOM CENTER LINE TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 note:CPCP

T

6 YE

I

6 YE

N

AMM 535100-200-802

294 299 366

Access panels :


0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 53 [68 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

535106-01-1

273 274

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN CENTER LINE AND TO FR 79 AND 80 TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : CEILING PANEL TOILETS AND GALLEYS NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

6 YE

References

Ctrl

Eff

N

AMM 535100-200-804

ALL

N

AMM 535100-200-812

ALL

Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF 311 312

535107-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FIN TO FUSELAGE MID AND AFT ATTACH FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN CENTER LINE AND TO FR 84, 85, 86 AND 87 note:CPCP Access panels :


0.00 Hrs

Skills :

4.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [69 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

535109-01-1

311 312

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE SUPPORT MEMBERS AND UPPER AND LOWER ATTACHMENT LUGS OF FR 91 LH/RH PREP. : HINGE ARMS

Threshold Interval

T

88 600 FH

T

14 800 CY

I

88 600 FH

I

14 800 CY

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 535100-200-811

ALL

N

AMM 535100-200-806

275

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 NDT R

311 312

535110-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF ATTACH FITTINGS FOR HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 86 AND 87 note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

943 946

See note

962

Check : NT

1019 1256 1266

Access panels :


0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [70 / 74] ATA

: 53


53

FUSELAGE

Task Number

Zone

535110-01-1S100

311 312

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF ATTACH FITTINGS FOR HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 86 AND 87 note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 535100-200-806

Eff 294 299 366

Skills :

0.50 MHrs

1 AF 311 312 313 314

535117-01-1

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF REAR FUSELAGE INTERNAL STRUCTURE BETWEEN FR 80/82 AND FR 95 FROM CROWN TO BOTTOM CENTER LINE, LH/RH NOTE: TPS APPLICATION IS FROM FR 80/82 TO FR 91 BELOW STRINGER 25 LH/RH, FROM FR 92 TO FR 95 BELOW STRINGER 13 LH/RH, AND AREA BETWEEN FR 86 AND FR 88 BELOW STR 15 TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 NOTE:CPCP

T

6 YE

I

6 YE

N

AMM 535100-200-817

Access panels :

312AR

313AL

Total access time :

0.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 53 [71 / 74] ATA

: 53

ALL


R

53

FUSELAGE

Task Number

Zone

535118-01-1

311 312

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR FUSELAGE INTERNAL STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT BETWEEN FR 86 AND FR 91 FROM STR 15 TO 30, AND FR 91 ASSEMBLY FROM CROWN TO BOTTOM CENTER LINE INCLUDING TAIL CONE ATTACHMENT FITTINGS, LH/RH . NOTE:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 535100-200-816

Eff 275 943 946 962 1019 1256 1266

THRESHOLD IS NEXT

Access panels :

312AR

313AL

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 535118-01-1S100

311 312

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR FUSELAGE INTERNAL STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT BETWEEN FR 86 AND FR 91 FROM STR 15 TO 30, AND FR 91 ASSEMBLY FROM CROWN TO BOTTOM CENTER LINE INCLUDING TAIL CONE ATTACHMENT FITTINGS, LH/RH . NOTE:CPCP

T

24 YE

I

6 YE

N

AMM 535100-200-816

299 366

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 53 [72 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

535124-01-1

310

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND BOTTOM CENTERLINE TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 535100-210-819

Eff 943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 535127-01-2

R

535127-01-3

Issue No

:

Date

:

311 312 313 314

MAIN STRUCTURE

311 312 313 314

MAIN STRUCTURE

10 01/12/2013

SDI

SPECIAL DETAILD INSPECTION (HFEC) OF THS SUPPORT STRUT ENDS (8X) AT FR 91. NOTE: - 24 MONTHS AFTER EFFECTIVE DATE OF EASA AD 2013-0076.

SPECIAL DETAILD INSPECTION (HFEC) OF THS SUPPORT STRUT ENDS (8X) AT FR 91. NOTE: - 36 MONTHS AFTER EFFECTIVE DATE OF EASA AD 2013-0076 OR SINCE FIRST FLIGHT, WHICHEVER OCCURS LATER.

Amendment No Date

: 01 : 06/09/2014

I

20 000 FH

I

42 MO

N

AMM 535100-220-801 EAD 2013-0076 ISB 53-3206

275 294 299 366

SDI

I

20 000 FH

I

42 MO

N

AMM 535100-220-801 EAD 2013-0076 ISB 53-3206

943 946 962 1019 1256 1266

Page : STR - 53 [73 / 74] ATA

: 53


R

53

FUSELAGE

Task Number

Zone

535129-01-1

270

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD FACE ATTACHMENT TO RIM ANGLE, ABOVE CABIN FLOOR LEVEL, INCLUDING FR80 AND ATTACHMENT TO SKIN PREP. : NOTE 1; TOILETS AND GALLEYS;

R

170

535130-01-1

310

535131-01-1

DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND CROWN CENTER LINE PREP. : IF LDF (PARTIAL OR FULL BULK) INSTALLED: 833 843 161AZ;

I

12 YE

N

AMM 535100-210-820

946

1266

T

6 YE

I

6 YE

N

AMM 535100-210-821

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

962 1019 1256 1266

T

12 YE

I

12 YE

N

AMM 535100-210-822

943 946 962 1019 1256 1266

0.00 MHrs

: 01 : 06/09/2014

943 946

Skills :

1 AF

943

1256

DI

MAIN STRUCTURE

12 YE

Eff

962

DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD FACE ATTACHMENT TO RIM ANGLE, BELOW MAIN DECK FLOOR LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN TPS : APPLICATION OF TPS TYPE 1 PLUS A SUBSEQUENT APPLICATION OF TPS TYPE 2 R

T

References

Ctrl

1019

DI

MAIN STRUCTURE

Threshold Interval

Page : STR - 53 [74 / 74] ATA

: 53


54

NACELLES / PYLONS

Task Number

Zone

545101-02-1

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH THE FWD ENGINE MOUNT FITTING, HOLES AND SPOTFACES. TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE; note:CPCP NOTE: RII TASK

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 545118-200-815

Eff 275 294 299 366

Skills :

0.80 MHrs

1 EN R

453 463

545101-02-2

DI

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH THE FWD ENGINE MOUNT FITTING, HOLES AND SPOTFACES. TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE; NOTE: CPCP NOTE: RII TASK

T

12 YE

I

12 YE

N

AMM 545118-200-815

946 962 1019 1256 1266

Skills :

0.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 54 [1 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545102-05-1

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT RIB 8C TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE note:CPCP NOTE: RII TASK

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 545118-200-817

ALL

N

AMM 545100-250-804

943

Check : C8

Skills :

0.80 MHrs

1 EN R

545104-02-20

453 463

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON PYRAMID ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB2 (2 FASTENER LOCATION/PYLON)

T

60 000 FH

T

17 000 CY

I

91 000 FH

962

14 000 CY

1019

I

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [2 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545106-01-2

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE TPS : TPS MUST NOT BE APPLIED note:CPCP NOTE: MSN 275 THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-922

Eff 275 943 946 962 1019 1256 1266

Access panels :

415AL 426BR

415BL

Total access time :

416AR

416BR

425AL

425BL

426AR

0.00 Hrs

Skills :

0.60 MHrs

1 AF 545106-01-2S100

453 463

DI

PYLON BOX DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE TPS : TPS MUST NOT BE APPLIED note:CPCP

T

24 YE

I

6 YE

N

AMM 545100-200-922

299 366

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [3 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545108-04-2

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 TPS : TPS MUST NOT BE APPLIED note:CPCP

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-919

415BL

Total access time :

416AR

416BR

425AL

425BL

299 366

426AR

0.00 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275 294

Access panels :

415AL 426BR

Eff

Page : STR - 54 [4 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545110-03-1

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT UPPER BEAM AT RIB 8C. TPS : TPS MUST NOT BE APPLIED "NOTE: MSN 275THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

174 600 FH

T

25 800 CY

T

12 YE

I

174 600 FH

I

25 800 CY

I

References

Ctrl

N

AMM 545118-200-827

12 YE See note


415AL 418CR 428BR

415BL 425AL 428CR

Total access time :

416AR 425BL

416BR 426AR

417AL 426BR

418AR 427AL

418BR 428AR

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [5 / 21] ATA

: 54

Eff ALL


R

54

NACELLES / PYLONS

Task Number

Zone

545118-02-2

453 463

Task code

Task Title

DI

PYLON LOWER SPAR DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 AND RIB 10) TPS : TPS MUST NOT BE APPLIED note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 545100-200-895

Eff 275 943 946 962 1019 1256 1266

Access panels :

415AL 425BL

415BL 426AR

Total access time :

416AR 426BR

416BR 427AL

417AL 428AR

418AR

425AL

0.00 Hrs

Skills :

0.60 MHrs

1 AF 545118-02-2S100

453 463

DI

PYLON LOWER SPAR DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 AND RIB 10) TPS : TPS MUST NOT BE APPLIED note:CPCP

T

24 YE

I

12 YE

N

AMM 545100-200-895

299 366

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [6 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545119-01-2

453 463

Task code

Task Title

DI

PYLON LOWER SPAR DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) AND RIB 18A TPS : TPS MUST NOT BE APPLIED note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 545100-200-902

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

415AL 425BL

415BL 426AR

Total access time :

545119-01-2S100

Issue No

:

Date

:

453 463

10 01/12/2013

416AR 426BR

416BR 427AL

417AL 428AR

418AR 454AL

0.00 Hrs

PYLON LOWER SPAR DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) AND RIB 18A TPS : TPS MUST NOT BE APPLIED note:CPCP

Amendment No Date

425AL 464AL

: 01 : 06/09/2014

DI

T

24 YE

I

12 YE

N

AMM 545100-200-902

294 299 366

Page : STR - 54 [7 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545121-02-1

453 463

Task code

Task Title

DI

PYLON UPPER SPAR DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER SURFACE, BETWEEN RIB 1 AND RIB 10A EXCLUDING PRECOOLER AREA TPS : TPS MUST NOT BE APPLIED note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

6 YE

References

Ctrl

Eff

N

AMM 545100-200-903

ALL

N

AMM 545100-200-904

275

Access panels :

451CL 452CL 462BL

451CR 452CR 462BR

Total access time :

451DL 461CL 462CL

451DR 461CR 462CR

452AL 461DL

452BL 461DR

452BR 462AL

0.00 Hrs

Skills :

0.00 MHrs

1 AF R

453 463

545122-01-2

DI

PYLON UPPER SPAR DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8 TPS : TPS MUST NOT BE APPLIED PREP. : AIR DUCT PRE-COOLER NOTE:CPCP NOTE: TASK REPLACE TASK 545122-01-5

943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [8 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545122-01-2S100

453 463

Task code

Task Title

DI

PYLON UPPER SPAR DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8 TPS : TPS MUST NOT BE APPLIED PREP. : AIR DUCT PRE-COOLER NOTE:CPCP

Threshold Interval

T

24 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-904

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 453 463

545124-02-2

DI

PYLON UPPER SPAR DETAILED INSPECTION OF PYLON UPPER SPAR UPPER SURFACE, BETWEEN RIB 10A AND RIB 15A

T

12 YE

I

12 YE

N

AMM 545100-200-892

Access panels :

452CL 464BR

454BL 464CL

Total access time :

454BR 464NR

454CL

454NR

462CL

464BL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [9 / 21] ATA

: 54

ALL


R

54

NACELLES / PYLONS

Task Number

Zone

545126-02-2

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 545100-200-893

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

454KL

454KR

Total access time :

464KL 464KR 0.00 Hrs

Skills :

0.00 MHrs

1 AF R

545126-02-2S100

453 463

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A

T

24 YE

I

12 YE

N

AMM 545100-200-893

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [10 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545128-01-2

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 TPS : TPS MUST NOT BE APPLIED PREP. : BEARING note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"" "

Threshold Interval

T

10 YE

I

10 YE

References

Ctrl

N

AMM 545100-200-894

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

454BL

454BR

Total access time :

464BL 464BR 0.00 Hrs

Skills :

0.00 MHrs

1 AF 545128-01-2S100

453 463

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 TPS : TPS MUST NOT BE APPLIED PREP. : BEARING note:CPCP

T

20 YE

I

10 YE

N

AMM 545100-200-894

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [11 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545137-01-2

453 463

Task code

Task Title

DI

PYLON LATERAL PANELS DETAILED INSPECTION OF PYLON, LATERAL PANELS, EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND CORE COWLS TPS : TPS MUST NOT BE APPLIED note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

T

24 YE

I

6 YE

References

Ctrl

Eff

N

AMM 545100-200-905

275

N

AMM 545100-200-905

294

THRESHOLD IS NEXT

Access panels :

415AL

415BL

Total access time :

545137-01-2S100

453 463

400

545138-01-6

416AR 416BR 0.00 Hrs

417AL

418AR

DI

PYLON LATERAL PANELS DETAILED INSPECTION OF PYLON, LATERAL PANELS, EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND CORE COWLS TPS : TPS MUST NOT BE APPLIED note:CPCP

366

DI

PYLON BOX DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS DOORS BETWEEN RIB 10 AND RIB 11

299

T

154 000 FH

T

23 700 CY

I

66 300 FH

I

10 200 CY

N

AMM 545100-200-913

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [12 / 21] ATA

: 54

275


D

54

NACELLES / PYLONS

Task Number

Zone

545139-02-7

400

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS BETWEEN RIB 13 AND RIB 14 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545139-03-7

400

545139-03-7

DI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS BETWEEN RIB 13 AND RIB 14 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545139-02-7

453 463

545143-02-1

DI

PYLON BOX DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11

Threshold Interval

T

156 300 FH

T

24 000 CY

I

35 100 FH

I

5 400 CY See note

T

156 300 FH

T

24 000 CY

I

130 000 FH

I

20 000 CY

T

186 800 FH

T

27 600 CY

I

41 200 FH

I

6 100 CY

References

Ctrl

N

AMM 545100-200-925 MRB 545139-02-7

275

N

AMM 545100-270-803 MRB 545139-03-7

275

N

AMM 545100-200-916

275

Access panels :

453BL

453BR

Total access time :

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

463BL

463BR

0.00 Hrs

: 01 : 06/09/2014

Eff

Page : STR - 54 [13 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545146-03-5S020

453 463

Task Title

Task code

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - HIGH FREQUENCY EDDY CURRENT INSPECTION - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-5S020 PREP. : AIR DUCT PRE-COOLER RODS

Threshold Interval

References

Ctrl

N

AMM 545100-250-808

Eff 943

T

118 900 FH

T

18 300 CY

I

68 900 FH

962

10 600 CY

1019

I

946

1256 1266

Skills :

1.00 MHrs

1 NDT R

545146-04-5S020

453 463

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 NOTE: - INSPECTION THROUGH FLEXIBLE BOROSCOPE - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-5S020 PREP. : AIR DUCT; PRE-COOLER; RODS;

N

AMM 545100-200-917

118 900 FH

T

18 300 CY

I

37 000 FH

962

I

5 700 CY

1019

946

1256 1266

Skills :

1.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

T

Page : STR - 54 [14 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545150-02-7S020

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 PREP. : AIR DUCT PRE-COOLER RODS

Threshold Interval

References

Ctrl

N

AMM 545100-200-918

Eff 943

T

108 200 FH

T

16 600 CY

I

65 000 FH

962

10 000 CY

1019

I

946

1256 1266

Access panels :

452AL

462AL

Total access time :

0.60 Hrs

Skills :

0.20 MHrs

1 AF 453 463

545154-01-1

DI

PYLON BOX DETAILED INSPECTION OF PYLON, RIB 18A ASSEMBLY, AFT FACE note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; YE"

T

20 YE

I

12 YE

N

AMM 545100-200-897

See note Check : NT THRESHOLD IS "20

Access panels :

454EL

454ER

Total access time :

464EL

464ER

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [15 / 21] ATA

: 54

275


54

NACELLES / PYLONS

Task Number

Zone

545154-01-1S100

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, RIB 18A ASSEMBLY, AFT FACE note:CPCP

Threshold Interval

T

24 YE

I

12 YE

T

12 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-897

Eff 294 299

Skills :

0.00 MHrs

1 AF R

453 463

545158-01-2

SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD FACE TPS : TPS MUST NOT BE APPLIED note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

N

AMM 545100-200-907

275 943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Access panels :

415BL 428AR

416BR 453AZ

Total access time :

545158-01-2S100

453 463

417AL 463AZ

418AR

425BL

426BR

427AL

0.00 Hrs SDI

PYLON BOX SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD FACE TPS : TPS MUST NOT BE APPLIED note:CPCP

T

24 YE

I

6 YE

N

AMM 545100-200-907

299 366

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [16 / 21] ATA

: 54


R

54

NACELLES / PYLONS

Task Number

Zone

545160-01-1

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 3 AFT FACE AND RIB 8 FORWARD FACE TPS : TPS MUST NOT BE APPLIED PREP. : AIR DUCT; PRE-COOLER; RODS; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-908

Eff 275 943 946 962 1019 1256 1266

THRESHOLD IS NEXT

Access panels :

452AL

452BL

Total access time :

452BR 462AL 0.00 Hrs

462BL

462BR

Skills :

0.00 MHrs

1 AF 545160-01-1S100

453 463

DI

PYLON BOX DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 3 AFT FACE AND RIB 8 FORWARD FACE TPS : TPS MUST NOT BE APPLIED PREP. : AIR DUCT; PRE-COOLER; RODS; note:CPCP

T

24 YE

I

6 YE

N

AMM 545100-200-908

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 54 [17 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545162-01-1

453 463

Task Title

Task code

DI

PYLON BOX DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 8 AFT FACE AND RIB 12 FORWARD FACE TPS : TPS MUST NOT BE APPLIED note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

6 YE

References

Ctrl

Eff

N

AMM 545100-200-909

ALL

N

AMM 545100-200-910

275

Access panels :

453BL

453BR

Total access time :

463BL 463BR 0.00 Hrs

Skills :

0.00 MHrs

1 AF R

453 463

545164-01-1

DI

PYLON BOX DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 12 AFT FACE AND RIB 18A FORWARD FACE note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

943 946 962 1019

THRESHOLD IS NEXT

1256 1266

Access panels :

453CL

453CR

Total access time :

463CL 463CR 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [18 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545164-01-1S100

453 463

Task code

Task Title

DI

PYLON BOX DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE BETWEEN RIB 12 AFT FACE AND RIB 18A FORWARD FACE note:CPCP

Threshold Interval

T

24 YE

I

6 YE

References

Ctrl

N

AMM 545100-200-910

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 454 464

545170-02-1

DI

PYLON TO WING LINKS DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES, LINKS AND BOLTS AT RIB 12 (4 PLACES PER PYLON) note:CPCP NOTE: RII TASK

T

12 YE

I

12 YE

N

AMM 545117-200-814

Access panels :

452CL 464BR

452CR

Total access time :

454BL

454BR

462CL

462CR

464BL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [19 / 21] ATA

: 54

ALL


54

NACELLES / PYLONS

Task Number

Zone

545174-04-1

454 464

Task code

Task Title

DI

PYLON TO WING FITTING DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING AND LINKS AT RIB 18A TPS : TPS MUST NOT BE APPLIED PREP. : BEARING ENGINE LINKS POST 43271 (ACCESS WITH SUFFIX KL, KR, ML,MR) PRE 43271 (ACCESS WITH SUFFIX DL, DR, FL, FR) note:CPCP NOTE: RII TASK

Threshold Interval

T

10 YE

I

10 YE

References

Ctrl

N

AMM 545117-200-813

Eff 275 294 299 366

Access panels :

454KL 464MR

454KR

Total access time :

R

454

545174-04-2

454ML

454MR

464KL

464KR

0.00 Hrs

PYLON TO WING FITTING DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE; PYLON TO WING AFT ATTACH FITTING; NOTE: CPCP NOTE: RII TASK

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

464ML

: 01 : 06/09/2014

DI

T

12 YE

I

12 YE

N

AMM 545117-200-813

943 946 962 1019 1256 1266

Page : STR - 54 [20 / 21] ATA

: 54


54

NACELLES / PYLONS

Task Number

Zone

545180-03-2

454 464

Task code

Task Title

DI

PYLON TO WING FITTING DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) TPS : TPS MUST NOT BE APPLIED PREP. : ENGINE; PYLON TO WING AFT ATTACH FITTING; NOTE: CPCP NOTE: RII TASK

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 545117-200-818

Access panels :

454KL 464MR

454KR

Total access time :

454ML

454MR

464KL

464KR

464ML

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 54 [21 / 21] ATA

: 54

Eff ALL


R

55

STABILIZERS

Task Number

Zone

551001-01-1

311 312

Task Title

Task code

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER, ASSEMBLY OF TRIM ACTUATING ARMS, SUPPORT FITTINGS AND UPPER AND LOWER ATTACHMENT PLATES note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 551634-200-801

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 AF 551001-01-1S100

311 312

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER, ASSEMBLY OF TRIM ACTUATING ARMS, SUPPORT FITTINGS AND UPPER AND LOWER ATTACHMENT PLATES note:CPCP

T

24 YE

I

12 YE

N

AMM 551634-200-801

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 55 [1 / 16] ATA

: 55


R

55

STABILIZERS

Task Number

Zone

551004-01-1

311 312

Task Title

Task code

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER, ASSEMBLY OF HINGE FITTING AT RIB 3, UPPER AND LOWER ATTACH FITTINGS, LH/RH note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 551638-200-801

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 AF 551004-01-1S100

311 312

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER, ASSEMBLY OF HINGE FITTING AT RIB 3, UPPER AND LOWER ATTACH FITTINGS, LH/RH note:CPCP

T

24 YE

I

12 YE

N

AMM 551638-200-801

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 55 [2 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

551008-01-3

311 312

Task Title

Task code

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES

Threshold Interval

References

Ctrl

Eff

N

AMM 551100-200-805

275

N

AMM 551100-200-805

943

T

60 000 FH

T

20 000 CY

I

37 900 FH

I

5 600 CY

T

60 000 FH

T

17 000 CY

I

29 900 FH

962

4 400 CY

1019

Access panels :

312AR

313AL

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF R

311 312

551008-01-9

HORIZONTAL STABILIZER

DI

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES

I

946

1256 1266

333 343

551009-01-6

Issue No

:

Date

:

10 01/12/2013

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, LH/RH PREP. : REARMOST UPPER FAIRING SUPPORT FITTING; NOTE: THRESHOLD IS NEXT 4C CHECK

Amendment No Date

: 01 : 06/09/2014

SDI

T

60 000 FH

T

20 000 CY

I

18 600 FH

N

AMM 551100-200-806

I


Page : STR - 55 [3 / 16] ATA

: 55

275


R

R

55

STABILIZERS

Task Number

Zone

551009-01-7

333 343

311 312

551011-01-1

Task Title

Task code

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, LH/RH PREP. : REARMOST UPPER FAIRING SUPPORT FITTING;

References

Ctrl

N

AMM 551100-200-806

Eff 943

T

60 000 FH

T

17 000 CY

I

22 600 FH

962

3 400 CY

1019

I

946

1256 1266

DI


Threshold Interval

DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR SPAR AFT FACE JOINT PLATE INBOARD OF RIB 3, LH/RH note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE OR OR ""NEXT 20000 FC"" FROM APPROVE DATE"

T

12 YE

I

12 YE

N

AMM 551638-200-802

275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 AF R

551011-01-1S100

311 312

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR SPAR AFT FACE JOINT PLATE INBOARD OF RIB 3, LH/RH note:CPCP

T

24 YE

I

12 YE

N

AMM 551638-200-802

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 55 [4 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

551013-01-1

311 312 334 344

Task Title

Task code

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, LH/RH note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

60 000 FH

T

20 000 CY

I

60 000 FH

I

20 000 CY

References

Ctrl

Eff

N

AMM 551100-200-801

ALL

N

AMM 551100-200-808

275

Access panels :

313AL

334AB

Total access time :

344AB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 311 312

551016-01-2

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [5 / 16] ATA

: 55


R

55

STABILIZERS

Task Number

Zone

551016-01-4S020

311 312

Task Title

Task code

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE IN THE AREA OF ATTACHMENT TO JOIN PLATE OUTBOARD OF RIB 3, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 551100-200-808

Eff 943

T

60 000 FH

T

17 000 CY

I

104 600 FH

962

15 400 CY

1019

I

946

1256 1266

Access panels :


0.03 Hrs

Skills :

0.20 MHrs

1 NDT 311 312

551019-01-2

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO REAR SPAR WEB FROM RIB 3LH TO RIB 3RH

T

60 000 FH

T

20 000 CY

I

21 100 FH

I

6 400 CY

N

ALI 551019-01-04 AMM 551100-200-809

Access panels :


0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [6 / 16] ATA

: 55

275


55

STABILIZERS

Task Number

Zone

551022-01-1

333 343

Task code

Task Title

DI

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 3 AND RIB 4 TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

Threshold Interval

References

Ctrl

Eff

N

AMM 551100-200-802

ALL

N

AMM 551100-200-817

ALL

N

AMM 551100-200-812

943

T

12 YE

I

12 YE

T

3 YE

I

3 YE

T

60 000 FH

T

17 000 CY

I

25 600 FH

962

3 900 CY

1019

Access panels :

331AT 343AB

331BT 343AR

Total access time :

333AB 343AT

333AL

333AT

341AT

341BT

0.00 Hrs

Skills :

0.00 MHrs

1 AF 300

551027-01-2

GVI

HORIZONTAL STABILIZER GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX BOTTOM SKIN LOWER SURFACE FROM CHORDWISE SPLICE LINE TO END RIB Skills :

0.00 MHrs

1 AF R

333 343

551028-02-4

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE FAIRINGS

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [7 / 16] ATA

: 55


R

55

STABILIZERS

Task Number

Zone

551028-02-8

333 343

319

551029-02-4

Task code

Task Title

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE FAIRINGS NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-8 NOTE: THRESHOLD IS NEXT 4C CHECK

SDI

HORIZONTAL STABILIZER SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO FRONT SPAR WEB FROM RIB 3LH TO RIB 3RH NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 551029-01-3 PREP. : DISCONNECT SCAVENGE WATER PIPE

Threshold Interval

T

60 000 FH

T

20 000 CY

I

29 200 FH

I

8 300 CY

T

20 000 FC

I

20 000 CY

References

Ctrl

Eff

N

AMM 551100-200-812

275

N

AMM 551100-200-814

275 943 946 962 1019 1256 1266

Access panels :

312AR

319AL

Total access time :

319AR 319BL 0.00 Hrs

319DR

319ER

Skills :

0.00 MHrs

1 NDT 334 344

551031-01-2

Issue No

:

Date

:

10 01/12/2013

HORIZONTAL STABILIZER DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE FITTINGS NO 2 AND 3 AND SUPPORT RIBS note:CPCP

Amendment No Date

: 01 : 06/09/2014

DI

T

6 YE

I

6 YE

N

AMM 551600-200-801

Page : STR - 55 [8 / 16] ATA

: 55

ALL


55

STABILIZERS

Task Number

Zone

551032-01-2

334 344


334 344


333 343


551033-01-2

551035-04-1

Task Title

Task code

DI

DETAILED INSPECTION OF HORIZONTAL STABILIZER ACTUATOR ATTACHMENT FITTING, REACTION BAR AND ACTUATOR PLATE AT RIBS 8 AND 9, LH AND RH. note:CPCP DI

DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE FITTINGS NO 1,4,5,6 AND 7 AND SUPPORT RIBS note:CPCP

SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END RIB LH / RH PREP. : FUEL TANK DRAINED AND VENTED; PEELABLE HOLE COVERS;

SDI

Threshold Interval

T

6 YE

I

6 YE

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 551600-200-802

ALL

N

AMM 551600-200-803

ALL

N

AMM 551100-200-803

275 294 299 366 943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [9 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

551036-01-1

334 344

Task Title


Task code

DI

DETAILED INSPECTION OF HORIZONTAL STABILIZER, BOX LATERAL LOAD FITTING AT RIB 4, LH/RH.

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 551600-200-811

Eff 275 294 299 366 943 946 962 1019 1256 1266

334 344

551037-01-1


DI

DETAILED INSPECTION OF HORIZONTAL STABILIZER, ELEVATOR LATERAL LOAD FITTING AT REAR SPAR, LH/RH.

T

12 YE

I

12 YE

N

AMM 551600-200-812

275 294 299 366 943 946 962 1019 1256 1266

335 345

552002-01-2

Issue No

:

Date

:

10 01/12/2013

DI

ELEVATORS DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO 2 AND 3 AND ACTUATOR FITTINGS note:CPCP

Amendment No Date

: 01 : 06/09/2014

T

6 YE

I

6 YE

N

AMM 552600-200-801

Page : STR - 55 [10 / 16] ATA

: 55

ALL


55

STABILIZERS

Task Number

Zone

552003-01-1

335 345

Task code

Task Title

DI

ELEVATORS DETAILED INSPECTION OF ELEVATOR SPAR FORWARD FACE

Threshold Interval

T

12 YE

I

12 YE

T

6 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 552000-200-801

ALL

N

AMM 552000-200-802

ALL

N

AMM 552600-200-802

ALL

Access panels :

334AB 335AB 344BB 345BB

334BB 335BB 344CB 345CB

Total access time :

334CB 335CB 344DB 345DB

334DB 335DB 344EB 345EB

334EB 335EB 344FB 345FB

334FB 335FB 344GB

334GB 344AB 345AB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 300

552004-01-1

SDI

ELEVATORS SPECIAL DETAILED INSPECTION OF ELEVATOR TOP AND BOTTOM SKIN PANELS IN AREA OF HINGE FITTINGS NO 2 AND 3 AND AREA OF ACTUATOR FITTINGS, EXTERNAL SURFACE Skills :

0.00 MHrs

1 NDT 335 345

552005-01-2

Issue No

:

Date

:

10 01/12/2013

DI

ELEVATORS DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO 1,4,5,6 AND 7 note:CPCP

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [11 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

552007-01-2

335 345

Task Title

Task code

SDI

ELEVATOR SPECIAL DETAILED INSPECTION OF ELEVATOR, TOP AND BOTTOM SKIN PANELS, EXCLUDING AREAS FROM ELEVATOR SPAR TO 440 MM BACKWARDS AND FROM ELEVATOR RIB 4 TO RIB 5, L/H R/H. NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT OR 24 MONTHS SINCE THE ISSUANCE DATE OF THE ISB 55-3039, WHICHEVER OCCURS LATER. NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 552007-02-2.

Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

6 YE

References

Ctrl

Eff

N

AMM EAD FAD ISB

552000-220-801 2009-0255 2011-03-10 55-3039

ALL

N

AMM EAD FAD ISB

552000-220-803 2009-0255 2011-03-10 55-3039

ALL

Skills :

0.00 MHrs

1 NDT D

335 345

552007-02-2

SDI

ELEVATOR SPECIAL DETAILED INSPECTION OF ELEVATOR, TOP AND BOTTOM SKIN PANELS, EXCLUDING AREAS FROM ELEVATOR SPAR TO 440 MM BACKWARDS AND FROM ELEVATOR RIB 4 TO RIB 5, L/H R/H. NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT OR 24 MONTHS SINCE THE ISSUANCE DATE OF THE ISB 55-3039, WHICHEVER OCCURS LATER. NOTE: THIS TASK IS AN ALTERNATIVE TO THE TASK 552007-01-2. PREP. : ELEVATOR REMOVAL; Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [12 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

552008-01-2

335 345

Task Title

Task code

SDI

ELEVATOR SPECIAL DETAILED INSPECTION OF ELEVATOR TOP AND BOTTOM SKIN PANELS INNER SURFACE FROM ELEVATOR SPAR TO 440 MM BACKWARDS AND FROM ELEVATOR RIB 4 TO RIB 5, LH/RH. NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT OR 24 MONTHS SINCE THE ISSUANCE DATE OF THE ISB 55-3039, WHICHEVER OCCURS LATER. PREP. : PEELABLE HOLE COVERS;

Threshold Interval

T

12 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM EAD FAD ISB

552000-220-802 2009-0255 2011-03-10 55-3039

ALL

N

AMM 553000-210-805

943

Skills :

0.00 MHrs

1 NDT R

323

553024-01-2

DI

VERTICAL STABILIZER DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS.

946 962 1019 1256 1266

Access panels :

311AZ

312AR

Total access time :

323DL

323EL

325LL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [13 / 16] ATA

: 55


55

STABILIZERS

Task Number

Zone

553026-01-1

325

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR SUPPORT FITTINGS. NOTE: CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 553000-210-806

Eff 275 294 299 366

Skills :

0.00 MHrs

1 AF R

325

553026-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR SUPPORT FITTINGS.

T

6 YE

I

6 YE

N

AMM 553000-210-806

943 946 962 1019 1256 1266

Access panels :

325LL 326NL

325NL 326PL

Total access time :

325SL 325TL 326RL 326SL 0.00 Hrs

325UL

325VL

326ML

Skills :

0.00 MHrs

1 AF 326

554021-01-1

DI

RUDDER DETAILED INSPECTION OF RUDDER FRONT SPAR. PREP. : PEELABLE HOLE COVERS;

T

12 YE

I

6 YE

N

AMM 554000-210-804

294 299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 55 [14 / 16] ATA

: 55


R

55

STABILIZERS

Task Number

Zone

554021-01-2

326

Task Title

Task code

DI

RUDDER DETAILED INSPECTION OF RUDDER FRONT SPAR. PREP. : PEELABLE HOLE COVERS;

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 554000-210-804

Eff 943 946 962 1019 1256 1266

326

554023-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF RUDDER HINGE FITTINGS. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 NOTE: CPCP

T

6 YE

I

6 YE

N

AMT 554600-210-803

275 294 299 366

Skills :

0.00 MHrs

1 AF R

326

554023-01-2

DI

MAIN STRUCTURE DETAILED INSPECTION OF RUDDER HINGE FITTINGS. TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 NOTE: CPCP

T

6 YE

I

6 YE

N

AMT 554600-210-803

943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 326

554024-01-1

SDI

RUDDER SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN BOOSTER AREA, LH/RH.

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

T

12 YE

I

6 YE

N

AMM 554000-270-808

Page : STR - 55 [15 / 16] ATA

: 55

ALL


55

STABILIZERS

Task Number

Zone

554025-01-1

326

Task Title

Task code

SDI

RUDDER SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN AREA OF FRONT SPAR AND RIB 0.

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

T

12 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 554000-280-805

ALL

N

AMM 554000-270-801

ALL

N

AMM 554000-270-802

ALL

N

AMM 554000-280-804

ALL

Skills :

0.00 MHrs

1 NDT 326

554026-01-1

SDI

RUDDER SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN AREA OF HOISTING POINTS AND TRAILING EDGE SCREW LINE, LH/RH. Skills :

0.00 MHrs

1 NDT 326

554027-01-1

SDI

RUDDER SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN ATTACH FITTING AREA, LH/RH.

326

554028-01-1

SDI

RUDDER SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL INTERNAL STRUCTURE, LH/RH. Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 55 [16 / 16] ATA

: 55


56

WINDOWS

Task Number

Zone

562101-01-2

221 222 231 232 241 242 251 252 261 262 271 272

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF PASSENGER CABIN WINDOW PANES INCLUDING PASSENGER/CREW DOOR AND EMERGENCY EXIT WINDOW PANES

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 562115-200-801

Access panels :

830

840

Total access time :

0.00 Hrs

Skills :

9.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 56 [1 / 1] ATA

: 56

Eff ALL


57

WINGS

Task Number

Zone

571104-01-7

130 190

130 190

571104-01-8

Issue No

:

Date

:

10 01/12/2013

Task Title

MAIN STRUCTURE

Task code

SDI

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENERS BETWEEN STR 38 AND 39, LH/RH. NOTE: - FOR THRESHOLD AND INTERVAL REFER TO ISB 57-3116.

Amendment No Date

: 01 : 06/09/2014

Ctrl

See note

N

Check : NT

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENERS BETWEEN STR 38 AND 39, LH/RH. NOTE: - FOR THRESHOLD AND INTERVAL REFER TO ISB 57-3115. MAIN STRUCTURE

Threshold Interval

References

AMM 571100-250-810 ISB 57-3115

Eff 275 294 299 366

SDI

N

AMM 571100-250-810 ISB 57-3116

275

T

101 400 FH

T

15 600 FC

I

31 500 FH

299


366

I

Page : STR - 57 [1 / 188] ATA

: 57

294


57

WINGS

Task Number

Zone

571105-01-1

143 190

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN LOWER SURFACE FROM FR 40 TO FR 47 BETWEEN RIB 1 LH AND RIB 1 RH TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : AIR CONDITIONING PACKS; FAIRING PANELS BETWEEN FR 40 AND FR 47; HEATSHIELDS; NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 571100-200-801

ALL

N

AMM 571100-200-809

ALL

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.50 MHrs

1 AF 191 192 195 196

571106-01-1

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER SPLICE AT RIB 1 BETWEEN FR 40 AND FR 47 note:CPCP Access panels :

191HB

191QB

Total access time :

192HB 192QB 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [2 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

571107-01-5S020

195 196

Task Title

Task code

SDI


Threshold Interval

References

Ctrl

N

AMM 571100-200-830

Eff 943

T

83 000 FH

T

12 700 CY

I

29 000 FH

962

4 450 CY

1019

I

946

1256 1266

Access panels :

191QB

192QB

Total access time :

5.56 Hrs

Skills :

0.40 MHrs

1 NDT R

571108-01-9S020

141 142

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. PREP. : FUEL TANK DRAINED AND VENTED;

N

AMM 571100-200-813

943

T

91 600 FH

T

14 100 CY

I

41 100 FH

962

6 300 CY

1019

I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734

744

1.08 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [3 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

571116-01-5S020

193

Task Title

Task code

SDI


Threshold Interval

References

Ctrl

N

AMM 571100-200-834

Eff 943

T

83 000 FH

T

12 700 CY

I

29 000 FH

962

4 450 CY

1019

I

946

1256 1266

Access panels :

193DB Total access time :

2.18 Hrs

Skills :

0.20 MHrs

1 NDT R

571118-01-9S020

143 195

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEEN STRINGERS 27 & 28..

N

AMM 571100-200-833

943

T

83 000 FH

T

12 700 CY

I

29 000 FH

962

4 450 CY

1019

I

946

1256 1266

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [4 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571122-01-5

195 196

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO Y=1959, LH/RH.

Threshold Interval

References

Ctrl

Eff

N

AMM 571100-200-819

275

N

AMM 571100-200-819

943

T

79 900 FH

T

22 800 FC

I

22 700 FH

I

6 500 CY See note

T

112 500 FH

T

17 300 CY

I

33 600 FH

962

5 150 CY

1019

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

571122-01-8S020

195 196

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO Y=1959, LH/RH.

I

946

1256 1266

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.60 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [5 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

571125-01-7S020

147 148

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND FRAME 47 LOWER CORNER FITTING, LH/RH.

Threshold Interval

References

Ctrl

N

AMM 571100-200-825

Eff 943

T

103 000 FH

T

15 800 CY

I

21 700 FH

962

3 300 CY

1019

I

946

1256 1266

Skills :

0.50 MHrs

1 NDT R

147

571126-01-6

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER.

N

AMM 571100-200-826

943

T

155 000 FH

T

23 800 CY

I

59 800 FH

962

9 200 CY

1019

I

946

1256 1266

141 142

571129-01-5

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES). PREP. : FUEL TANK DRAINED AND VENTED;

T

113 700 FH

T

17 500 CY

I

111 800 FH

I

17 200 CY

N

AMM 571100-200-814

Access panels :

147AZ

148AZ

Total access time :

734 744 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [6 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

571129-01-6S020

141 142

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR 30MM AROUND ACCESS CUT-OUTS (2 PLACES). PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 571100-200-814

Eff 943

T

117 000 FH

T

18 000 CY

I

117 100 FH

962

18 000 CY

1019

I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734

744

1.08 Hrs

Skills :

0.00 MHrs

1 AF R

141 142 147 148

571130-01-6

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES).

SDI

N

AMM 571100-200-827

943

T

130 800 FH

T

20 000 CY

I

50 800 FH

962

7 800 CY

1019

I

946

1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [7 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571131-01-1

147 148

Task Title

Task code

GVI

MAIN STRUCTURE GENERAL VISUAL INSPECTION OF CENTER WING BOX, REAR SPAR, AFT FACE note:CPCP

Threshold Interval

References

Ctrl

Eff

N

AMM 571100-200-810

ALL

N

AMM 571100-200-815

943

T

6 YE

I

6 YE

T

78 800 FH

T

17 000 CY

I

78 800 FH

962

12 100 CY

1019

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF R

571133-01-5S020

141 142

DI


I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734

744

1.08 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [8 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571137-01-4

191 192

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM AT FR.40, LH/RH. "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT ""0500 FC OR 36000 FH" FROM APPROVE DATE"

Threshold Interval

T

60 000 FH

T

20 000 CY

I

36 000 FH

I

10 500 CY See note

References

Ctrl

Eff

N

AMM 571100-200-828

275

N

AMM 571100-200-828

943

Check : NT

Access panels :

191HB

192HB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

571137-01-6S020

191 192

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM AT FR.40, LH/RH.

T

60 000 FH

T

17 000 CY

I

36 000 FH

962

10 500 CY

1019

I

946

1256 1266

Access panels :

191HB

192HB

Total access time :

4.24 Hrs

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [9 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

571140-01-1

145 146

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE FITTED ABOVE THIS AREA TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : CABIN FLOOR PANELS; GALLEYS; TOILETS; NOTE: CPCP

Threshold Interval

T

6 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 571100-200-804

ALL

N

AMM 571100-200-811

ALL

Skills :

1.00 MHrs

1 AF 145 146

571140-02-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT FITTED ABOVE THIS AREA TPS : APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 3 PREP. : FLOOR PANELS Z250; SEATS AND FURNISHINGS Z250; NOTE: CPCP Skills :

1.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [10 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571144-01-3

191 192 195 196

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, LH/RH.

Threshold Interval

References

Ctrl

Eff

N

AMM 571100-270-802

275

N

AMM 571100-270-802

943

T

140 800 FH

T

21 600 CY

I

30 300 FH

I

4 650 CY See note

T

137 500 FH

T

21 100 CY

I

29 700 FH

962

4 550 CY

1019

Access panels :

191HB

191QB

Total access time :

192HB 192QB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

571144-01-6S020

191 192 195 196

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, LH/RH.

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [11 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571149-01-6

191 192

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 DATUM TO STRINGER 1 LEVEL, LH/RH.

Threshold Interval

T

194 200 FH

T

29 800 CY

I

35 100 FH

I

5 400 CY

T

18 400 FH

T

5 650 FC

I

8 000 FH

I

2 450 CY See note

References

Ctrl

Eff

N

AMM 571100-250-801

275

N

EAD 2010-0024 FAD 2011-24-05 ISB 57-3081

366

Access panels :

191HB

192HB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 141 142 191 192

571150-01-4

Issue No

:

Date

:

10 01/12/2013

MAIN STRUCTURE MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF THE KEEL BEAM HORIZONTAL FLANGE AT FR40. NOTE: MANDATORY TASK AT FH OPTIMIZED: TH: 12000 FC/ 78400 FH IN: 8550 FC/ 55600 FH FC OPTIMIZED: TH: 13500 FC/ 44200 FH IN: 9600 FC/ 31400 FH

Amendment No Date

: 01 : 06/09/2014

SDI

Page : STR - 57 [12 / 188] ATA

: 57


57

WINGS

Task Number

Zone

571152-01-3

141 142

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT FASTENERS 3 TO 12, LH/RH. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 571100-200-822

275

N

AMM 571100-200-822

943

T

135 200 FH

T

20 800 CY

I

94 100 FH

I

14 400 CY See note

T

137 200 FH

T

21 100 CY

I

92 700 FH

962

14 200 CY

1019

Access panels :

147AZ

148AZ

Total access time :

734 744 0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

571152-01-5S020

141 142

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE FASTENERS 3 TO 12, LH/RH. PREP. : FUEL TANK DRAINED AND VENTED;

I

946

1256 1266

Access panels :

147AZ

148AZ

Total access time :

734

744

1.08 Hrs

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [13 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

571159-01-7S020

145 146

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPARE VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) PREP: CABIN FLOOR PANELS;

Threshold Interval

References

Ctrl

N

AMM 571100-200-823

Eff 943

T

98 900 FH

T

15 200 CY

I

54 900 FH

962

8 450 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 NDT 141 142

571160-01-1

DI

CENTER WING BOX STRUTS DETAILED INSPECTION OF CENTER WING BOX, STRUTS (54 PLACES) PREP. : FUEL TANK DRAINED AND VENTED;

T

12 YE

I

12 YE

T

156 700 FH

T

24 100 CY

I

24 600 FH

I

3 700 CY

N

AMM 571100-200-807

ALL

N

AMM 572000-210-821

275

Access panels :

147AZ

148AZ

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 500 600

572001-02-1

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 9 AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON REINFORCING Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [14 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572002-01-4

452 454 462 464

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A

Threshold Interval

T

74 400 FH

T

21 200 CY

I

21 800 FH

I

6 200 CY

T

138 800 FH

T

39 600 CY

I

25 900 FH

I

7 400 CY See note

References

Ctrl

Eff

N

AMM 572000-210-804

275

N

AMM 572000-210-833

275

Access panels :

454KL 464MR

454KR

Total access time :

454ML

454MR

464KL

464KR

464ML

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 454 464

572003-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00;

Access panels :

454BL 464NR

454BR

Total access time :

454CL

454NR

464BL

464BR

464CL

0.00 Hrs

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [15 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572004-02-7S020

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING PREP. : FUEL PUMP FAIRINGS

Threshold Interval

References

Ctrl

N

AMM 572000-210-822

Eff 943

T

131 400 FH

T

20 200 CY

I

25 000 FH

962

3 800 CY

1019

I

946

1256 1266

Skills :

1.60 MHrs

1 AF 572007-01-4S100

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING. PREP. : FIXED FLAP TRACK FAIRING Z531; FIXED FLAP TRACK FAIRING Z631; NOTE: CPCP

N

AMM 572000-210-806

275

T

103 300 FH

T

29 500 CY

294

T

12 YE

299

I

32 600 FH

I

9 300 CY

I

12 YE

T

12 YE

I

12 YE

366

Skills :

0.20 MHrs

1 AF R

500 600

572007-01-7

Issue No

:

Date

:

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING. PREP. : FIXED FLAP TRACK FAIRING Z531; FIXED FLAP TRACK FAIRING Z631;

Amendment No Date

: 01 : 06/09/2014

N

AMM 572000-210-806

943 946 962 1019 1256 1266

Page : STR - 57 [16 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572008-01-3

531 631

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING.

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-834

275

N

AMM 572000-210-807

943

T

125 000 FH

T

19 200 CY

I

25 300 FH

I

3 900 CY

T

105 000 FH

T

16 100 CY

I

28 900 FH

962

4 400 CY

1019

Access panels :

531AB

631AB

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 NDT R

572009-01-8S020

Issue No

:

Date

:

540 640

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-8 PREP. : FIXED FLAP TRACK FAIRING Z531; FUEL PUMP FAIRINGS Z500; FIXED FLAP TRACK FAIRING Z631; FUEL PUMP FAIRINGS Z600;

Amendment No Date

: 01 : 06/09/2014

I

946

1256 1266

Page : STR - 57 [17 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572009-02-8S020

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-8 PREP. : FIXED FLAP TRACK FAIRING Z531; FUEL PUMP FAIRINGS Z500; FIXED FLAP TRACK FAIRING Z631; FUEL PUMP FAIRINGS Z600; NOTE: RII TASK

Threshold Interval

References

Ctrl

N

AMM 572000-210-823

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

105 000 FH

T

16 100 CY

I

93 900 FH

962

14 400 CY

1019

I

946

1256 1266

0.80 MHrs

: 01 : 06/09/2014

943

T

Skills :

1 NDT

Eff

Page : STR - 57 [18 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572010-01-1

541 641

Task code

Task Title

DI

ACCESS DOOR CUTOUTS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUT IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572000-210-808

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 641DB

541DB 641EB

541EB 641FB

541FB

641AB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572010-01-1S100

541 641

DI

ACCESS DOOR CUTOUTS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUT IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

T

24 YE

I

12 YE

N

AMM 572000-210-808

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [19 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572010-02-4

541 641

Task code

Task Title

SDI

ACCESS DOOR CUTOUTS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-220-852

275

N

AMM 572000-220-852

943

T

119 100 FH

T

18 300 CY

I

34 800 FH

I

5 300 CY

T

104 000 FH

T

16 000 CY

I

74 100 FH

962

I

11 400 CY

1019

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 641DB

541DB 641EB

541EB 641FB

541FB

641AB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT R

572010-02-9S020

541 641

SDI

ACCESS DOOR CUTOUTS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12. PREP. : FUEL TANK DRAINED AND VENTED;

946

1256 1266

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 641DB

541DB 641EB

541EB 641FB

541FB

641AB

6.00 Hrs

Skills :

1.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [20 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572011-02-1

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING.

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-824

275

N

AMM 572000-210-826

943

T

134 200 FH

T

20 600 CY

I

29 800 FH

I

4 500 CY

T

130 400 FH

T

20 000 CY

I

27 900 FH

962

4 300 CY

1019

Skills :

0.20 MHrs

1 AF R

572012-02-6S020

500 600

DI


I

946

1256 1266

Skills :

0.30 MHrs

1 AF 500 600

572012-03-2

GVI

WING BOTTOM SKIN GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING note:CPCP

T

6 YE

I

6 YE

N

AMM 572000-210-825

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [21 / 188] ATA

: 57

ALL


57

WINGS

Task Number

Zone

572013-03-1

454 464

Task code

Task Title

DI

WING BOTTOM SKIN DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.

Threshold Interval

T

125 000 FH

T

19 200 CY

I

32 900 FH

I

5 000 CY

T

81 800 FH

T

23 300 CY

I

22 900 FH

I

6 500 CY See note

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 572000-220-870

275

N

AMM 572000-210-827

275

N

AMM 572000-210-811

ALL

Access panels :

454BL 454KL 464CL 464ML

454BR 454KR 464GL 464MR

Total access time :

500 600

572014-02-1

454CL 454ML 464GR 464NR

454GL 454MR 464HL

454GR 454NR 464HR

454HL 464BL 464KL

454HR 464BR 464KR

0.00 Hrs DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY FAIRINGS. Skills :

0.00 MHrs

1 AF 500 600

572015-01-2

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. note:CPCP Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [22 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572015-02-1

500 600

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-819

275

N

AMM 572000-210-819

943

T

88 800 FH

T

25 300 CY

I

27 700 FH

I

7 900 CY

T

88 800 FH

T

25 300 CY

I

23 900 FH

962

6 800 CY

1019

Skills :

0.60 MHrs

1 NDT R

572015-02-6S020

500 600

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.

I

946

1256 1266

Skills :

0.60 MHrs

1 NDT 500 600

572016-01-2

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4. note:CPCP

T

6 YE

I

6 YE

N

AMM 572000-210-812

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [23 / 188] ATA

: 57

ALL


57

WINGS

Task Number

Zone

572016-02-4

500 600

541 641

572017-01-4

Task code

Task Title

SDI

OUTER WING SPECIAL VISIBLE AND RIB PREP. :

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 4. FUEL PUMP FAIRINGS DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

T

93 200 FH

T

26 600 CY

I

12 600 FH

I

3 600 CY See note

T

81 200 FH

T

23 200 CY

I

33 000 FH

I

9 400 CY

References

Ctrl

N

AMM 572000-210-813

275

N

AMM 572000-210-839

275

Access panels :

541AB

541AZ

Total access time :

541BZ

641AB

641AZ

641BZ

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Eff

Page : STR - 57 [24 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572017-01-7S020

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-839

Eff 943

T

153 700 FH

T

23 600 CY

I

74 200 FH

962

11 400 CY

1019

I

946

1256 1266

Access panels :

541AB

541AZ

Total access time :

541BZ

641AB

641AZ

641BZ

2.72 Hrs

Skills :

1.20 MHrs

1 AF 541 641

572018-01-5

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20 BETWEEN RIB 5 AND RIB 7. PREP. : FUEL TANK DRAINED AND VENTED;

T

131 600 FH

T

20 200 CY

I

43 700 FH

I

6 700 CY

N

AMM 572000-210-840

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :

541BB 541FZ 641DB

541BZ 641AB 641DZ

541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

0.00 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [25 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572018-01-9S020

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20 BETWEEN RIB 5 AND RIB 7. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-840

Eff 943

T

131 300 FH

T

20 200 CY

I

40 400 FH

962

6 200 CY

1019

I

946

1256 1266

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :


541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

Skills :

3.00 MHrs

2 AF R

572019-01-9S020

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS UPPER SURFACE BETWEEN FRONT SPAR AND STRINGER 8 AND BOTTOM STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 20. PREP. : FUEL TANK DRAINED AND VENTED;

N

AMM 572000-210-841

131 300 FH

T

20 200 CY

I

31 000 FH

962

4 700 CY

1019

I

946

1256 1266

Skills :

2.00 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

T

Page : STR - 57 [26 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572020-01-1

541 641

Task code

Task Title

GVI

OUTER WING GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE INCLUDING STRINGERS AND BUTTSTRAPS BETWEEN RIB 1 AND RIB 3. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

96 700 FH

T

27 600 CY

I

25 400 FH

I

7 200 CY

References

Ctrl

Eff

N

AMM 572000-210-880

ALL

N

AMM 572000-220-869

275

Access panels :

541AB

541AZ

Total access time :

541BZ 641AB 0.00 Hrs

641AZ

641BZ

Skills :

1.00 MHrs

2 AF 454 464 531 631

572021-03-1

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND FLAP TRACK 2 FAIRING. Access panels :

454GL 464MR

454GR 531AB

Total access time :

454ML 454MR 631AB 6.12 Hrs

464GL

464GR

464ML

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [27 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572023-02-8S020

500 600

Task code

Task Title

DI

BOTTOM SKIN AT STGR ATTACHMENTS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.

Threshold Interval

References

Ctrl

N

AMM 572000-210-832

Eff 943

T

96 700 FH

T

14 800 CY

I

24 900 FH

962

3 800 CY

1019

I

946

1256 1266

Skills :

0.60 MHrs

1 AF 541 641

572026-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9. PREP. : FUEL TANK DRAINED AND VENTED;

T

79 700 FH

T

22 700 CY

I

38 500 FH

I

11 000 CY

N

AMM 572000-210-845

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :


541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

Skills :

0.80 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [28 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572027-01-9S020

541 641

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-220-855

Eff 943

T

107 800 FH

T

16 500 CY

I

44 200 FH

962

6 800 CY

1019

I

946

1256 1266

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :


541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

Skills :

0.80 MHrs

1 NDT 500 600

572029-01-3

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SKIN SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 12.

T

143 100 FH

T

23 800 CY

I

105 700 FH

I

16 200 CY

N

AMM 572000-210-847

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [29 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572029-01-8S020

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SKIN SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 12.

Threshold Interval

References

Ctrl

N

AMM 572000-210-847

Eff 943

T

144 200 FH

T

22 200 CY

I

50 500 FH

962

7 700 CY

1019

I

946

1256 1266

Skills :

0.40 MHrs

1 AF 572030-01-4S100

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND RIB 11.

T

144 200 FH

N

AMM 572000-220-847

275

N

AMM 572000-220-847

943

T

22 200 CY

I

105 600 FH

I

16 200 CY

T

144 200 FH

T

22 100 CY

I

70 300 FH

962

I

10 800 CY

1019

Skills :

0.20 MHrs

1 AF R

572030-01-9S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND RIB 11.

946

1256 1266

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [30 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572034-01-4

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENO RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-851

275

N

AMM 572000-210-851

943

T

127 700 FH

T

19 600 CY

I

81 700 FH

I

12 500 CY

T

127 700 FH

T

19 600 CY

I

127 700 FH

962

19 600 CY

1019

Skills :

0.60 MHrs

1 AF R

572034-01-8S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENO RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13

I

946

1256 1266

Skills :

0.60 MHrs

1 AF 500 600

572035-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB 8

T

127 700 FH

T

19 600 CY

I

67 600 FH

I

10 400 CY

N

AMM 572000-210-852

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [31 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572035-01-8S020

500 600

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB 8

Threshold Interval

References

Ctrl

N

AMM 572000-210-852

Eff 943

T

127 700 FH

T

19 600 CY

I

127 700 FH

962

19 600 CY

1019

I

946

1256 1266

Skills :

0.20 MHrs

1 AF 572036-01-4S100

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS. PREP. : FUEL TANK DRAINED AND VENTED;

N

AMM 572000-210-853

275

N

AMM 572000-210-853

943

T

74 700 FH

T

21 300 CY

I

37 100 FH

I

10 600 CY

T

90 900 FH

T

13 900 CY

I

67 300 FH

962

I

10 300 CY

1019

Skills :

0.60 MHrs

1 AF R

572036-01-8S020

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS. PREP. : FUEL TANK DRAINED AND VENTED;

946

1256 1266

Access panels :

541AB

541AZ

Total access time :

541BZ 641AB 2.72 Hrs

641AZ

641BZ

Skills :

0.60 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [32 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572037-01-4

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 AND TOP SKIN LOWER SURFACE AT ROOT JOINT FROM FRONT SPAR TO REAR SPAR. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-854

275

N

AMM 572000-210-854

943

T

74 700 FH

T

21 300 CY

I

50 600 FH

I

14 400 CY

T

90 900 FH

T

13 900 CY

I

90 900 FH

962

13 900 CY

1019

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :

541BB 541FZ 641DB

541BZ 641AB 641DZ

541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

0.00 Hrs

Skills :

0.00 MHrs

1 AF R

572037-01-7S020

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 AND TOP SKIN LOWER SURFACE AT ROOT JOINT FROM FRONT SPAR TO REAR SPAR. PREP. : FUEL TANK DRAINED AND VENTED;

I

946

1256 1266

Access panels :

541AB 541DZ 641CB

541AZ 541EZ 641CZ

Total access time :


541CB 641AZ 641EZ

541CZ 641BB 641FZ

541DB 641BZ

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [33 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572039-01-4

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 AND FROM RIB 11 TO 12.

Threshold Interval

T

143 100 FH

References

Ctrl

Eff

N

AMM 572000-210-855

275

N

AMM 572000-210-855

943

T

23 800 CY

I

105 700 FH

I

16 200 CY

T

144 200 FH

T

22 200 CY

I

69 300 FH

962

10 600 CY

1019

Skills :

0.30 MHrs

1 AF R

572039-01-9S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 AND FROM RIB 11 TO 12.

I

946

1256 1266

Skills :

0.30 MHrs

1 AF 500 600

572040-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND RIB 13. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

T

127 700 FH

T

19 600 CY

I

90 000 FH

I

13 800 CY

N

AMM 572000-210-856

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [34 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572040-01-8S020

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND RIB 13.

Threshold Interval

References

Ctrl

N

AMM 572000-210-856

Eff 943

T

127 700 FH

T

19 600 CY

I

127 700 FH

962

19 600 CY

1019

I

946

1256 1266

Skills :

0.20 MHrs

1 AF 573 673

572043-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 9.

N

AMM 572000-210-857

275

N

AMM 572000-210-857

943

T

73 400 FH

T

20 900 CY

I

49 600 FH

I

14 100 CY

T

92 400 FH

T

14 200 CY

I

39 000 FH

962

I

6 000 CY

1019

Skills :

0.20 MHrs

1 AF R

572043-01-9S020

573 673

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 9.

946

1256 1266

Access panels :

573FB

673FB

Total access time :

3.44 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [35 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572045-01-3

541 641

572045-01-3S020

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED;

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572000-210-814

Eff 294 299 366

DI

OUTER WING

Threshold Interval

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

T

83 100 FH

T

27 700 CY

T

12 YE

I

35 800 FH

I

10 200 CY

I

12 YE

N

AMM 572000-210-814

275

N

AMM 572000-210-814

943

See note Check : NT R

541 641

572045-01-4

Issue No

:

Date

:

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED;

Amendment No Date

: 01 : 06/09/2014

T

128 000 FH

T

21 300 CY

T

12 YE

I

52 400 FH

I

8 000 CY

I

12 YE

946 962 1019 1256 1266

Page : STR - 57 [36 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572047-01-8S020

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING BOLTING AREAS) AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. PREP. : SEALANT REMOVAL AS PER NTM;

Threshold Interval

References

Ctrl

N

AMM 572000-220-856

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

16 000 CY

1019

I

946

1256 1266

Skills :

0.40 MHrs

1 NDT 571 671

572055-01-2

Issue No

:

Date

:

10 01/12/2013

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT ATTACHMENT TO UPPER AND LOWER ROOT JOINT FITTINGS. PREP. : FLAPS EXTENDED; SEALANT REMOVAL AS PER NTM;

Amendment No Date

: 01 : 06/09/2014

T

135 500 FH

T

38 700 CY

I

24 700 FH

I

7 000 CY

N

AMM 572000-250-801

Page : STR - 57 [37 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572062-01-1

541 641

Task Title

Task code

DI

OUTER WING

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE UPPER AND LOWER ROOT JOINT FITTINGS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572000-210-815

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

541AB

641AB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572062-01-1S100

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE UPPER AND LOWER ROOT JOINT FITTINGS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

T

24 YE

I

12 YE

N

AMM 572000-210-815

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [38 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572063-01-5

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-210-860

275

N

AMM 572000-210-860

943

T

75 600 FH

T

21 600 CY

I

20 200 FH

I

5 700 CY

T

97 900 FH

T

15 000 CY

I

28 300 FH

962

4 300 CY

1019

Access panels :

541AB 641BB

541BB 641CB

Total access time :

R

572063-01-9S020

541 641

541CB 641DB

541DB 641EB

541EB 641FB

541FB

641AB

6.00 Hrs DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12. PREP. : FUEL TANK DRAINED AND VENTED;

I

946

1256 1266

Access panels :

541AB 641BB

541BB 641CB

Total access time :

541CB 641DB

541DB 641EB

541EB 641FB

541FB

641AB

6.00 Hrs

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [39 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572064-01-1

540 640

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-861

Eff 943

T

117 200 FH

T

18 000 CY

I

31 500 FH

962

4 800 CY

1019

I

946

1256 1266

540 640

572064-01-5

DI

OUTER WING

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES. PREP. : FUEL TANK DRAINED AND VENTED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS 100% THRESHOLD ""25200 FC OR 116000 FH"" OR NEXT ""6900FC OR 31700 FH "" FROM APPROVE DATE"

T

83 000 FH

T

23 700 CY

I

26 900 FH

I

7 600 CY

N

AMM 572000-210-861

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [40 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572065-01-1

522 622

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12. NOTE: CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

90 400 FH

T

25 800 CY

T

12 YE

I

90 400 FH

I

25 800 CY

I

6 YE

T

20 YE

I

6 YE

References

Ctrl

Eff

N

AMM 572000-210-816

275

N

AMM 572000-210-816

294

Access panels :

522DB

522EB

Total access time :

622DB 622EB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 572065-01-1S100

522 622

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12. NOTE: CPCP

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [41 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572065-01-6S020

522 622

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12. NOTE: CPCP

Threshold Interval

T

116 300 FH

T

17 800 CY

T

12 YE

References

Ctrl

N

AMM 572000-210-816

Eff 943 946 962 1019

I

116 300 FH

I

17 800 CY

I

6 YE

T

116 300 FH

T

17 800 CY

I

116 300 FH

962

17 800 CY

1019

1256 1266

Access panels :

522DB

522EB

Total access time :

622DB 622EB 0.00 Hrs

Skills :

0.00 MHrs

1 AF R

500 600

572066-01-1

DI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12.

I

N

AMM 572000-220-866

943 946

1256 1266

500 600

572066-01-4

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12.

T

90 400 FH

T

25 800 CY

I

90 400 FH

I

25 800 CY

N

AMM 572000-220-866

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [42 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572067-03-7

541

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. PREP. : FUEL TANK DRAINED AND VENTED;

R

572068-01-9S020

541 641

Threshold Interval

References

Ctrl

N

AMM 572000-220-877

128 300 FH

T

19 700 CY

I

108 200 FH

962

16 600 CY

1019

946

1256 1266

DI

DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. PREP. : FUEL TANK DRAINED AND VENTED;

N

AMM 572000-220-848

Total access time :

541EZ

541FZ

641CB

641DB

60 000 FH

T

17 000 CY

I

50 000 FH

962

12 500 CY

1019

I

946

1256 1266

641EZ

3.96 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

T

Access panels :

541DB

943

T

I

OUTER WING

541CB 641FZ

Eff

Page : STR - 57 [43 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572071-01-8S020

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-866

Eff 943

T

193 100 FH

T

32 100 CY

I

91 700 FH

962

14 100 CY

1019

I

946

1256 1266

Access panels :

541AB 641AB

541AZ 641AZ

Total access time :

541BB 641BB

541BZ 641BZ

541CZ 641CZ

541DZ 641DZ

541EZ 641EZ

4.68 Hrs

Skills :

2.00 MHrs

1 AF 541 641

572071-01-9

Issue No

:

Date

:

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING.

Amendment No Date

: 01 : 06/09/2014

T

193 100 FH

T

32 100 CY

I

193 100 FH

I

32 100 CY

N

AMM 572000-210-866

Page : STR - 57 [44 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572073-01-4

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS PREP. : FIXED FLAP TRACK FAIRING Z532; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FUEL TANK DRAINED AND VENTED; NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

60 000 FH

T

20 000 FC

I

50 000 FH

I

20 000 CY See note

References

Ctrl

N

AMM 572000-210-868

Check : NT

Access panels :

541FB

541GB

Total access time :

641FB 641GB 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [45 / 188] ATA

: 57

Eff ALL


R

57

WINGS

Task Number

Zone

572073-01-8S020

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. PREP. : FIXED FLAP TRACK FAIRING Z532; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-868

541GB

Total access time :

60 000 FH

T

20 000 CY

I

50 000 FH

962

11 700 CY

1019

I

946

1256 1266

641FB 641GB 2.00 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

T

Access panels :

541FB

Eff

Page : STR - 57 [46 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572075-01-1

541 641

Task Title

Task code

DI

OUTER WING

DETAILED INSPECTION OF OUTER WING BOX, RIB 1 EXTERNAL SURFACE AND UPPER SURFACE OF TRIFORM FITTING, BETWEEN FRONT SPAR AND REAR SPAR. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572000-220-801

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

541AB

641AB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572075-01-1S100

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOX, RIB 1 EXTERNAL SURFACE AND UPPER SURFACE OF TRIFORM FITTING, BETWEEN FRONT SPAR AND REAR SPAR. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED;

T

24 YE

I

12 YE

N

AMM 572000-220-801

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [47 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572082-01-5S100

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

T

72 500 FH

T

20 700 CY

I

29 500 FH

I

8 400 CY

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 572000-210-870

275

N

AMM 572000-210-818

275

Skills :

2.00 MHrs

1 AF R

541 641

572083-01-1

DI

OUTER WING

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY AFT FACE BETWEEN RIBS 1 AND 2. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

943 946

See note Check : NT

962 1019 1256 1266

Access panels :

541AB

541BZ

Total access time :

641AB 641BZ 0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [48 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572083-01-1S100

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY AFT FACE BETWEEN RIBS 1 AND 2. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572000-210-818

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 191 192

572085-01-1

GVI

OUTER WING GENERAL VISUAL INSPECTION OF OUTER WING BOX, CRUCIFORM FITTING, OUTBOARD FLANGE UPPER SURFACE AS FAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RH note:CPCP

T

12 YE

I

12 YE

T

101 000 FH

T

28 800 CY

I

19 200 FH

I

5 400 CY

N

AMM 572000-210-874

ALL

N

AMM 572000-220-868

275

Access panels :

191BT

191CT

Total access time :

192BT

192CT

0.00 Hrs

Skills :

0.00 MHrs

1 AF 500 600

572090-01-1

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-1 Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [49 / 188] ATA

: 57


D

57

WINGS

Task Number

Zone

572090-02-1

500 600

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-1

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-220-872

275

N

AMM 572000-210-872

943

T

101 000 FH

T

28 800 CY

I

47 600 FH

I

13 600 CY

T

110 100 FH

T

16 900 CY

I

36 300 FH

962

5 500 CY

1019

Skills :

0.00 MHrs

1 NDT R

572092-01-8S020

541 641

DI


I

946

1256 1266

Access panels :

541EB

541FB

Total access time :

641EB

641FB

2.00 Hrs

Skills :

0.60 MHrs

2 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [50 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572093-01-4S020

541 641

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-4 PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572000-210-873

Eff 943

T

94 700 FH

T

14 500 CY

I

29 000 FH

962

4 400 CY

1019

I

946

1256 1266

Access panels :

541FB

641FB

Total access time :

1.00 Hrs

Skills :

0.20 MHrs

1 AF 541 641

572093-01-6

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME A TASK 572093-02-6 PREP. : FUEL TANK DRAINED AND VENTED;

T

81 700 FH

T

23 300 CY

I

29 000 FH

I

8 200 CY

N

AMM 572000-210-873

Access panels :

541FB

641FB

Total access time :

1.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [51 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572093-02-4S020

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-4S020 PREP. : SEALANT REMOVAL AS PER NTM;

Threshold Interval

References

Ctrl

N

AMM 572000-220-865

Eff 943

T

94 700 FH

T

14 500 CY

I

29 000 FH

962

4 400 CY

1019

I

946

1256 1266

Access panels :

541FB

641FB

Total access time :

1.00 Hrs

Skills :

0.20 MHrs

1 NDT 541 641

572093-02-6

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-6 PREP. : SEALANT REMOVAL AS PER NTM;

T

81 700 FH

T

23 300 CY

I

29 000 FH

I

8 200 CY

N

AMM 572000-220-865

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [52 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572094-01-5

541 641

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 AND RIB 12. PREP. : FIXED FLAP TRACK FAIRING Z532; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572000-220-861

275

N

AMM 572000-220-861

943

T

70 600 FH

T

20 100 CY

I

32 200 FH

I

9 200 CY

T

107 400 FH

T

16 500 CY

I

42 300 FH

962

6 500 CY

1019

Access panels :

541EB

541FB

Total access time :

541GB 641EB 3.00 Hrs

641FB

641GB

Skills :

0.40 MHrs

1 NDT R

572094-01-9S020

541 641

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 AND RIB 12. PREP. : FIXED FLAP TRACK FAIRING Z532; FUEL TANK DRAINED AND VENTED; FIXED FLAP TRACK FAIRING Z632; FUEL TANK DRAINED AND VENTED;

I

946

1256 1266

Access panels :

541EB

541FB

Total access time :

541GB 641EB 3.00 Hrs

641FB

641GB

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [53 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572095-01-5

541 641

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM STRINGER 20 BETWEEN RIB 5 AND RIB 7.

Threshold Interval

T

137 300 FH

T

39 200 CY

I

32 400 FH

I

9 200 CY See note

T

25 000 FH

T

8 000 FC

I

25 000 FH

References

Ctrl

Eff

N

AMM 572000-220-862

275

N

AMM EAD FAD ISB

275

Access panels :

541BB

541CB

Total access time :

641BB

641CB

2.00 Hrs

Skills :

0.40 MHrs

1 NDT 541 641

572099-01-1

SDI

OUTER WING

DETAILED INSPECTION OF RIB 6 AFT WEB BETWEEN BOTTOM SKIN STRINGERS 18 TO 20. PREP. : FUEL TANK DRAINED AND VENTED NOTE : TASK IS COVERED BY REPAIR TASK 572099-275 OR 572099-294, 572099-299, 572099-366. ALL A/C REPAIRED ACC. R572-57023 OR R572-57026, ARE NOT ANYMORE RELATED BY EASA-2007-0148.

I


572000-210-885 2007-0148 2006-22-14 57-3085

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [54 / 188] ATA

: 57

294 299 366


57

WINGS

Task Number

Zone

572099-275

541 641

OUTER WING

541 641

OUTER WING

541 641

OUTER WING

572099-294

572099-299

Issue No

:

Date

:

10 01/12/2013

Task code

Task Title

DVI

Amendment No Date

275

T

112 901 FH

N

294

N

299

33 381 FC See note Check : NT

DVI

: 01 : 06/09/2014

N

T

ABOVE

ABOVE

103 015 FH

Eff


DVI

DETAILED VISUAL INSPECTION RIB 6 REPAIR ATTACHMENT END BOLTS STRINGER 21/22 IN BOTH RIB AND REPAIR PLATE. NOTE : THIS TASK COVERS TASK 572099-01-1 AND 572099-02-1 REF. NOTE : RAS/BAE/1002101/2006 ISSUE A INTERVAL NOTE : TBD INSPECTION METHOD : TBD

T

References

Ctrl

T

DETAILED VISUAL INSPECTION RIB 6 AFT REPAIR PLATE SATELLITE HOLES AT 71.5 MM DIAMETER FUEL SYSTEM HOLE. DETAILED VISUAL INSPECTION RIB 6 REPAIR ATTACHMENT END BOLTS ABOVE STRINGER 21/22 IN BOTH RIB AND REPAIR PLATE. NOTE : THIS TASK COVERS MPD TASK 572099-01-1 AND 572099-02-1 REF. NOTE : RAS/BAE/1000398/2005 ISSUE B INTERVAL NOTE : TBD INSPECTION METHOD : TBD

DETAILED VISUAL INSPECTION RIB 6 REPAIR ATTACHMENT END BOLTS STRINGER 21/22 IN BOTH RIB AND REPAIR PLATE. NOTE : THIS TASK COVERS TASK 572099-01-1 AND 572099-02-1 REF. NOTE : RAS/BAE/1002000/2005 ISSUE A INTERVAL NOTE : TBD INSPECTION METHOD : TBD

Threshold Interval

T

113 652 FH

T


Page : STR - 57 [55 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572099-366

541 641

OUTER WING

500 600

OUTER WING

572101-01-4

Task code

Task Title

DVI

DETAILED VISUAL INSPECTION RIB 6 REPAIR ATTACHMENT END BOLTS STRINGER 21/22 IN BOTH RIB AND REPAIR PLATE. NOTE : THIS TASK COVERS TASK 572099-01-1 AND 572099-02-1 REF. NOTE : RAS/BAE/1002281/2006 ISSUE B INTERVAL NOTE : TBD INSPECTION METHOD : TBD

Threshold Interval

T

102 642 FH

References

Ctrl

N

Eff 366

T


ABOVE

DI

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

T

103 300 FH

T

29 500 CY

I

22 700 FH

I

6 400 CY

T

103 300 FH

T

29 500 CY

I

23 600 FH

I

6 700 CY

N

AMM 572100-210-846

275

N

AMM 572100-210-847

275

Skills :

0.00 MHrs

1 AF 500 600

572104-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED B PYLON REINFORCING, PYLON FAIRING, PLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND RIB 39. Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [56 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572106-01-4

500 600

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 AND RIB 23. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572106-02-1.

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-220-809

275

N

AMM 572100-220-809

943

T

72 800 FH

T

20 800 CY

I

45 400 FH

I

12 900 CY

T

129 500 FH

T

19 900 CY

I

88 700 FH

962

13 600 CY

1019

Skills :

0.00 MHrs

1 NDT R

572106-01-8S020

500 600

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 AND RIB 23. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572106-02-4.

I

946

1256 1266

Skills :

1.20 MHrs

1 NDT 500 600

572106-02-1

Issue No

:

Date

:

10 01/12/2013

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 AND RIB 23. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572106-01-4.

Amendment No Date

: 01 : 06/09/2014

T

72 800 FH

T

20 800 CY

I

16 600 FH

I

4 700 CY

N

AMM 572100-210-893

Page : STR - 57 [57 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572106-02-4

500

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 AND RIB 23. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572106-01-8.

500 600

572107-01-4

References

Ctrl

N

AMM 572100-210-893

Eff 943

T

129 500 FH

T

19 900 CY

I

29 400 FH

962

4 500 CY

1019

I

946

1256 1266

SDI

OUTER WING

Threshold Interval

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-1.

N

AMM 572100-220-810

275

N

AMM 572100-220-810

943

T

95 700 FH

T

27 300 CY

I

32 900 FH

I

9 400 CY

T

106 700 FH

T

16 400 CY

I

84 800 FH

962

13 000 CY

1019

Skills :

0.00 MHrs

1 NDT R

572107-01-8S020

500 600

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-5.

I

946

1256 1266

Skills :

1.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [58 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572107-02-1

500 600

500

572107-02-5

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-4.

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-8.

Issue No

:

Date

:

10 01/12/2013

Task code

Amendment No Date

: 01 : 06/09/2014

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-210-892

275

N

AMM 572100-210-892

943

T

95 700 FH

T

27 300 CY

I

11 500 FH

I

3 200 CY

T

106 700 FH

T

16 400 CY

I

27 000 FH

962

4 100 CY

1019

I

946

1256 1266

Page : STR - 57 [59 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572108-01-2

541 542 641 642

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. note:CPCP

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 572100-210-801

Access panels :

532AB 541LB 542AB 641GB 641PB 642DB

533AB 541MB 542BB 641HB 641QB

Total access time :

534AB 541NB 542CB 641JB 641RB

541GB 541PB 542DB 641KB 641SB

541HB 541QB 632AB 641LB 642AB

541JB 541RB 633AB 641MB 642BB

541KB 541SB 634AB 641NB 642CB

0.00 Hrs

Skills :

4.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [60 / 188] ATA

: 57

Eff ALL


57

WINGS

Task Number

Zone

572108-02-4

541 542 641 642

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27.

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-210-821

275

N

AMM 572100-210-821

943

T

89 400 FH

T

25 500 CY

I

27 200 FH

I

7 700 CY

T

104 000 FH

T

16 000 CY

I

83 700 FH

962

12 800 CY

1019

Access panels :

532AB 541LB 542AB 641GB 641PB 642DB

533AB 541MB 542BB 641HB 641QB

Total access time :

534AB 541NB 542CB 641JB 641RB

541GB 541PB 542DB 641KB 641SB

541HB 541QB 632AB 641LB 642AB

541JB 541RB 633AB 641MB 642BB

541KB 541SB 634AB 641NB 642CB

0.00 Hrs

Skills :

4.00 MHrs

1 NDT R

572108-02-9S020

541 542 641 642

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27.

I

946

1256 1266

Skills :

4.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [61 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572109-01-1

542 550 642 650

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39. note:CPCP

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 572100-210-802

Access panels :

542EB 550BB 642GB 650DB

542FB 550CB 642HB 650EB

Total access time :

542GB 550DB 642JB 650FB

542HB 550EB 642KB

542JB 550FB 650AB

542KB 642EB 650BB

550AB 642FB 650CB

6.00 Hrs

Skills :

4.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [62 / 188] ATA

: 57

Eff ALL


57

WINGS

Task Number

Zone

572109-02-4

542 550 642 650

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

Threshold Interval

T

91 400 FH

T

26 100 CY

I

29 900 FH

I

8 500 CY

References

Ctrl

N

AMM 572100-220-812

Access panels :

542EB 550BB 642GB 650DB

542FB 550CB 642HB 650EB

Total access time :

542GB 550DB 642JB 650FB

542HB 550EB 642KB

542JB 550FB 650AB

542KB 642EB 650BB

550AB 642FB 650CB

12.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [63 / 188] ATA

: 57

Eff 275


R

57

WINGS

Task Number

Zone

572109-02-8S020

542 550 642 650

Task code

Task Title

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

Threshold Interval

References

Ctrl

N

AMM 572100-220-812

Eff 943

T

87 200 FH

T

13 400 CY

I

74 400 FH

962

11 400 CY

1019

I

946

1256 1266

Access panels :

542EB 550BB 642GB 650DB

542FB 550CB 642HB 650EB

Total access time :

542GB 542HB 550DB 550EB 642JB 642KB 650FB 18.00 Hrs

542JB 550FB 650AB

542KB 642EB 650BB

550AB 642FB 650CB

Skills :

4.80 MHrs

1 NDT R

572110-01-9S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

N

AMM 572100-210-848

943

T

117 000 FH

T

18 000 CY

I

32 600 FH

962

I

5 000 CY

1019

946

1256 1266

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [64 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572112-03-1

500 600

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRING 5.

Threshold Interval

T

91 000 FH

T

26 000 CY

I

35 000 FH

I

10 000 CY

T

78 200 FH

T

22 300 CY

I

23 300 FH

I

6 600 CY

References

Ctrl

Eff

N

AMM 572100-210-862

275

N

AMM 572100-210-853

275

Skills :

0.00 MHrs

1 AF 532 533 534 632 633 634

572117-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. Access panels :

532AB 632CB

532CB 633AB

Total access time :

533AB 533CB 633CB 634AB 0.00 Hrs

534AB 634CB

534CB

632AB

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [65 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572119-02-1

500 600

Task Title

WING BOTTOM SKIN AT HOLES

Task code

DI

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 12 AND 23. TPS : TPS MUST NOT BE APPLIED

Threshold Interval

References

Ctrl

N

AMM 572100-210-822

Eff 275

T

88 800 FH

T

25 300 CY

294

T

6 YE

299

I

24 500 FH

I

7 000 CY

I

6 YE

T

60 000 FH

T

20 000 CY

I

22 600 FH

366

Skills :

0.00 MHrs

1 AF 500 600

572120-01-4

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 IN RIB BAY 22-23. "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

N

AMM 572100-210-855

275

N

AMM 572100-210-855

943

I


Skills :

0.00 MHrs

1 AF R

572120-01-8S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 IN RIB BAY 22-23.

T

118 100 FH

T

18 100 CY

I

50 800 FH

962

7 800 CY

1019

I

946

1256 1266

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [66 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572121-01-9S020

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

Threshold Interval

References

Ctrl

N

AMM 572100-210-856

Eff 943

T

80 900 FH

T

12 400 CY

I

48 500 FH

962

7 400 CY

1019

I

946

1256 1266

Access panels :

541GB 541PB 641KB 641SB

541HB 541QB 641LB

Total access time :

541JB 541RB 641MB

541KB 541SB 641NB

541LB 641GB 641PB

541MB 641HB 641QB

541NB 641JB 641RB

11.00 Hrs

Skills :

0.60 MHrs

1 AF 572122-01-4S100

542 550 642 650

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY 26-28 AND STRINGERS 15 & 18.

T

88 100 FH

T

25 100 CY

I

23 800 FH

I

6 800 CY

N

AMM 572100-210-857

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [67 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572123-01-1

542 550 642 650

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ACCESS DOORS BETWEEN RIB 27 AND RIB 39 INCLUDING NACA DUCT DOOR. note:CPCP

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 572100-210-804

Access panels :

542EB 550BB 642GB 650DB

542FB 550CB 642HB 650EB

Total access time :

542GB 550DB 642JB 650FB

542HB 550EB 642KB

542JB 550FB 650AB

542KB 642EB 650BB

550AB 642FB 650CB

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [68 / 188] ATA

: 57

Eff ALL


57

WINGS

Task Number

Zone

572124-01-3

542 642

Task Title

OUTER WING OUTBOARD OF RIB 12

Task code

GVI

GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE BETWEEN RIB 23 AND RIB 24. NOTE: TASK INTERVAL MAY BE INFLUENCED BY MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL ENVIRONMENT TPS : TPS MUST NOT BE APPLIED note: CPCP

Threshold Interval

T

6 YE

I

6 YE

T

99 400 FH

T

15 300 CY

T

12 YE

References

Ctrl

Eff

N

AMM 572100-210-869

ALL

N

AMM 572100-210-805

943

Access panels :

542AB

642AB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF R

572125-01-11S020

542 642

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-9S020 note:CPCP

I

58 800 FH

I

9 000 CY

I

12 YE

946 962 1019 1256 1266

Access panels :

542DB

542EB

Total access time :

642DB 642EB 3.00 Hrs

Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [69 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572125-02-9S020

542 642

Task Title

Task code

SDI

OUTER WING SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-11S020 PREP. : SEALANT REMOVAL AS PER NTM

Threshold Interval

References

Ctrl

N

AMM 572100-210-823

Eff 943

T

99 400 FH

T

15 300 CY

I

58 800 FH

962

9 000 CY

1019

I

946

1256 1266

Access panels :

542DB

542EB

Total access time :

642DB 642EB 3.00 Hrs

Skills :

0.80 MHrs

1 NDT R

542 642

572126-01-1

DI

MAIN STRUCTURE

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

T

12 YE

I

12 YE

N

AMM 572100-210-806

275 943 946

See note

962

Check : NT

1019 1256 1266

Access panels :

542EB

642EB

Total access time :

2.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [70 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572126-01-1S100

542 642

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-806

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 542 642

572126-02-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27.

T

74 200 FH

T

21 200 CY

I

19 100 FH

I

5 400 CY

N

AMM 572100-220-813

Access panels :

542EB

642EB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [71 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572126-02-8S020

542 642

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27.

Threshold Interval

References

Ctrl

N

AMM 572100-220-813

Eff 943

T

120 300 FH

T

18 500 CY

I

39 400 FH

962

6 000 CY

1019

I

946

1256 1266

Access panels :

542EB

642EB

Total access time :

2.00 Hrs

Skills :

0.60 MHrs

1 NDT R

550 650

572127-01-2

OUTER WING OUTBOARD OF RIB 12 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN UPPER SURFACE BETWEEN RIB 33 AND RIB 34. NOTE: TASK INTERVAL MAY BE INFLUENCED BY MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL ENVIRONMENT TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

GVI

T

6 YE

I

6 YE

N

AMM 572100-210-870

Access panels :

550AB

650AB

Total access time :

2.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [72 / 188] ATA

: 57

ALL


57

WINGS

Task Number

Zone

572131-01-4

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27. NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00

Threshold Interval

T

130 700 FH

References

Ctrl

Eff

N

AMM 572100-210-837

275

N

AMM 572100-210-837

943

T

21 700 CY

I

101 100 FH

I

15 500 CY

T

130 700 FH

T

21 700 CY

I

52 100 FH

962

8 000 CY

1019

Skills :

2.00 MHrs

1 AF R

572131-01-9S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

I

946

1256 1266

Skills :

2.00 MHrs

1 AF R

572133-01-9S020

500 600

DI


N

AMM 572100-210-835

943

T

86 200 FH

T

13 200 CY

I

54 000 FH

962

I

8 300 CY

1019

946

1256 1266

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [73 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572140-01-4

541 641

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-210-833

275

N

AMM 572100-210-833

943

T

74 400 FH

T

21 200 CY

I

52 500 FH

I

15 000 CY

T

105 800 FH

T

16 200 CY

I

105 800 FH

962

16 200 CY

1019

Access panels :

541EB 541MB 641FB 641NB

541FB 541NB 641GB 641PB

Total access time :

541GB 541PB 641HB 641QB 13.00 Hrs

541HB 541QB 641JB 641RB

541JB 541RB 641KB 641SB

541KB 541SB 641LB

541LB 641EB 641MB

Skills :

16.00 MHrs

1 AF R

572140-01-7S020

541 641

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.

I

946

1256 1266

Access panels :

541EB 541MB 641FB 641NB

541FB 541NB 641GB 641PB

Total access time :

541GB 541PB 641HB 641QB

541HB 541QB 641JB 641RB

541JB 541RB 641KB 641SB

541KB 541SB 641LB

541LB 641EB 641MB

13.00 Hrs

Skills :

16.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [74 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572141-01-4

542 550 642 650

Task code

Task Title

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. PREP. : FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-210-832

275

N

AMM 572100-210-832

943

T

109 000 FH

T

31 100 CY

I

61 200 FH

I

17 400 CY

T

151 900 FH

T

23 300 CY

I

122 400 FH

962

I

18 800 CY

1019

Access panels :

542AB 542HB 550EB 642FB 650CB

542BB 542JB 550FB 642GB 650DB

Total access time :

542CB 542KB 642AB 642HB 650EB 22.00 Hrs

542DB 550AB 642BB 642JB 650FB

542EB 550BB 642CB 642KB

542FB 550CB 642DB 650AB

542GB 550DB 642EB 650BB

Skills :

4.80 MHrs

2 AF R

572141-01-7S020

542 550 642 650

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. PREP. : FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED;

946

1256 1266

Skills :

4.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [75 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572144-01-8S020

542 642

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER SURFACE AT CHORDWISE JOINT AT RIB 27.

Threshold Interval

References

Ctrl

N

AMM 572100-210-831

Eff 943

T

120 300 FH

T

18 500 CY

I

120 300 FH

962

18 500 CY

1019

I

946

1256 1266

Access panels :

542EB

642EB

Total access time :

2.00 Hrs

Skills :

0.20 MHrs

1 AF 542 642

572144-01-9

DI

OUTER WING DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER SURFACE AT CHORDWISE JOINT AT RIB 27.

T

74 200 FH

T

21 200 CY

I

74 200 FH

I

21 200 CY

N

AMM 572100-210-831

Access panels :

542EB

642EB

Total access time :

2.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [76 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572148-01-4

542 642

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-210-830

275

N

AMM 572100-210-830

943

T

79 700 FH

T

22 700 CY

I

38 400 FH

I

10 900 CY

T

110 100 FH

T

16 900 CY

I

48 200 FH

962

7 400 CY

1019

Access panels :

542DB

542EB

Total access time :

642DB 642EB 3.00 Hrs

Skills :

0.40 MHrs

1 AF R

572148-01-9S020

542 642

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

I

946

1256 1266

Access panels :

542DB

542EB

Total access time :

642DB

642EB

3.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [77 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572149-01-4

500 600

Task Title

Task code

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 23 AND 39. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

Threshold Interval

References

Ctrl

N

AMM 572100-220-802

Eff 275

T

98 500 FH

T

28 100 CY

294

T

6 YE

299

I

20 600 FH

I

5 800 CY

I

6 YE

T

82 000 FH

T

23 400 CY

T

6 YE

366

Skills :

0.00 MHrs

1 AF R

572149-01-7S020

500 600

DI

OUTER WING DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 23 AND 39. TPS : TPS MUST NOT BE APPLIED note:CPCP

I

66 900 FH

I

10 200 CY

I

6 YE

N

AMM 572100-220-802

946 962 1019 1256 1266

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [78 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572151-01-1

574 674

Task code

Task Title

DI

MAIN STRUCTURE

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 12 AND RIB 27. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-808

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

574AT 574HB 674BB 674JB

574BB 574JB 674CB 674KB

Total access time :

574CB 574KB 674DB 674LB

574DB 574LB 674EB 674MB

574EB 574MB 674FB 674NB

574FB 574NB 674GB

574GB 674AT 674HB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572151-01-1S100

574 674

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 12 AND RIB 27. note:CPCP

T

20 YE

I

12 YE

N

AMM 572100-210-808

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [79 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572152-01-1

575 675

Task code

Task Title

DI

MAIN STRUCTURE

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 27 AND RIB 39. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-809

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

574AT 592AB 691AB 692DB

575AT 592BB 691BB

Total access time :

575BT 592CB 691CB

591AB 592DB 691DB

591BB 674AT 692AB

591CB 675AT 692BB

591DB 675BT 692CB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572152-01-1S100

575 675

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 27 AND RIB 39. note:CPCP

T

24 YE

I

12 YE

N

AMM 572100-210-809

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [80 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572153-01-10S020

574 575 674 675

Task code

Task Title

DI


Threshold Interval

T

78 900 FH

T

12 100 CY

T

12 YE

I

32 700 FH

I

5 000 CY

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-810

Eff 943 946 962 1019 1256 1266

Skills :

0.40 MHrs

1 AF R

542 550 642 650

572155-01-1

DI

MAIN STRUCTURE

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 30 AND RIB 39. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

N

AMM 572100-210-812

275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

542HB 550EB 650CB

542JB 550FB 650DB

Total access time :

542KB 642HB 650EB

550AB 642JB 650FB

550BB 642KB

550CB 650AB

550DB 650BB

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [81 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572155-01-1S100

542 550 642 650

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 30 AND RIB 39. note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-812

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 542 642

572156-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27.

T

87 100 FH

T

24 900 CY

I

52 100 FH

I

14 800 CY

N

AMM 572100-220-803

Access panels :

542DB

542EB

Total access time :

642DB

642EB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [82 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572156-01-8S020

542 642

Task code

Task Title

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. PREP. : SEALANT REMOVAL AS PER NTM

Threshold Interval

References

Ctrl

N

AMM 572100-220-803

Eff 943

T

146 900 FH

T

22 600 CY

I

56 800 FH

962

8 700 CY

1019

I

946

1256 1266

Access panels :

542DB

542EB

Total access time :

642DB

642EB

3.00 Hrs

Skills :

0.20 MHrs

1 NDT R

572158-01-9S020

541 641

DI


N

AMM 572100-210-826

943

T

79 200 FH

T

12 100 CY

I

45 900 FH

962

7 000 CY

1019

I

946

1256 1266

Access panels :

541GB 541PB 641KB 641SB

541HB 541QB 641LB

Total access time :

541JB 541RB 641MB

541KB 541SB 641NB

541LB 641GB 641PB

541MB 641HB 641QB

541NB 641JB 641RB

11.00 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [83 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572159-01-4

542 642

Task code

Task Title

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26.

Threshold Interval

References

Ctrl

Eff

N

AMM 572100-220-807

275

N

AMM 572100-220-807

943

T

71 400 FH

T

20 400 CY

I

21 200 FH

I

6 000 CY

T

116 100 FH

T

17 800 CY

I

45 900 FH

962

7 000 CY

1019

Access panels :

542AB

542BB

Total access time :

542CB 642AB 0.00 Hrs

642BB

642CB

Skills :

0.20 MHrs

1 NDT R

572159-01-8S020

542 642

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26.

I

946

1256 1266

Access panels :

542AB

542BB

Total access time :

542CB

642AB

642BB

642CB

3.00 Hrs

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [84 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572161-01-1

522 523 622 623

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 572100-210-813

Eff 275 943 946 962 1019

THRESHOLD IS NEXT

1256 1266

Access panels :

522EB 522MB 523AB 622HB 622QB 623DB

522FB 522NB 523BB 622JB 622RB

Total access time :

522GB 522PB 523CB 622KB 622SB

522HB 522QB 523DB 622LB 622TB

522JB 522RB 622EB 622MB 623AB

522KB 522SB 622FB 622NB 623BB

522LB 522TB 622GB 622PB 623CB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572161-01-1S100

522 523 622 623

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. note:CPCP

T

24 YE

I

6 YE

N

AMM 572100-210-813

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [85 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572162-01-4

523 623

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER FACE SPAR JOINT PLATE AT RIB NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE 50000FH FROM APPROVE DATE OF

WING FRONT SPAR FORWARD 27. A/C. THRESHOLD IS NEXT 6YE OR 20000 FC OR AMS A330 I09 A00"

Threshold Interval

T

113 800 FH

T

32 500 CY

T

12 YE

I

105 900 FH

I

30 200 CY

I

6 YE

T

24 YE

I

6 YE

References

Ctrl

Eff

N

AMM 572100-210-814

275

N

AMM 572100-210-814

294

Access panels :

523CB

623CB

Total access time :

0.68 Hrs

Skills :

0.20 MHrs

1 AF 572162-01-4S100

523 623

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 27. NOTE: CPCP

299 366

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [86 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572162-01-7S020

523 623

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 27. . . . . note:CPCP

Threshold Interval

T

132 000 FH

T

20 300 CY

T

12 YE

I

132 000 FH

I

20 300 CY

I

6 YE

References

Ctrl

N

AMM 572100-210-814

962 1019 1256 1266

623CB

Total access time :

0.68 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943 946

Access panels :

523CB

Eff

Page : STR - 57 [87 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572163-01-1

523 623

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE BETWEEN RIB 27 AND RIB 39. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS 4C-CHECK FROM APPROVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 572100-210-815

Eff 275 943 946

See note Check : NT

962 1019

NEXT

1256 1266

Access panels :

523EB 523MB 623KB

523FB 523NB 623LB

Total access time :

523GB 623EB 623MB

523HB 623FB 623NB

523JB 623GB

523KB 623HB

523LB 623JB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572163-01-1S100

523 623

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE BETWEEN RIB 27 AND RIB 39. note:CPCP

T

24 YE

I

6 YE

N

AMM 572100-210-815

294 299 366 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [88 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572164-01-10S020

541 542 641 642

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. TPS : TPS MUST NOT BE APPLIED PREP. : FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED;

Threshold Interval

T

83 700 FH

T

12 800 CY

T

12 YE

I

24 200 FH

I

3 700 CY

I

12 YE

References

Ctrl

N

AMM 572100-210-816

541HB 541QB 641GB 641PB 642DB

Total access time :

541JB 541RB 641HB 641QB

541KB 541SB 641JB 641RB

541LB 542AB 641KB 641SB

541MB 542BB 641LB 642AB

962 1019 1256 1266

541NB 542CB 641MB 642BB

15.00 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943 946

Access panels :

541GB 541PB 542DB 641NB 642CB

Eff

Page : STR - 57 [89 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572165-01-10

542 550 642 650

542 550 642 650

572165-01-5

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM FLANGES. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED;

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM FLANGES. NOTE: CPCP

Threshold Interval

T

150 200 FH

T

23 100 CY

T

12 YE

I

23 600 FH

I

3 600 CY

I

12 YE

T

136 800 FH

T

39 100 CY

T

12 YE

I

26 200 FH

I

7 500 CY

I

12 YE

References

Ctrl

N

AMM 572100-210-817

542FB 550CB 642HB 650EB

Total access time :

542GB 542HB 550DB 550EB 642JB 642KB 650FB 0.00 Hrs

542JB 550FB 650AB

542KB 642EB 650BB

962 1019 1256 1266

N

AMM 572100-210-817

550AB 642FB 650CB

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943 946

Access panels :

542EB 550BB 642GB 650DB

Eff

Page : STR - 57 [90 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572165-01-5S100

542 550 642 650

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM FLANGES. NOTE: CPCP

Threshold Interval

References

Ctrl

N

AMM 572100-210-817

Eff 294

T

24 YE

I

31 800 FH

299

I

8 800 CY

366

I

12 YE

T

113 800 FH

T

32 500 CY

I

113 800 FH

I

32 500 CY

Skills :

0.00 MHrs

1 AF 542 642

572166-01-4

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. PREP. : FUEL TANK DRAINED AND VENTED;

N

AMM 572100-220-806

Access panels :

542DB

542EB

Total access time :

642DB

642EB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [91 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572166-01-7S020

542 642

Task Title

Task code

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572100-220-806

Eff 943

T

132 000 FH

T

20 300 CY

I

132 000 FH

962

20 300 CY

1019

I

946

1256 1266

Access panels :

542DB

542EB

Total access time :

642DB

642EB

3.00 Hrs

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [92 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572171-02-1

541 542 550 641 642 650

Task code

Task Title

DI

MAIN STRUCTURE

DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB 39 AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION OF STR CUTOUTS EXCLUDING RIBS 18 & 23. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 572100-210-825

Eff 275 943 946 962 1019 1256 1266

Access panels :

541HB 541QB 542EB 550BB 641KB 641SB 642GB 650DB

541JB 541RB 542FB 550CB 641LB 642AB 642HB 650EB

Total access time :

541KB 541SB 542GB 550DB 641MB 642BB 642JB 650FB 0.00 Hrs

541LB 542AB 542HB 550EB 641NB 642CB 642KB

541MB 542BB 542JB 550FB 641PB 642DB 650AB

541NB 542CB 542KB 641HB 641QB 642EB 650BB

541PB 542DB 550AB 641JB 641RB 642FB 650CB

Skills :

0.00 MHrs

1 AF 572171-02-1S100

541 542 550 641 642 650

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB 39 AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION OF STR CUTOUTS EXCLUDING RIBS 18 & 23. note:CPCP

T

24 YE

I

12 YE

N

AMM 572100-210-825

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [93 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572174-01-4

541 542 641 642

Task code

Task Title

Threshold Interval

DI

T

60 000 FH

DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER CUTOUTS AND FORWARD FLAP TRACK BRACKETS. TPS : TPS MUST NOT BE APPLIED note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 20000 FC OR 50000 FH FROM APPROVE DATE OF AMS A330 I09 A00"

T

20 000 CY

MAIN STRUCTURE

T

12 YE

I

50 000 FH

I

20 000 CY

I

12 YE

References

Ctrl

Eff

N

AMM 572100-210-841

275

N

AMM 572100-210-841

294

Access panels :

541GB 641HB

541HB 641MB

Total access time :

541MB 641NB

541NB 641SB

541SB 642AB

542AB

641GB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 572174-01-4S100

541 542 641 642

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER CUTOUTS AND FORWARD FLAP TRACK BRACKETS. TPS : TPS MUST NOT BE APPLIED note:CPCP

T

24 YE

I

50 000 FH

299

I

20 000 CY

366

I

12 YE

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [94 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572174-01-6S020

541 542 641 642

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER CUTOUTS AND FORWARD FLAP TRACK BRACKETS. TPS : TPS MUST NOT BE APPLIED PREP. : FUEL TANK DRAINED AND VENTED; note:CPCP

Threshold Interval

T

60 000 FH

T

17 000 CY

T

12 YE

References

Ctrl

N

AMM 572100-210-841

Eff 943 946 962 1019

I

50 000 FH

I

17 000 CY

I

12 YE

T

70 300 FH

T

20 100 CY

294

I

42 700 FH

299

I

12 200 CY

366

1256 1266

Access panels :

541GB 641HB

541HB 641MB

Total access time :

541MB 641NB

541NB 641SB

541SB 642AB

542AB

641GB

6.00 Hrs

Skills :

1.60 MHrs

1 AF 572181-01-4S100

542 642

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26

N

AMM 572100-210-839

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [95 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

572184-01-4S100

541 641

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-4S100 PREP. : FUEL TANK DRAINED AND VENTED;

Threshold Interval

References

Ctrl

N

AMM 572100-210-867

Eff 275

T

81 400 FH

T

23 200 CY

294

I

29 400 FH

299

I

8 400 CY

366

T

81 400 FH

T

23 200 CY

I

29 400 FH

I

8 400 CY

T

24 YE

I

12 YE

Skills :

0.60 MHrs

1 AF 572184-02-4S100

541 641

SDI

MAIN STRUCTURE SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-4S100 PREP. : SEALANT REMOVAL AS PER NTM

N

AMM 572100-220-804

275

N

AMM 572600-210-801

294

Skills :

0.60 MHrs

1 NDT 572605-01-11

Issue No

:

Date

:

573 673

10 01/12/2013

DI

FITTINGS DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS).

Amendment No Date

: 01 : 06/09/2014

299 366

Page : STR - 57 [96 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572605-01-11S020

573 673

Task Title

Task code

DI

FITTINGS DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS). NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

116 700 FH

T

33 300 FC

T

12 YE

I

52 200 FH

I

14 900 CY

I

References

Ctrl

Eff

N

AMM 572600-210-801

275

N

AMM 572600-210-801

943

12 YE See note

Check : NT

R

572605-01-5S020

573 673

DI

FITTINGS DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS). NOTE: CPCP

T

123 300 FH

T

20 500 CY

T

12 YE

I

88 900 FH

I

13 600 CY

I

12 YE

946 962 1019 1256 1266

Access panels :

573BB

573FB

Total access time :

673BB 673FB 6.36 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [97 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572607-01-2S020

531 532 533 534 631 632 633 634

Task code

Task Title

DI

FITTINGS DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. PREP. : FIXED FLAP TRACK FAIRING Z531; FIXED FLAP TRACK FAIRING Z532; FIXED FLAP TRACK FAIRING Z533; FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z631; FIXED FLAP TRACK FAIRING Z632; FIXED FLAP TRACK FAIRING Z633; FIXED FLAP TRACK FAIRING Z634; note:CPCP

Threshold Interval

T

60 000 FH

T

17 000 CY

T

12 YE

I

50 000 FH

I

17 000 CY

I

12 YE

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

20 000 CY

References

Ctrl

N

AMM 572600-210-802

Eff 943 946 962 1019 1256 1266

Skills :

0.80 MHrs

1 AF 522 622

572608-02-1

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING.

N

AMM 572600-220-810

Access panels :

522AB 622CT

522AT

Total access time :

522BB

522CT

622AB

622AT

622BB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [98 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572608-02-2S020

522 622

Task code

Task Title

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. PREP. : ENGINE; LINKS; SLEEVES;

Threshold Interval

References

Ctrl

N

AMM 572600-220-810

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

17 000 CY

1019

I

946

1256 1266

Access panels :

522AB 622CT

522AT

Total access time :

522BB

522CT

622AB

622AT

622BB

0.40 Hrs

Skills :

0.00 MHrs

1 NDT R

541 641

572610-01-2

DI

FITTINGS DETAILED INSPECTION OF OUTER WING PYLON SPIGOT FITTING. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 572600-210-804

943 946

See note Check : NT

962 1019 1256 1266

Access panels :

453CL 463CR

453CR 464BL

Total access time :

454BL 464BR

454BR 464CL

454CL 464NR

454NR

463CL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [99 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572610-01-2S100

541 641

Task code

Task Title

DI

FITTINGS DETAILED INSPECTION OF OUTER WING PYLON SPIGOT FITTING. TPS : TPS MUST NOT BE APPLIED NOTE: CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572600-210-804

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 541 641

572610-02-2

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON SPIGOT FITTING. NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

50 000 FH

I

14 600 CY

N

275

Access panels :

454BL 464CR

454BR

Total access time :

454CL

454CR

464BL

464BR

464CL

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [100 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

572610-02-8S020

541 641

Task code

Task Title

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON SPIGOT FITTING.

Threshold Interval

References

Ctrl

N

AMM 572600-220-811

Eff 943

T

60 000 FH

T

17 000 CY

I

49 300 FH

962

7 500 CY

1019

I

946

1256 1266

Access panels :

454BL 464NR

454BR

Total access time :

454CL

454NR

464BL

464BR

464CL

1.68 Hrs

Skills :

0.20 MHrs

1 NDT R

541 641

572612-01-3

DI

FITTINGS DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. TPS : TPS MUST NOT BE APPLIED PREP. : PIPE SUPPORT BRACKET; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 572600-210-806

943 946

See note Check : NT

962 1019 1256 1266

Access panels :

454KL 464MR

454KR

Total access time :

454ML

454MR

464KL

464KR

464ML

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [101 / 188] ATA

: 57


57

WINGS

Task Number

Zone

572612-01-3S100

541 641

Task code

Task Title

DI

FITTINGS DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. TPS : TPS MUST NOT BE APPLIED PREP. : PIPE SUPPORT BRACKET; NOTE: CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 572600-210-806

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 541 641

572612-02-3

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-1 PREP. : PIPE SUPPORT BRACKET; NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

24 300 FH

I

6 900 CY See note

N

AMM 572600-270-805

Access panels :

464BL 474FR

464BR

Total access time :

464FL

464FR

474BL

474BR

474FL

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [102 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572612-02-9S020

541 641

Task code

Task Title

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-4S020 PREP. : PIPE SUPPORT BRACKET;

Threshold Interval

References

Ctrl

N

AMM 572600-270-805

Eff 943

T

60 000 FH

T

17 000 CY

I

42 300 FH

962

6 500 CY

1019

I

946

1256 1266

Access panels :

454BL 464MR

454BR

Total access time :

454ML

454MR

464BL

464BR

464ML

5.10 Hrs

Skills :

0.20 MHrs

1 NDT 541 641

572612-03-1

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-3 PREP. : BEARING REMOVAL; ENGINE, LINKS AND SLEEVES, PIPE SUPPORT BRACKET REMOVED / DISPLACED; "NOTE: THRESHOLD IS NEXT 4C CHECK

T

60 000 FH

T

20 000 CY

I

50 000 FH

N

AMM 572600-210-811

I


Access panels :

454CL 464CR

454CR 464DL

Total access time :

454DL 464DR

454DR 464FL

454FL 464FR

454FR

464CL

0.00 Hrs

Skills :

0.20 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [103 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

572612-03-4S020

541 641

Task Title

Task code

SDI

FITTINGS SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT ATTACHMENT FITTING. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-9S020 PREP. : BEARING REMOVAL; ENGINE, LINKS AND SLEEVES, PIPE SUPPORT BRACKET REMOVED / DISPLACED;

Threshold Interval

References

Ctrl

N

AMM 572600-210-811

Eff 943

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

15 400 CY

1019

I

946

1256 1266

Skills :

0.20 MHrs

1 NDT 571 671

572649-01-1

DI

OUTER WING - FITTINGS DETAILED INSPECTION OF MAIN LANDING GEAR RIB 6 AFT BEARING LUGS

T

5 YE

I

1 500 FH

I

300 CY

T

60 000 FH

T

17 000 CY

T

12 YE

B1 AMM 572600-220-821 EAD 2007-0247E ISB 57-3096

ALL

Skills :

0.30 MHrs

1 AF R

573001-01-10S020

550 650

DI

WING TIP SPECIAL DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTO SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AN BUTTSTRAPS. PREP. : WINGTIP LEADING EDGE ASSY; WINGTIP NAVIGATION LIGHT; WINGTIP STROBE LIGHT;

I

39 500 FH

I

6 000 CY

I

12 YE

N

AMM 573000-280-801

946 962 1019 1256 1266

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [104 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

573002-01-3S020

500 600

Task Title

Task code

DI

WING TIP DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE.

Threshold Interval

References

Ctrl

N

AMM 573000-210-806

Eff 943

T

60 000 FH

T

17 000 CY

I

39 500 FH

962

6 000 CY

1019

I

946

1256 1266

Skills :

0.30 MHrs

1 AF R

535 635

573003-01-1

DI

WING TIP DETAILED INSPECTION OF WINGTIP TO WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). PREP. : WINGLET; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 573000-210-802

275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 573003-01-1S100

535 635

DI

WING TIP DETAILED INSPECTION OF WINGTIP TO WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). PREP. : WINGLET; note:CPCP

T

24 YE

I

12 YE

N

AMM 573000-210-802

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [105 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

573003-02-8S020

535 635

Task Title

Task code

SDI


Threshold Interval

References

Ctrl

N

AMM 573000-220-806

Eff 943

T

122 800 FH

T

18 800 CY

I

50 300 FH

962

7 700 CY

1019

I

946

1256 1266

Skills :

0.80 MHrs

1 NDT R

535 635

573004-01-1

DI

WING TIP DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; YE"" "

T

12 YE

I

12 YE

N

AMM 573000-210-803

275 943 946 962 1019

THRESHOLD IS ""20

1256 1266

Skills :

0.20 MHrs

1 AF 573004-01-1S100

535 635

DI

WING TIP DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. note:CPCP

T

24 YE

I

12 YE

N

AMM 573000-210-803

299 366

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [106 / 188] ATA

: 57


57

WINGS

Task Number

Zone

573005-01-1

535 635

Task code

Task Title

DI

WING TIP DETAILED INSPECTION OF WINGTIP TO WINGLET JOINT BOLTS. PREP. : JOINT BOLTS; note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 573000-210-804

ALL

N

AMM 574100-210-801

275

Access panels :

535AB

535BB

Total access time :

635AB 635BB 0.00 Hrs

Skills :

0.00 MHrs

1 AF R

521 522 523 621 622 623

574101-01-1

DI


DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TRACK RIBS 1 TO 16. PREP. : SLATS EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

943 946

See note

962

Check : NT

1019 1256 1266

Access panels :

521BB 522LB 523JB 621JB 623CB

521CB 522NB 523LB 622CB 623EB

Total access time :

521DB 522RB 523NB 622JB 623GB

521GB 522TB 621BB 622LB 623JB

521JB 523CB 621CB 622NB 623LB

522CB 523EB 621DB 622RB 623NB

522JB 523GB 621GB 622TB

0.00 Hrs

Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [107 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574101-01-1S100

521 522 523 621 622 623

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TRACK RIBS 1 TO 16. PREP. : SLATS EXTENDED; note:CPCP

Threshold Interval

T

20 YE

I

12 YE

References

Ctrl

N

AMM 574100-210-801

Eff 294 299 366

Skills :

0.00 MHrs

1 AF 521 522 523 621 622 623

574102-01-4

SDI

INBOARD LEADING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK RIBS 1 TO TRACK RIB 11.

T

83 200 FH

T

23 700 CY

I

21 000 FH

I

6 000 CY

N

AMM 574100-210-802

Access panels :

521BB 522LB 621DB 622RB

521CB 522NB 621GB 622TB

Total access time :

521DB 522RB 621JB 623CB

521GB 522TB 622CB

521JB 523CB 622JB

522CB 621BB 622LB

522JB 621CB 622NB

0.00 Hrs

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [108 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

574102-01-8S020

521 522 523 621 622 623

Task code

Task Title

SDI

INBOARD LEADING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK RIBS 1 TO TRACK RIB 11.

Threshold Interval

References

Ctrl

N

AMM 574100-210-802

Eff 943

T

104 700 FH

T

16 100 CY

I

47 600 FH

962

7 300 CY

1019

I

946

1256 1266

Skills :

1.20 MHrs

1 NDT 521 522 523 621 622 623

574103-02-1

DI

T

83 200 FH

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. NOTE: CPCP NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 13600 FC OR 48900 FH FROM APPROVE DATE OF AMS A330 I09 A00"

T

23 700 CY


T

12 YE

I

12 500 FH

I

3 500 CY

I

12 YE

N

AMM 574100-210-811

See note Access panels :

521DB 522GB 621FB 622HB

521FB 522HB 621GB 622JB

Total access time :

521GB 522JB 622AB 622NB 0.00 Hrs

522AB 522NB 622BB 622RB

522BB 522RB 622CB 622UB

522CB 522UB 622EB

522EB 621DB 622GB

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [109 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

574103-02-1S100

521 522 523 621 622 623

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. NOTE: CPCP

Threshold Interval

References

Ctrl

N

AMM 574100-210-811

Eff 294

T

24 YE

I

12 500 FH

299

I

3 500 CY

366

I

12 YE

T

104 700 FH

T

16 100 CY

T

12 YE

Skills :

0.00 MHrs

1 AF R

574103-02-4S020

521 522 523 621 622 623

001256INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. note:CPCP

DI

I

21 300 FH

I

3 200 CY

I

12 YE

N

AMM 574100-210-811

946 962 1019 1256 1266

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [110 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574104-01-4

521 522 523 621 622 623

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES.

Threshold Interval

T

83 200 FH

T

23 700 CY

I

21 500 FH

I

6 100 CY

References

Ctrl

N

AMM 574100-210-804

Access panels :

521AB 521HB 522FB 522NB 523FB 523NB 621FB 622DB 622LB 623DB 623LB

521BB 521JB 522GB 522PB 523GB 523PB 621GB 622EB 622MB 623EB 623MB

Total access time :

521CB 522AB 522HB 522RB 523HB 621AB 621HB 622FB 622NB 623FB 623NB 0.00 Hrs

521DB 522BB 522JB 522SB 523JB 621BB 621JB 622GB 622PB 623GB 623PB

521EB 522CB 522KB 523CB 523KB 621CB 622AB 622HB 622RB 623HB

521FB 522DB 522LB 523DB 523LB 621DB 622BB 622JB 622SB 623JB

521GB 522EB 522MB 523EB 523MB 621EB 622CB 622KB 623CB 623KB

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [111 / 188] ATA

: 57

Eff 275


R

57

WINGS

Task Number

Zone

574104-01-7S020

521 522 523 621 622 623

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES.

Threshold Interval

References

Ctrl

N

AMM 574100-210-804

Eff 943

T

104 700 FH

T

16 100 CY

I

42 600 FH

962

6 500 CY

1019

I

946

1256 1266

Skills :

1.20 MHrs

1 AF 521 522 523 621 622 623

574105-01-3

DI


DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 7600 FC OR 27300 FH FROM APPROVE DATE OF AMS A330 I09 A00"

T

60 000 FH

T

20 000 CY

T

12 YE

I

21 100 FH

I

6 000 CY

I

12 YE

N

AMM 574100-210-805

Access panels :

521BB 522LB 523JB 621JB 623CB

521CB 522NB 523LB 622CB 623EB

Total access time :

521DB 522RB 523NB 622JB 623GB 0.00 Hrs

521GB 522TB 621BB 622LB 623JB

521JB 523CB 621CB 622NB 623LB

522CB 523EB 621DB 622RB 623NB

522JB 523GB 621GB 622TB

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [112 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

574105-01-3S100

521 522 523 621 622 623

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16.

Threshold Interval

References

Ctrl

N

AMM 574100-210-805

Eff 294

T

24 YE

I

21 100 FH

299

I

6 000 CY

366

I

12 YE

T

60 000 FH

T

17 000 CY

T

12 YE

Skills :

0.00 MHrs

1 AF R

574105-01-7S020

521 522 523 621 622 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. note:CPCP

I

49 000 FH

I

7 500 CY

I

12 YE

N

AMM 574100-210-805

946 962 1019 1256 1266

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [113 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574107-01-2

521 522 523 621 622 623

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12. note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574100-210-807

Eff 275 943 946 962 1019 1256 1266

Access panels :

521FB 522DB 522LB 523CB 622AB 622HB 622QB

521GB 522EB 522MB 523DB 622BB 622JB 622RB

Total access time :

521HB 522FB 522NB 523EB 622CB 622KB 622SB 0.00 Hrs

521JB 522GB 522PB 621FB 622DB 622LB 623CB

522AB 522HB 522QB 621GB 622EB 622MB 623DB

522BB 522JB 522RB 621HB 622FB 622NB 623EB

522CB 522KB 522SB 621JB 622GB 622PB

Skills :

0.00 MHrs

1 AF 574107-01-2S100

521 522 523 621 622 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12. note:CPCP

T

24 YE

I

12 YE

N

AMM 574100-210-807

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [114 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574107-02-7S020

521 522 523 621 622 623

Task Title

Task code

SDI

INBOARD LEADING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

Threshold Interval

References

Ctrl

N

AMM 574100-210-812

Eff 943

T

100 300 FH

T

15 400 CY

I

87 300 FH

962

13 400 CY

1019

I

946

1256 1266

Skills :

2.40 MHrs

1 NDT R

574110-02-4S020

500 600

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. TPS : TPS MUST NOT BE APPLIED note:CPCP

T

137 100 FH

T

21 000 CY

T

6 YE

N

AMM 574100-210-813

943 946 962 1019

I

77 700 FH

I

11 900 CY

I

6 YE

T

75 600 FH

T

21 600 CY

294

I

67 000 FH

299

I

19 100 CY

366

1256 1266

Skills :

0.40 MHrs

1 AF 500 600

574111-01-4

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39. MSN 255-SAMPLE A/C FOUND CORROSION, PROGRAM CONCEPT CHANGE TO 100% ; NEXT DUE IS NEXT 4C-CHECK FROM APPROVE DATE OF AMS A330 I09 A00

N

AMM 574100-210-821

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [115 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

574111-01-7S020

500 600

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39.

Threshold Interval

References

Ctrl

N

AMM 574100-210-821

Eff 943

T

105 200 FH

T

16 100 CY

I

105 200 FH

962

16 100 CY

1019

I

946

1256 1266

R

523 623

574112-01-1

DI

000962INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE HOLD DOWN RIB BETWEEN SLAT TRACK RIB 15 AND SLAT TRACK 16, AREA OF SLAT TRACK BRAKE FITTING note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 574100-210-810

275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

523LB

523NB

Total access time :

623LB

623NB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 574112-01-1S100

523 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE HOLD DOWN RIB BETWEEN SLAT TRACK RIB 15 AND SLAT TRACK 16, AREA OF SLAT TRACK BRAKE FITTING note:CPCP

T

24 YE

I

12 YE

N

AMM 574100-210-810

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [116 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574114-03-5S020

500 600

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.

Threshold Interval

References

Ctrl

N

AMM 574100-210-830

Eff 943

T

117 300 FH

T

18 000 CY

I

78 200 FH

962

12 000 CY

1019

I

946

1256 1266

Skills :

2.00 MHrs

1 AF R

574115-02-6S020

522 622

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11 AND RIB 24 TO RIB 26. note:CPCP

T

60 000 FH

T

17 000 CY

T

12 YE

I

50 000 FH

I

11 200 CY

I

12 YE

N

AMM 574100-210-844

946 962 1019 1256 1266

Access panels :

522AB

522BB

Total access time :

522CB

622AB

622BB

622CB

1.32 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [117 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574116-01-4

521 522 523 621 622 623

Task code

Task Title

Threshold Interval

DI

T

88 000 FH

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND SLAT HOLD DOWN RIBS. NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 14600 FC OR 50000 FH FROM APPROVE DATE OF AMS A330 I09 A00"

T

25 100 CY


T

12 YE

I

62 100 FH

I

17 700 CY

I

12 YE

References

Ctrl

N

AMM 574100-210-824 MRB 574116-01-4

Access panels :

521AB 521HB 522FB 522NB 523EB 523MB 621EB 622CB 622KB 622SB 623JB

521BB 521JB 522GB 522PB 523FB 523NB 621FB 622DB 622LB 623CB 623KB

Total access time :

521CB 522AB 522HB 522QB 523GB 523PB 621GB 622EB 622MB 623DB 623LB 0.00 Hrs

521DB 522BB 522JB 522RB 523HB 621AB 621HB 622FB 622NB 623EB 623MB

521EB 522CB 522KB 522SB 523JB 621BB 621JB 622GB 622PB 623FB 623NB

521FB 522DB 522LB 523CB 523KB 621CB 622AB 622HB 622QB 623GB 623PB

521GB 522EB 522MB 523DB 523LB 621DB 622BB 622JB 622RB 623HB

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [118 / 188] ATA

: 57

Eff 275


57

WINGS

Task Number

Zone

574116-01-4S100

521 522 523 621 622 623

Task Title

Task code

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND SLAT HOLD DOWN RIBS.

Threshold Interval

References

Ctrl

N

AMM 574100-210-824

Eff 294

T

24 YE

I

62 100 FH

299

I

17 700 CY

366

I

12 YE

T

125 200 FH

T

19 200 CY

T

12 YE

Skills :

1.20 MHrs

1 AF R

574116-01-7S020

521 522 523 621 622 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND SLAT HOLD DOWN RIBS. note:CPCP

I

102 200 FH

I

15 700 CY

I

12 YE

N

AMM 574100-210-824

946 962 1019 1256 1266

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

943

Page : STR - 57 [119 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574119-01-1

521 523 621 623

Task code

Task Title

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIBS 1 AND 2 AND TRACK RIBS 13 TO 16. note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574100-210-825

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

521BB 621GB

521GB 623GB

Total access time :

523GB 523JB 623JB 623LB 0.00 Hrs

523LB 623NB

523NB

621BB

Skills :

0.00 MHrs

1 AF 574119-01-1S100

521 523 621 623

DI

INBOARD LEADING EDGE DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIBS 1 AND 2 AND TRACK RIBS 13 TO 16. note:CPCP

T

24 YE

I

12 YE

N

AMM 574100-210-825

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [120 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574301-01-3

511 611

Task Title

Task code

SDI

SLAT 1 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3, VISIBLE PART OF ROLLER CONTACT AREA. PREP. : SLAT FULLY EXTENDED; NOTE: THRESHOLD NEXT 4C CHECK

Threshold Interval

References

Ctrl

N

AMM 574300-220-801

Eff 275

T

60 000 FH

T

20 000 CY

943

I

18 300 FH

946

I

5 900 CY

962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT 511 611

574303-01-1

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

T

12 YE

I

6 YE

N

AMM 574300-210-801

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [121 / 188] ATA

: 57

ALL


R

57

WINGS

Task Number

Zone

574304-01-1

511 611

Task Title

Task code

SDI

SLAT 1

SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME A TASK 574304-03-2. TPS : TPS MUST NOT BE APPLIED"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE""" PREP. : SLAT FULLY EXTENDED; NOTE: CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574300-210-802

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT 574304-01-1S100

511 611

SDI

SLAT 1 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME A TASK 574304-03-2S100 TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; NOTE: CPCP

T

24 YE

I

12 YE

N

AMM 574300-210-802

299 366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [122 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574304-03-2

511 611

Task Title

Task code

DI

SLAT 1

DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574300-210-809

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574304-03-2S100

511 611

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH PREP. : SLAT FULLY EXTENDED; note:CPCP

T

24 YE

I

12 YE

N

AMM 574300-210-809

294 299 366

Skills :

0.00 MHrs

1 AF R

511 611

574305-01-1

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1 HOLD DOWN BRACKET, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 574300-210-804

943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [123 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574305-01-1S100

511 611

Task Title

Task code

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1 HOLD DOWN BRACKET, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 574300-210-804

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

511 611

574307-01-1

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 ACTUATION LINK CONNECTION BOLTS LH/RH. PREP. : REMOVAL OF THE BOLTS ONE AT A TIME.; SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

T

12 YE

I

6 YE

N

AMM 574300-210-806

943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Access panels :

521DB

521GB

Total access time :

621DB

621GB

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [124 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574307-01-1S100

511 611

Task Title

Task code

DI

SLAT 1 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 ACTUATION LINK CONNECTION BOLTS LH/RH. PREP. : REMOVAL OF THE BOLTS ONE AT A TIME.; SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

24 YE

I

6 YE

References

Ctrl

N

AMM 574300-210-806

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

512 612

574401-01-3

SDI

SLAT 2 SPECIAL DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

N

AMM 574400-210-801

275

T

60 000 FH

T

20 000 CY

943

I

20 300 FH

946 962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT R

512 612

574401-02-1

DI

SLAT 2 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

T

12 YE

I

6 YE

N

AMM 574400-220-801

943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [125 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574401-02-1S100

512 612

Task Title

Task code

DI

SLAT 2 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

24 YE

I

6 YE

References

Ctrl

N

AMM 574400-220-801

Eff 294 299 366 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 512 612

574403-01-1

DI

SLAT 2 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

N

AMM 574400-210-802

ALL

N

AMM 574400-250-803

275

T

12 YE

I

6 YE

T

60 000 FH

T

20 000 CY

943

I

23 300 FH

946

Skills :

0.00 MHrs

1 AF R

512 612

574404-01-1

SDI

SLAT 2 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [126 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574404-02-3

512 612

Task Title

Task code

DI

SLAT 2 DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH PREP. : SLAT FULLY EXTENDED; MSN 255-SAMPLE A/C FOUND CORROSION, PROGRAM CONCEPT CHANGE TO 100% ; NEXT DUE IS NEXT 4C-CHECK FROM APPROVE DATE OF AMS A330 I09 A00

Threshold Interval

T

60 000 FH

T

20 000 CY

T

12 YE

I

23 300 FH

I

6 600 CY

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 574400-210-804

ALL

N

AMM 574400-210-803

275

Skills :

0.00 MHrs

1 AF R

512 612

574404-03-2

DI

SLAT 2

SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATI INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [127 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574404-03-2S100

512 612

Task Title

Task code

DI

SLAT 2 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATI INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 574400-210-803

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

512 612

574405-01-1

DI


T

12 YE

I

12 YE

N

AMM 574400-210-805

275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574405-01-1S100

512 612

DI


T

24 YE

I

12 YE

N

AMM 574400-210-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [128 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574501-01-1

513 613

Task Title

Task code

DI

SLAT 3 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 574500-210-801

Eff 275 943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Skills :

0.00 MHrs

1 AF 574501-01-1S100

513 613

DI

SLAT 3 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

T

24 YE

I

6 YE

N

AMM 574500-210-801

294 299 366

Skills :

0.00 MHrs

1 AF R

513 613

574501-02-4

SDI

SLAT 3 SPECIAL DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

N

AMM 574500-220-801

60 000 FH

T

20 000 CY

943

I

24 400 FH

946 962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : STR - 57 [129 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574503-01-1

513 613

Task Title

Task code

DI

SLAT 3 DETAILED INSPECTION OF SLAT 3, TRACKS 7 TO 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

References

Ctrl

Eff

N

AMM 574500-210-802

ALL

N

AMM 574500-210-803

275

T

12 YE

I

6 YE

T

60 000 FH

T

20 000 CY

943

I

23 300 FH

946

I

6 600 CY See note

1019

Skills :

0.00 MHrs

1 AF R

513 613

574504-01-1

SDI

SLAT 3 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

962 1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [130 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574504-02-4

513 613

Task Title

Task code

DI

SLAT 3

DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH PREP. : SLAT FULLY EXTENDED; NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 6600 FC OR 23300 FH FROM APPROVE DATE OF AMS A330 I09 A00"

Threshold Interval

References

Ctrl

N

AMM 574500-210-804

Eff 275

T

60 000 FH

T

20 000 CY

943

T

12 YE

946

I

23 300 FH

I

6 600 CY

I

12 YE

962 1019 1256 1266


0.00 MHrs

1 AF 574504-02-4S100

513 613

513 613

574504-03-1

DI

SLAT 3 DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH PREP. : SLAT FULLY EXTENDED;

SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, INTERNAL, LH/RH.

24 YE

I

12 YE

N

AMM 574500-210-804

294 299 366

SDI

SLAT 3

T

T

12 YE

I

12 YE

N

AMM 574500-210-803

275 943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [131 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574504-03-1S100

513 613

513 613

574505-01-1

Task Title

Task code

SDI

SLAT 3 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, INTERNAL, LH/RH.

T

24 YE

I

12 YE

References

Ctrl

N

AMM 574500-210-803

Eff 294 299 366

DI

SLAT 3

Threshold Interval

DETAILED INSPECTION OF SLAT 3 HOLD DOWN BRACKET, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

T

12 YE

I

12 YE

N

AMM 574500-210-805

275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574505-01-1S100

513 613

DI


T

24 YE

I

12 YE

N

AMM 574500-210-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [132 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574601-01-3

514 614

Task Title

Task code

SDI

SLAT 4 SPECIAL DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

N

AMM 574600-220-801

Eff 275

T

60 000 FH

T

20 000 CY

943

I

23 300 FH

946

I

3 500 CY See note

1019

962 1256

Check : NT

1266

Skills :

0.00 MHrs

1 NDT R

514 614

574601-02-1

DI

SLAT 4 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

T

12 YE

I

6 YE

N

AMM 574600-210-801

275 943 946 962 1019

THRESHOLD IS NEXT

1256 1266

Skills :

0.00 MHrs

1 AF 574601-02-1S100

514 614

DI

SLAT 4 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

T

24 YE

I

6 YE

N

AMM 574600-210-801

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [133 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574603-01-2

514 614

Task Title

Task code

DI

SLAT 4 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

References

Ctrl

Eff

N

AMM 574600-210-802

ALL

N

AMM 574600-250-802

275

T

12 YE

I

6 YE

T

60 000 FH

T

20 000 CY

943

I

23 300 FH

946

I

6 600 CY See note

1019

Skills :

0.00 MHrs

1 AF R

514 614

574604-01-1

SDI

SLAT 4 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT HOLD DOWN RIB STATIONS, EXTERNAL LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP

962 1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [134 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574604-02-3

514 614

Task Title

Task code

DI

SLAT 4

DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 6600 FC OR 23300 FH FROM APPROVE DATE OF AMS A330 I09 A00"

Threshold Interval

References

Ctrl

N

AMM 574600-210-804

Eff 275

T

60 000 FH

T

20 000 CY

943

T

12 YE

946

I

23 300 FH

I

6 600 CY

I

12 YE

962 1019 1256 1266


0.00 MHrs

1 AF 574604-02-3S100

514 614

514 614

574604-03-1

DI


SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS, INTERNAL, LH/RH.

24 YE

I

12 YE

N

AMM 574600-210-804

294 299 366

SDI

SLAT 4

T

T

12 YE

I

12 YE

N

AMM 574600-210-803

275 943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [135 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574604-03-1S100

514 614

514 614

574605-01-1

Task Title

Task code

SDI


T

24 YE

I

12 YE

References

Ctrl

N

AMM 574600-210-803

Eff 294 299 366

DI

SLAT 4

Threshold Interval


T

12 YE

I

12 YE

N

AMM 574600-210-805

275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574605-01-1S100

514 614

DI


T

24 YE

I

12 YE

N

AMM 574600-210-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [136 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574701-01-1

515 615

Task Title

Task code

DI

SLAT 5 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; 4C CHECK FROM APPOVE DATE

Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 574700-210-801

Eff 275 943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Skills :

0.00 MHrs

1 AF 574701-01-1S100

515 615

DI

SLAT 5 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

T

24 YE

I

6 YE

N

AMM 574700-210-801

294 299 366

Skills :

0.00 MHrs

1 AF R

515 615

574701-02-4

SDI

SLAT 5 SPECIAL DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

N

AMM 574700-220-801

60 000 FH

T

20 000 CY

943

I

24 400 FH

946 962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : STR - 57 [137 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574703-01-1

515 615

Task Title

Task code

DI

SLAT 5 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 574700-210-802

ALL

N

AMM 574700-210-803

275

Skills :

0.00 MHrs

1 AF R

515 615

574704-01-1

SDI

SLAT 5 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00;THRESHOLD IS ""20 YE""" note:CPCP

943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [138 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574704-01-1S100

515 615

Task Title

Task code

SDI

SLAT 5 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 574700-210-803

Eff 294 299 366

Skills :

0.00 MHrs

1 NDT R

515 615

574705-01-1

DI


T

12 YE

I

12 YE

N

AMM 574700-210-805

275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574705-01-1S100

515 615

DI


T

24 YE

I

12 YE

N

AMM 574700-210-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [139 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574801-01-1

516 616

Task Title

Task code

DI


Threshold Interval

T

12 YE

I

6 YE

References

Ctrl

N

AMM 574800-210-801

Eff 275 943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Skills :

0.00 MHrs

1 AF 574801-01-1S100

516 616

DI


T

24 YE

I

6 YE

N

AMM 574800-210-801

294 299 366

Skills :

0.00 MHrs

1 AF R

516 616

574801-02-3

SDI

SLAT 6 SPECIAL DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND 14; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT4C CHECK

N

AMM 574800-220-801

60 000 FH

T

20 000 CY

943

I

20 800 FH

946 962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

T

Page : STR - 57 [140 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574803-01-1

516 616

Task Title

Task code

DI


Threshold Interval

T

12 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 574800-210-802

ALL

N

AMM 574800-210-803

275

Skills :

0.00 MHrs

1 AF R

516 616

574804-03-2

DI

SLAT 6

SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574804-03-2S100

516 616

DI

SLAT 6 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS INTERNAL, LH/RH. TPS : TPS MUST NOT BE APPLIED PREP. : SLAT FULLY EXTENDED; note:CPCP

T

24 YE

I

12 YE

N

AMM 574800-210-803

299 366

Skills :

0.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [141 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

574805-01-1

516 616

Task Title

Task code

DI


Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574800-210-805

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 574805-01-1S100

516 616

DI


T

24 YE

I

12 YE

N

AMM 574800-210-805

294 299 366

Skills :

0.00 MHrs

1 AF R

517 617

574901-01-1

DI


T

12 YE

I

6 YE

N

AMM 574900-210-801

943 946 962 1019 1256

THRESHOLD IS NEXT

1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : STR - 57 [142 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574901-01-1S100

517 617

Task Title

Task code

DI


Threshold Interval

T

24 YE

I

6 YE

References

Ctrl

N

AMM 574900-210-801

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

517 617

574901-02-3

SDI

SLAT 7 SPECIAL DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND 16; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. PREP. : SLAT FULLY EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C CHECK

N

AMM 574900-220-801

275

T

60 000 FH

T

20 000 CY

943

I

20 800 FH

946 962

I


1019 1256 1266

Skills :

0.00 MHrs

1 NDT 517 617

574903-01-1

DI


T

12 YE

I

6 YE

N

AMM 574900-210-802

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [143 / 188] ATA

: 57

ALL


R

57

WINGS

Task Number

Zone

574904-01-1

517 617

Task Title

Task code

SDI

SLAT 7 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN CONNECTIONS AT TRACK RIBS AND HOLD DOWN RIB STATIONS EXTERNAL, LH/RH. PREP. : SLAT FULLY EXTENDED; note:CPCP NOTE: THRESHOLD FOR MSN 275 IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

N

AMM 574900-250-803

Eff 275

T

60 000 FH

T

20 000 CY

943

I

23 300 FH

946

I

6 600 CY See note

1019

962 1256

Check : NT

1266

Skills :

0.00 MHrs

1 NDT R

574904-02-4S020

574904-02-4S100

Issue No

:

Date

:

517 617

517 617

10 01/12/2013

DI


DI


Amendment No Date

: 01 : 06/09/2014

N

AMM 574900-210-804

275

T

60 000 FH

T

20 000 CY

943

T

12 YE

946

I

23 300 FH

I

6 600 CY

I

12 YE

T

24 YE

I

12 YE

962 1019 1256 1266

N

AMM 574900-210-804

294 299 366

Page : STR - 57 [144 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574904-03-1

517 617

Task Title

Task code

SDI


Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 574900-210-803

Eff 275 943 946 962 1019 1256 1266

574904-03-1S100

R

517 617

517 617

574905-01-1

SDI



24 YE

I

12 YE

N

AMM 574900-210-803

299

T

12 YE

I

12 YE

N

AMM 574900-210-805

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

946

See note Check : NT

962 1019 1256 1266

0.00 MHrs

: 01 : 06/09/2014

275 943

Skills :

1 AF

294 366

DI

SLAT 7

T

Page : STR - 57 [145 / 188] ATA

: 57


57

WINGS

Task Number

Zone

574905-01-1S100

517 617

Task Title

Task code

DI


Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 574900-210-805

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

573 673

575001-01-1


DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILER 1 ACTUATOR SUPPORT FITTING. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"

T

12 YE

I

12 YE

N

AMM 575000-210-801

275 943 946

See note

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575001-01-1S100

573 673

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILER 1 ACTUATOR SUPPORT FITTING. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-801

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [146 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575002-01-1

573 673

Task code

Task Title

DI

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR SPAR OR FALSE REAR SPAR AND SPOILER 1 HINGE FITTINGS. note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-802

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

573BB

573DB

Total access time :

573FB 673BB 0.00 Hrs

673DB

673FB

Skills :

0.00 MHrs

1 AF 575002-01-1S100

573 673

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR SPAR OR FALSE REAR SPAR AND SPOILER 1 HINGE FITTINGS. note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-802

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [147 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575003-01-1

574 674

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 PLACES) LUGS AND ATTACHMENT TO BOTTOM SKIN OVERHANG. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-803

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575003-01-1S100

574 674

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 PLACES) LUGS AND ATTACHMENT TO BOTTOM SKIN OVERHANG. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-803

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [148 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575004-01-1

574 674

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN OVERHANG. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-220-868

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575004-01-1S100

574 674

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN OVERHANG. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-220-868

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [149 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575005-01-1

574 674

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS AND OUTER LINK HINGE RIBS (16 PLACES). PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-805

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575005-01-1S100

574 674

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS AND OUTER LINK HINGE RIBS (16 PLACES). PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [150 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575006-01-1

575 675

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AND OUTBOARD AILERON JACK BRACKETS (4 PLACES) AT LUG AND ATTACHMENT TO TOP AND BOTTOM SKIN OVERHANGS (INTERNAL AND EXTERNAL). note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-806

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

575AB

575DB

Total access time :

675AB 675DB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 575006-01-1S100

575 675

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AND OUTBOARD AILERON JACK BRACKETS (4 PLACES) AT LUG AND ATTACHMENT TO TOP AND BOTTOM SKIN OVERHANGS (INTERNAL AND EXTERNAL). note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-806

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [151 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575008-01-1

573 574 673 674

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIB 10 FLAP CRUISE ROLLERS SUPPORT. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-807

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575008-01-1S100

573 574 673 674

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIB 10 FLAP CRUISE ROLLERS SUPPORT. PREP. : FLAPS EXTENDED; SPOILERS EXTENDED; note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-807

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [152 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575009-01-1

573 673

Task code

Task Title

GVI

TRAILING EDGE AND TRAILING EDGE DEVICE GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, TOP AND BOTTOM SKIN OVERHANGS AND OUTER FLAP CRUISE ROLLER SUPPORT ATTACHMENT TO TRAILING EDGE RIB 10. note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

80 500 FH

T

23 000 CY

T

12 YE

I

23 900 FH

I

6 800 CY

I

12 YE

References

Ctrl

Eff

N

AMM 575000-210-843

ALL

N

AMM 575000-210-808

275

Access panels :

573BB 673CB

573CB 673DB

Total access time :

573DB 673EB

573EB 673FB

573FB 673GB

573GB

673BB

0.00 Hrs

Skills :

0.00 MHrs

1 AF 573 673

575010-01-4

DI


DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE REAR SPAR FORWARD AND AFT FACES. NOTE: CPCP NOTE: MSN 275 BECOME SAMPLE A/C. THRESHOLD IS "20 YE" OR "NEXT 7500 FC OR 27000 FH FROM APPROVE DATE OF AMS A330 I09 A00" Access panels :

573BB

573DB

Total access time :

573FB 673BB 0.00 Hrs

673DB

673FB

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [153 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575010-01-4S100

573 673

Task code

Task Title

DI

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE REAR SPAR FORWARD AND AFT FACES. NOTE: CPCP

Threshold Interval

T

24 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-808

Eff 294 299 366

Skills :

0.00 MHrs

1 AF R

575010-01-7S020

573 673

DI

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE REAR SPAR FORWARD AND AFT FACES. note:CPCP

T

105 800 FH

T

16 200 CY

T

12 YE

N

AMM 575000-210-808

943 946 962 1019

I

69 000 FH

I

10 600 CY

I

12 YE

T

98 500 FH

T

15 100 CY

I

48 400 FH

962

7 400 CY

1019

1256 1266

Access panels :

573BB

573DB

Total access time :

573FB

673BB

673DB

673FB

6.88 Hrs

Skills :

0.40 MHrs

1 AF R

575011-01-9S020

500 600

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

DI

I

N

AMM 575000-210-828

943 946

1256 1266

Skills :

0.40 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [154 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575012-01-7S020

500 600

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

Threshold Interval

References

Ctrl

N

AMM 575000-210-809

Eff 943

T

92 900 FH

T

14 300 CY

I

29 900 FH

962

4 600 CY

1019

I

946

1256 1266

Skills :

0.00 MHrs

1 AF 500 600

575013-01-2

SDI

WING BOTTOM SKIN AT RIB 6 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6. "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT ""14900 FC OR 50000 FH "" FROM APPROVE DATE"

T

60 000 FH

T

20 000 CY

I

50 000 FH

N

AMM 575000-210-810

275

N

AMM 575000-210-810

943

I


Skills :

0.20 MHrs

1 NDT R

575013-01-5S020

500 600

SDI

WING BOTTOM SKIN AT RIB 6 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

T

60 000 FH

T

17 000 CY

I

50 000 FH

962

I

8 300 CY

1019

946

1256 1266

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [155 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575014-01-4

570 670

Task Title

Task code

SDI

TRAILING EDGE SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG REINFORCING. "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT ""17700 FC OR 50000 FH "" FROM APPROVE DATE"

Threshold Interval

T

70 100 FH

T

20 000 CY

I

59 400 FH

I

16 900 CY

T

108 700 FH

T

20 000 CY

I

31 000 FH

I

8 800 CY

References

Ctrl

Eff

N

AMM 575000-220-840

275

N

AMM 575000-220-867

275

Access panels :

573DB

673DB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 NDT 454 464 500 532 533 534 600 632 633 634

575015-02-2

Issue No

:

Date

:

10 01/12/2013

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 12 TO RIB 39.

Amendment No Date

: 01 : 06/09/2014

DI

Page : STR - 57 [156 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575015-02-3

454 464 500 532 533 534 600 632 633 634


531 631


575016-01-4

Task Title

Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 12 TO RIB 39.

Threshold Interval

References

Ctrl

N

AMM 575000-220-867

138 000 FH

T

21 200 CY

I

30 300 FH

962

4 600 CY

1019

I

946

1256 1266

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING. note:CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

DI

T

60 000 FH

T

20 000 CY

T

12 YE

I

31 300 FH

I

8 900 CY

I

N

AMM 575000-210-812

12 YE


531AB

631AB

Total access time :

6.12 Hrs

Skills :

0.20 MHrs

1 AF

:

Date

:

10 01/12/2013

943

T

See note

Issue No

Eff

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [157 / 188] ATA

: 57

275


57

WINGS

Task Number

Zone

575016-01-4S100

531 631

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING. note:CPCP

Threshold Interval

References

Ctrl

N

AMM 575000-210-812

Eff 294

T

24 YE

I

31 300 FH

299

I

8 900 CY

366

I

12 YE

T

92 900 FH

T

14 300 CY

T

12 YE

Skills :

0.20 MHrs

1 AF R

575016-01-9S020

531 631


DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING. note:CPCP

I

28 000 FH

I

4 300 CY

I

12 YE

T

80 800 FH

T

23 000 FC

I

21 100 FH

I

6 000 CY

N

AMM 575000-210-812

943 946 962 1019 1256 1266

Skills :

0.20 MHrs

1 AF 573 673

575017-01-4

TRAILING EDGE AND TRAILING EDGE DEVICE SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR SUPPORT RIB 6.

SDI

N

AMM 575000-210-824

Access panels :

573DB

673DB

Total access time :

0.52 Hrs

Skills :

0.20 MHrs

1 NDT Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [158 / 188] ATA

: 57

275


R

57

WINGS

Task Number

Zone

575017-01-8S020

573 673

Task Title


Task code

SDI

SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR SUPPORT RIB 6.

Threshold Interval

References

Ctrl

N

AMM 575000-210-824

Eff 943

T

116 300 FH

T

17 900 CY

I

116 300 FH

962

17 900 CY

1019

I

946

1256 1266

Access panels :

573DB

673DB

Total access time :

0.52 Hrs

Skills :

0.20 MHrs

1 NDT 573 673

575017-02-1

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR SUPPORT RIB 6. TPS : TPS MUST NOT BE APPLIED note:CPCP

DI

T

6 YE

I

6 YE

N

AMM 575000-210-813

Access panels :

573DB

673DB

Total access time :

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [159 / 188] ATA

: 57

ALL


57

WINGS

Task Number

Zone

575018-02-1

572 672

Task Title


Task code

GVI

GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. PREP. : FLAPS EXTENDED; note:CPCP

Threshold Interval

T

12 YE

I

12 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 575000-210-845

ALL

N

AMM 575000-210-841

ALL

Access panels :

147AT

148AT

Total access time :

191CT 192CT 5.12 Hrs

Skills :

0.00 MHrs

1 AF 571 671

575019-01-1

DI

TRAILING EDGE DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF OVERWING PANEL. note:CPCP Access panels :

147AT

148AT

Total access time :

2.36 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [160 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575023-01-3S020

575 675

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL. note:CPCP

Threshold Interval

T

84 200 FH

T

12 900 CY

T

12 YE

I

47 300 FH

I

7 200 CY

I

12 YE

T

24 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-815

Eff 943 946 962 1019 1256 1266

Access panels :

575CB

575DB

Total access time :

675CB 675DB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 575 675

575023-01-9

Issue No

:

Date

:

10 01/12/2013

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

Amendment No Date

: 01 : 06/09/2014

DI

N

AMM 575000-210-815

294 299 366

Page : STR - 57 [161 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575023-01-9S020

575 675

Task Title


Task code

DI

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL. NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

83 800 FH

T

23 900 CY

T

12 YE

I

34 600 FH

I

9 900 CY

I

References

Ctrl

Eff

N

AMM 575000-210-815

275

N

AMM 575000-210-864

ALL

N

AMM 575000-210-836

943

12 YE See note

Check : NT

500 600

575025-02-1

R

147 148

575051-01-2


GVI

I

GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12. TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS. PREP. : FLAPS EXTENDED;

T

12 YE 12 YE See note

DI

T

17 800 FC

I

8 000 CY

946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [162 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575053-01-1

147 148

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACK NO 1, DRIVE LINK, DRIVE LEVER, DRIVE STRUT AND CARRIAGE. PREP. : FLAPS EXTENDED; note:CPCP NOTE: THRESHOLD IS NEXT 4C CHECK

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 575000-210-816

275

N

AMM 575000-210-837

294

See note Check : NT

Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.00 MHrs

1 AF R

147 148

575054-01-1

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOX SUPPORT, FORK ASSY, DRIVE STRUT AND CARRIAGE. PREP. : FLAPS EXTENDED;

DI

T

12 YE

I

12 YE

299 366 943 946 962 1019 1256 1266

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [163 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575055-01-1

147 148

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACK NO 1, ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING. MSN 275: THRESHOLD IS NEXT 4C CHECK note:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-817

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

575055-01-1S100

147 148

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK NO 1, ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING. note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-817

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [164 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575057-01-2

531 532 533 534 631 632 633 634

Task Title

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 5, UPPER FLANGES RADII. PREP. : FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z531; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z532; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z533; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z534; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z631; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z632; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z633; FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING Z634;

Task code

DI

Threshold Interval

T

20 000 CY

I

14 500 CY

References

Ctrl

N

AMM 575000-210-838

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

946 962 1019 1256 1266

0.00 MHrs

: 01 : 06/09/2014

275 943

Skills :

1 AF

Eff

Page : STR - 57 [165 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575059-01-1

531 532 533 534 631 632 633 634

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACKS NO 2, 3, 4 AND 5 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELLING BEAM AT TRACK NO 4. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-818

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.80 MHrs

1 AF 575059-01-1S100

531 532 533 534 631 632 633 634

TRAILING EDGE AND TRAILING EDGE DEVICE DETAILED INSPECTION OF FLAP TRACKS NO 2, 3, 4 AND 5 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELLING BEAM AT TRACK NO 4. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; MOVABLE FLAP TRACK FAIRING note:CPCP

DI

T

24 YE

I

12 YE

N

AMM 575000-210-818

299 366

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [166 / 188] ATA

: 57


57

Task Number

Zone

575061-01-1

531 532 533 534 631 632 633 634


531 532 533 534 631 632 633 634


531 532 533 534 631 632 633 634


575061-01-1S100

R

WINGS

575063-01-3

Issue No

:

Date

:

10 01/12/2013

Task Title

Task code

DI

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, CARRIAGE ASSEMBLIES

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

Eff 275 943 946 962 1019 1256 1266

DI

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, CARRIAGE ASSEMBLIES

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 5 LOWER FLANGES, STRAP AND ANGLES.

T

24 YE

I

12 YE

N

AMM 575000-210-819

294 299 366

DI

T

12 YE

I

12 YE

N

AMM 575000-210-839

943 946 962 1019 1256 1266

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [167 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575065-01-1

531 532 533 534 631 632 633 634

Task Title


Task code

SDI

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, INTERNAL STRUCTURE TPS : TPS MUST NOT BE APPLIED PREP. : FLAP TRACK FAIRINGS; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-820

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT 575065-01-1S100

531 532 533 534 631 632 633 634

TRAILING EDGE AND TRAILING EDGE DEVICE SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, INTERNAL STRUCTURE TPS : TPS MUST NOT BE APPLIED PREP. : FLAP TRACK FAIRINGS; note:CPCP

SDI

T

24 YE

I

12 YE

N

AMM 575000-210-820

299 366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [168 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575069-01-2

531 532 533 534 631 632 633 634

Task Title


Task code

DI

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, AFT ATTACHMENT SPIGOTS PREP. : FLAP TRACK FAIRINGS; NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS NEXT 4C-CHECK FROM APPROVE DATE

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575000-210-823

Eff 275 943 946

See note

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575069-01-2S100

R

575402-01-1

531 532 533 534 631 632 633 634


500 600

INBOARD FLAP

DI

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, AFT ATTACHMENT SPIGOTS PREP. : FLAP TRACK FAIRINGS;

24 YE

I

12 YE

N

AMM 575000-210-823

294 299 366

SDI

SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN AND DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT TRACK 2, LH/RH. PREP. : FLAPS EXTENDED;

T

T

18 000 CY

I

8 000 CY

N

AMM 575400-220-801

275 943 946 962 1019 1256 1266

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [169 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575403-01-1

581 681

Task Title

Task code

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND EXTERNAL. note:CPCP NOTE: MSN 275 THRESHOLD IS NEXT 4C CHECK

Threshold Interval

References

Ctrl

N

AMM 575400-200-801

Eff 275

T

22 100 CY

T

12 YE

943

I

75 200 FH

946

I

11 500 CY

I

962 1019

12 YE

1256

See note Check : NT

1266

Access panels :

581AB

681AB

Total access time :

734 744 0.00 Hrs

Skills :

0.00 MHrs

1 AF R

575403-01-1S100

581 681

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND EXTERNAL. note:CPCP

N

AMM 575400-200-801

294

T

24 YE

I

75 200 FH

299

I

11 500 CY

366

I

12 YE

T

22 100 CY

T

12 YE

I

75 200 FH

962

I

11 500 CY

1019

I

12 YE

Skills :

0.00 MHrs

1 AF 581 681

575403-02-1

Issue No

:

Date

:

10 01/12/2013

INBOARD FLAP SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL. TPS : TPS MUST NOT BE APPLIED PREP. : SPEED TAPES; NOTE: CPCP

Amendment No Date

: 01 : 06/09/2014

SDI

N

AMM 575400-200-802

943 946

1256 1266

Page : STR - 57 [170 / 188] ATA

: 57


57

WINGS

Task Number

Zone

575403-02-1S100

581 681

Task Title

Task code

DI

INBOARD FLAP SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL. TPS : TPS MUST NOT BE APPLIED PREP. : SPEED TAPES; NOTE: CPCP

Threshold Interval

References

Ctrl

N

AMM 575400-200-802

Eff 275

T

24 YE

I

75 200 FH

294

I

11 500 CY

299

I

12 YE

T

6 YE

I

6 YE

366

Skills :

0.00 MHrs

1 NDT 581 681

575404-03-1

R

581 681

575404-03-2

INBOARD FLAP

SDI

SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING EDGE. PREP. : FLAPS EXTENDED; NOTE: CPCP INBOARD FLAP SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING EDGE. PREP. : FLAPS EXTENDED; NOTE: CPCP

N

AMM 575400-220-805

275 294 299 366

SDI

T

12 YE

I

12 YE

N

AMM 575400-220-805

943 946 962 1019 1256 1266

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [171 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575405-01-1

500 681

Task Title

Task code

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 2 AND EXTERNAL DRIVE STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM ATTACHMENT BRACKET PREP. : FLAPS EXTENDED; note:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575400-200-803

Eff 275 943 946 962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575405-01-1S100

581 681

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 2 AND EXTERNAL DRIVE STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM ATTACHMENT BRACKET PREP. : FLAPS EXTENDED; note:CPCP

T

24 YE

I

12 YE

N

AMM 575400-200-803

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [172 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575405-02-1

581 681

Task Title

Task code

Threshold Interval

SDI

T

12 YE

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL FITTING AT TRACK NO 2 TPS MUST NOT BE APPLIED FLAPS EXTENDED; SPEED TAPES; note:CPCP note: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE "

I

12 YE

INBOARD FLAP SPECIAL SUPPORT TPS : PREP. :

References

Ctrl

N

AMM 575400-200-804

Eff 275 943 946 962 1019 1256 1266

Access panels :

531AT

531CB

Total access time :

631AT 631CB 0.00 Hrs

Skills :

0.00 MHrs

0 NDT 575405-02-1S100

581 681

SDI

INBOARD FLAP SPECIAL SUPPORT TPS : PREP. :

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL FITTING AT TRACK NO 2 TPS MUST NOT BE APPLIED FLAPS EXTENDED; SPEED TAPES; note:CPCP

T

24 YE

I

12 YE

N

AMM 575400-200-804

299 366

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [173 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575407-01-1

581 681

Task Title

Task code

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, OUTER END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET PREP. : FLAPS EXTENDED; RUBBER SEALS; TPS : TPS MUST NOT BE APPLIED"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE""" note:CPCP

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575400-200-805

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 575407-01-1S100

581 681

DI

INBOARD FLAP DETAILED INSPECTION OF INBOARD FLAP, OUTER END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET PREP. : FLAPS EXTENDED; RUBBER SEALS; TPS : TPS MUST NOT BE APPLIED note:CPCP

T

24 YE

I

12 YE

N

AMM 575400-200-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [174 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575409-01-1

581 681

Task Title

Task code

SDI

INBOARD FLAP SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL STRUCTURE TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; note:CPCP"NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575400-290-801 MRB 575409-01-1

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 NDT 575409-01-1S100

581 681

SDI

INBOARD FLAP SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL STRUCTURE TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; note:CPCP

T

24 YE

I

12 YE

N

AMM 575400-290-801 MRB 575409-01-1

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

0.00 MHrs

: 01 : 06/09/2014

299 366

Skills :

1 NDT

294

Page : STR - 57 [175 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575503-01-1

583 683

Task Title

Task code

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3, AND EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE W ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING PREP. : FLAPS EXTENDED; "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575500-200-801

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

532AT

532CB

Total access time :

632AT 632CB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 575503-01-1S100

583 683

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3, AND EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE W ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING PREP. : FLAPS EXTENDED;

T

24 YE

I

12 YE

N

AMM 575500-200-801

299 366

See note

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [176 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575503-02-1

583 683

Task Title

Task code

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE "

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575500-200-802

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

532AT

532CB

Total access time :

632AT 632CB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT 575503-02-1S100

583 683

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; NOTE: CPCP

T

24 YE

I

12 YE

N

AMM 575500-200-802

299 366

See note

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [177 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575505-01-1

583 683

Task Title

Task code

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 4, AND EXTERNAL FWD SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING PREP. : FLAPS EXTENDED; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE "

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575500-200-803

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

533AT

533CB

Total access time :

633AT 633CB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 575505-01-1S100

583 683

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 4, AND EXTERNAL FWD SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING PREP. : FLAPS EXTENDED; NOTE: CPCP

T

24 YE

I

12 YE

N

AMM 575500-200-803

299 366

See note

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [178 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575505-02-1

583 683

Task Title

Task code

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 4. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575500-200-804

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

533AT

533CB

Total access time :

633AT 633CB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT 575505-02-1S100

583 683

SDI


T

24 YE

I

12 YE

N

AMM 575500-200-804

299 366

See note

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [179 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575507-01-1

583 683

Task Title

Task code

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 5, AND EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING PREP. : FLAPS EXTENDED; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE "

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 575500-200-805

Eff 275 943 946

See note

962 1019 1256 1266

Access panels :

534AT

534CB

Total access time :

634AT 634CB 0.00 Hrs

Skills :

0.00 MHrs

1 AF 575507-01-1S100

583 683

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 5, AND EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING PREP. : FLAPS EXTENDED; NOTE: CPCP

T

24 YE

I

12 YE

N

AMM 575500-200-805

299 366

See note

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [180 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575507-02-1

583 683

Task Title

Task code

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 5. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; SPEED TAPES; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE "

Threshold Interval

References

Ctrl

N

AMM 575500-200-806

Eff 275

T

20 000 FC

T

12 YE

943

I

15 500 CY

946

I

12 YE

962 1019

See note

1256

Check : C4

1266

Access panels :

534AT

534CB

Total access time :

634AT 634CB 0.00 Hrs

Skills :

0.00 MHrs

1 NDT 575507-02-1S100

583 683

SDI


N

AMM 575500-200-806

20 000 FC

T

20 YE

299

I

15 500 CY

366

I

12 YE See note

Skills :

0.00 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

T

Page : STR - 57 [181 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575509-01-1

583 683

Task Title

Task code

DI

OUTBOARD FLAP

DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNA SURFACE OF INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET. PREP. : FLAPS EXTENDED; RUBBER SEALS; NOTE: CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

References

Ctrl

N

AMM 575500-200-807

Eff 275

T

29 000 FC

T

12 YE

943

I

73 200 CY

946

I

12 YE

962 1019

See note

1256

Check : NT

1266

Skills :

0.00 MHrs

1 AF 575509-01-1S100

583 683

DI

OUTBOARD FLAP DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNA SURFACE OF INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET. PREP. : FLAPS EXTENDED; RUBBER SEALS; NOTE: CPCP

N

AMM 575500-200-807

29 000 CY

T

24 YE

299

I

73 200 CY

366

I

12 YE

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

T

Page : STR - 57 [182 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

575509-02-1

583 683

Task Title

Task code

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FL INTERNAL STRUCTURE OF INNER END RIB. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; RUBBER SEALS; SPEED TAPES; NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"

Threshold Interval

References

Ctrl

N

AMM 575500-200-808

Eff 275

T

20 000 FC

T

12 YE

943

I

15 500 CY

946

I

12 YE

962 1019 1256 1266

Skills :

0.40 MHrs

1 NDT 575509-02-1S100

583 683

SDI

OUTBOARD FLAP SPECIAL DETAILED INSPECTION OF OUTBOARD FL INTERNAL STRUCTURE OF INNER END RIB. TPS : TPS MUST NOT BE APPLIED PREP. : FLAPS EXTENDED; RUBBER SEALS; SPEED TAPES; SPEED TAPES; NOTE: CPCP

N

AMM 575500-200-808

20 000 FC

T

20 YE

299

I

15 500 CY

366

I

12 YE

Skills :

0.40 MHrs

1 NDT

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

T

Page : STR - 57 [183 / 188] ATA

: 57


57

WINGS

Task Number

Zone

576101-01-1

590 690

Task Title

Task code

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF OUTBOARD AILERON, UPPER AND LOWER SKINS, EXTERNAL SURFACE

Threshold Interval

T

6 YE

I

6 YE

T

12 YE

I

12 YE

References

Ctrl

Eff

N

AMM 576100-200-801

ALL

N

AMM 576100-200-802

275

Skills :

0.66 MHrs

1 AF R

592 692

576103-01-1

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF OUTBOARD AILERON END RIBS, EXTERNAL SURFACE PREP. : ONLY OUTBOARD AILERON DEFLECTED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 576103-01-1S100

592 692

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF OUTBOARD AILERON END RIBS, EXTERNAL SURFACE PREP. : ONLY OUTBOARD AILERON DEFLECTED; note:CPCP

T

24 YE

I

12 YE

N

AMM 576100-200-802

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [184 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

576104-01-1

592 692

Task code

Task Title

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS (7 PLACES) NOTE: CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 576100-200-803

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

575BT 675BT

575CB 675CB

Total access time :

575DB 592AB 675DB 692AB 0.00 Hrs

592BB 692BB

592CB 692CB

592DB 692DB

Skills :

0.00 MHrs

1 AF 576104-01-1S100

592 692

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS (7 PLACES) NOTE: CPCP

T

24 YE

I

12 YE

N

AMM 576100-200-803

294 299 366

Skills :

0.00 MHrs

1 AF 590 690

576111-01-1

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF INBOARD AILERON, UPPER AND LOWER SKINS, EXTERNAL SURFACE

T

6 YE

I

6 YE

N

AMM 576100-200-804

Skills :

0.30 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [185 / 188] ATA

: 57

ALL


R

57

WINGS

Task Number

Zone

576113-01-1

591 691

Task Title

Task code

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF INBOARD AILERON END RIBS, EXTERNAL SURFACE PREP. : INBOARD AILERON ONLY DEFLECTED; note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 576100-200-805

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Skills :

0.00 MHrs

1 AF 576113-01-1S100

591 691

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF INBOARD AILERON END RIBS, EXTERNAL SURFACE PREP. : INBOARD AILERON ONLY DEFLECTED; note:CPCP

T

24 YE

I

12 YE

N

AMM 576100-200-805

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [186 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

576114-01-1

591 691

Task code

Task Title

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF INBOARD AILERON FITTINGS (7 PLACES) note:CPCP "NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS ""20 YE"""

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 576100-200-806

Eff 275 943 946

See note Check : NT

962 1019 1256 1266

Access panels :

575AB 675AB

575AT 675AT

Total access time :

575BB 591AB 675BB 691AB 0.00 Hrs

591BB 691BB

591CB 691CB

591DB 691DB

Skills :

0.00 MHrs

1 AF 576114-01-1S100

591 691

DI

AILERON MAIN STRUCTURE DETAILED INSPECTION OF INBOARD AILERON FITTINGS (7 PLACES) note:CPCP

T

24 YE

I

12 YE

N

AMM 576100-200-806

299 366

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

294

Page : STR - 57 [187 / 188] ATA

: 57


R

57

WINGS

Task Number

Zone

577003-01-1

582 682

Task Title

Task code

DI

SPOILER

DETAILED INSPECTION OF SPOILER NO 1, HINGE AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES) PREP. : FLAPS EXTENDED SPOILERS DEPLOYED NOTE: CPCP NOTE: MSN 275 BECOME SAMPLE A/C FROM AMS A330 I09 A00; THRESHOLD IS "20 YE"

Threshold Interval

T

29 600 FC

T

12 YE

I

23 500 CY

I

References

Ctrl

Eff

N

AMM 577000-200-801

275

N

AMM 577000-200-801

294

12 YE See note

Check : NT

Skills :

0.00 MHrs

1 AF 577003-01-1S100

582 682

SDI

SPOILER DETAILED INSPECTION OF SPOILER NO 1, HINGE AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES) PREP. : FLAPS EXTENDED SPOILERS DEPLOYED NOTE: CPCP

T

24 YE

I

12 YE

299 366

Skills :

0.00 MHrs

1 AF N

582 682

577003-01-3

DI

SPOILER DETAILED INSPECTION OF SPOILER NO. 1, HINGE AND ACTUATOR ATTACHMENT FITTINGS. PREP. : FLAPS EXTENDED; SPOILERS DEPLOYED;

T

12 YE

I

12 YE

N

AMM 577000-200-801

943 946 962 1019 1256 1266

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 57 [188 / 188] ATA

: 57


71


Task Number

Zone

711301-01-1

415 416 425 426

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). TPS : TPS MUST NOT BE APPLIED note:CPCP

Threshold Interval

T

6 YE

I

6 YE

T

6 YE

I

6 YE

References

Ctrl

Eff

N

AMM 711300-210-803

ALL

N

AMM 711300-220-802

ALL

Access panels :

415AL 426BR

415BL

Total access time :

416AR

416BR

425AL

425BL

426AR

0.16 Hrs

Skills :

0.00 MHrs

1 EN 415 416 425 426

711302-01-1

DI

MAIN STRUCTURE DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). TPS : TPS MUST NOT BE APPLIED note:CPCP Access panels :

415AL 426BR

415BL

Total access time :

416AR

416BR

425AL

425BL

426AR

0.16 Hrs

Skills :

0.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 71 [1 / 2] ATA

: 71


71


Task Number

Zone

712201-03-1

413 423

Task Title

Task code

DI

MAIN STRUCTURE DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM TPS : TPS MUST NOT BE APPLIED PREP. : AFT ENGINE MOUNT DISASSEMBLED; ENGINE; note:CPCP NOTE: RII TASK

Threshold Interval

T

12 YE

I

12 YE

References

Ctrl

N

AMM 712211-220-801

Skills :

0.00 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 71 [2 / 2] ATA

: 71

Eff ALL


78

ENGINE EXHAUST

Task Number

Zone

783201-02-1

417 418 427 428

Task code

Task Title

DI

MAIN STRUCTURE DETAILED INSPECTION OF THRUST REVERSER HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE ATTACHMENTS). note:CPCP

Threshold Interval

T

6 YE

I

6 YE

References

Ctrl

N

AMM 783200-210-803

Access panels :

415BL 428AR

416BR

Total access time :

417AL

418AR

425BL

426BR

427AL

0.08 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : STR - 78 [1 / 1] ATA

: 78

Eff ALL


PAGE

AMDT / ISSUE NO

26

01/10

TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

ZNL-00

1

01/10

ZNL-00

ZNL-00

2

01/10

ZNL-00

ZNL-00

3

01/10

ZNL-00

ZNL-00

4

01/10

ZNL-00

ZNL-00

5

01/10

ZNL-00

ZNL-00

6

01/10

ZNL-00

ZNL-00

7

01/10

ZNL-00

ZNL-00

8

01/10

ZNL-00

ZNL-00

9

01/10

ZNL-00

ZNL-00

10

01/10

ZNL-00

ZNL-00

11

01/10

ZNL-00

ZNL-00

12

01/10

ZNL-00

ZNL-00

13

01/10

ZNL-00

ZNL-00

14

01/10

ZNL-00

ZNL-00

15

01/10

ZNL-00

ZNL-00

16

01/10

ZNL-00

ZNL-00

17

01/10

ZNL-00

ZNL-00

18

01/10

ZNL-00

ZNL-00

19

01/10

ZNL-00

ZNL-00

20

01/10

ZNL-00

ZNL-00

21

01/10

ZNL-00

ZNL-00

22

01/10

ZNL-00

ZNL-00

23

01/10

ZNL-00

24

01/10

ZNL-00

25

01/10

ISSUE 10 AMD 01


TITLE/CHAPTER/ZONE

PAGE

AMDT / ISSUE NO

Page: 1


00

GENERAL

Task Number

Zone

ZL-100-01-2

100

Task Title

LOWER HALF OF FUSELAGE

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052100-200-802

ALL

GVI

Check : 2C

N

AMM 052110-200-801

ALL

GVI

Check : 1C

N

AMM 052120-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF LOWER HALF OF FUSELAGE Skills :

1.00 MHrs

1 AF 110

ZL-110-01-1

RADOME GENERAL VISUAL INSPECTION OF RADOME (EWIS) Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF 121 122

ZL-121-01-1

AVIONICS COMPARTMENT GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT Access panels :

132AZ

821

Total access time :

0.02 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [1 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-121-02-1

121 122

Task Title

AVIONICS COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052120-200-802

ALL

GVI

Check : 1C

N

AMM 052120-200-803

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT (EWIS) Access panels :

121AF 121HF 122JF 132AZ

121BF 121KF 122LF 132CW

Total access time :

121CF 122CF 122MF 821

121DF 122DF 122NF

121EF 122FF 122PF

121FF 122GF 131AW

121GF 122HF 131BW

0.02 Hrs

Skills :

1.20 MHrs

1 AF 123

ZL-123-01-1

NOSE GEAR WELL GENERAL VISUAL INSPECTION OF NOSE GEAR WELL (EWIS) Access panels :

713

714

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [2 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-131-01-1

131 132

Task code

Task Title

GVI


Threshold Interval

I

800 FH

References

Ctrl

Eff

N

AMT 052130-200-801

ALL

N

AMM 052130-200-802

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT(EWIS) Access panels :


0.02 Hrs

Skills :

0.40 MHrs

1 AF 131 132

ZL-131-02-2

GVI


Check : 4C

GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT(EWIS). Access panels :

131BC 131VC

131FC 131XC

Total access time :

131FX 131KW 132FX 132UW 0.02 Hrs

131PC 132WW

131RC 821

131TC

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [3 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-131-03-1

131 132

Task Title


Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052130-200-803

ALL

GVI

Check : 4C

N

AMM 052130-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT(EWIS). Access panels :


0.02 Hrs

Skills :

1.20 MHrs

1 AF 133 134

ZL-133-01-1

BAY UNDER FWD CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF BAY UNDER FWD CARGO COMPARTMENT (EWIS). Access panels :

133AL

133BL

Total access time :

821 0.02 Hrs

Skills :

2.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [4 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-137-01-1

137 138

Task Title

BAY BEHIND FWD CARGO COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052130-200-806

ALL

GVI

Check : 8C

N

AMM 052140-200-801

ALL

GVI

Check : 8C

N

AMM 052140-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF BAY BEHIND FWD CARGO COMPARTMENT (EWIS). Access panels :

131BX 132DG

131CG 132DX

Total access time :

131CX 821

131DG

131DX

132CG

132CX

0.02 Hrs

Skills :

0.80 MHrs

1 AF 141 142

ZL-141-01-1

CENTER WING TANK GENERAL VISUAL INSPECTION OF CENTER WING BOX (EWIS) Access panels :

147AZ

148AZ

Total access time :

734 744 0.60 Hrs

Skills :

0.60 MHrs

1 AF 143

ZL-143-01-1

AREA BETWEEN KEEL BEAMS GENERAL VISUAL INSPECTION OF AREA BETWEEN KEEL BEAMS UNDER WING CENTRE BOX TO BOTTOM FUSELAGE(EWIS). Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.33 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [5 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-145-01-1

145 146

Task Title

ZONE UNDER CABIN FLOOR

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052140-200-803

ALL

GVI

I

N

AMM 052140/6 AMT 052140-200-804

ALL

N

AMM 052140-200-809

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF ZONE UNDER CABIN FLOOR, ABOVE WING CENTRE BOX AND MAIN GEAR WELL (EWIS). PREP. : FLOOR PANELS FROM FR 40 TO FR 53.2; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

0.30 MHrs

1 AF 147 148

ZL-147-01-1

MLG WELL AND HYDRAULIC COMPARTMENT

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF MAIN LANDING GEARS WELL AND HYDRAULICS COMPARTMENT(EWIS). Access panels :

734

744

Total access time :

0.16 Hrs

Skills :

0.06 MHrs

1 AF 149

ZL-149-05-1

GVI

CENTER LINE BAY

Check : 8C

GENERAL VISUAL INSPECTION OF CENTER LINE BAY (EWIS). Access panels :

149AB

149CB

Total access time :

734 744 0.00 Hrs

Skills :

0.05 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [6 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-151-01-1

151 152

Task code

Task Title

GVI


Threshold Interval

I

800 FH

Eff

N

AMM 052150/6 AMT 052150-200-801

ALL

N

AMM 052150-200-802

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (AS FAR AS VISIBLE IF LD-MCR AND/OR LDL INSTALLED) (EWIS).

References

Ctrl

Access panels :


0.00 Hrs

Skills :

0.40 MHrs

1 AF 151 152

ZL-151-02-2

GVI


Check : 4C

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS). PREP. : LD-MCR-IF INSTALLED; Access panels :

151BW 151TW 822

151BY 152AX

Total access time :

151FC 152BW

151HC 152BX

151JW 152DW

151KC 152JW

151PC 152LW

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [7 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-151-02-3

151 152

Task code

Task Title


Threshold Interval

References

Ctrl

Eff

Check : 4C

N

AMM 052150-200-802

ALL

Check : 8C

N

AMM 052150-200-803

ALL

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT(EWIS). Access panels :

151BC 151RW 152JW

151BW 151SW 152KW

Total access time :

151FC 151TW 822

151HW 152BW

151JW 152DW

151KW 152EW

151QW 152GW

0.00 Hrs

Skills :

1.40 MHrs

1 AF 151 152

ZL-151-03-1

GVI

AFT CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS). PREP. : LD-MCR-IF INSTALLED; SIDEWALL AND CEILING PANELS FROM FR 53.2 TO FR 66; Access panels :


0.00 Hrs

Skills :

1.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [8 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-153-01-1

153 154

Task Title

BAY UNDER AFT CARGO COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052150-200-805

ALL

GVI

I

N

AMM 052160/6 AMT 052160-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF BAY UNDER AFT CARGO COMPARTMENT (EWIS). PREP. : FLOOR PANELS FROM FR 53.2 TO FR 66,; LD-MCR-IF INSTALLED; NOTE 1; Access panels :


0.00 Hrs

Skills :

0.80 MHrs

1 AF 161 162

ZL-161-01-1

BULK CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS)

800 FH

Check : 1A

Access panels :


0.02 Hrs

Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [9 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-161-02-1

161 162

Task Title

BULK CARGO COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052160-200-802

ALL

GVI

Check : 8C

N

AMM 052160-200-803

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS). Access panels :

161AC 162TW

161BC 162WW

Total access time :

161CW 822

161EC

162LW

162RW

162SW

0.00 Hrs

Skills :

1.00 MHrs

1 AF 161 162

ZL-161-03-1

BULK CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS). PREP. : NOTE 1; SIDEWALL AND CEILING PANELS FROM FR 65 TO FR 73; Access panels :


0.05 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [10 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-163-01-1

163 164

Task Title

BAY UNDER BULK CARGO COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052160-200-804

ALL

GVI

Check : 1C

N

AMM 052170-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF BAY UNDER BULK CARGO COMPARTMENT (EWIS). PREP. : FLOOR PANELS FROM FR 65 TO FR 73; NOTE 1; Access panels :

164AR

823

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF 171 172

ZL-171-01-1

AFT CABIN UNDERFLOOR COMPARTMENT GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS). Access panels :

162ZW

171AL

Total access time :

822 0.00 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [11 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-171-02-1

171 172

Task Title

AFT CABIN UNDERFLOOR COMPARTMENT

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052170-200-802

ALL

GVI

Check : 2C

N

AMM 052190-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS). PREP. : FLOOR PANELS Z170; INSULATION Z170; Access panels :


0.00 Hrs

Skills :

1.60 MHrs

1 AF 191 192

ZL-191-01-1

AIR CONDITIONING COMPT AND FAIRING GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPT AND FAIRING (EWIS). Access panels :

191FB

191KB

Total access time :

192JB 192PB 0.00 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [12 / 60] ATA

: 00


R

00

GENERAL

Task Number

Zone

ZL-191-02-1

191 192

Task Title

AIR CONDITIONING COMPT AND FAIRING

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052190-200-802

ALL

GVI

Check : 2C

N

AMM 052190-200-810

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS). Access panels :

191AB 191EB 192BT 192NB

191AT 191FB 192CB 192PB

Total access time :

191BB 191HB 192CT 192QB

191BT 191KB 192GB

191CB 191QB 192HB

191CT 192AT 192JB

191DB 192BB 192MB

0.00 Hrs

Skills :

1.00 MHrs

1 AF 193

ZL-193-01-1

AIR CONDITIONING COMPARTMENT AND FAIRING GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS). Access panels :

193BB

193DB

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [13 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-193-02-1

193

Task Title

AIR CONDITIONING COMPARTMENT AND FAIRING

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052190-200-811

ALL

GVI

I

N

AMM 052190/6 AMT 052190-200-805

ALL

N

AMM 052190-200-806

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS). Access panels :

193AB

193BB

Total access time :

193CB 193DB 0.00 Hrs

Skills :

0.20 MHrs

1 AF 195 196

ZL-195-01-1

HYDRAULIC COMPARTMENT AND FAIRINGS

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENT AND FAIRINGS (AS FAR AS VISIBLE) (EWIS). Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF 195 196

ZL-195-02-1

HYDRAULIC COMPARTMENT AND FAIRINGS

GVI

Check : 2C

GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS). Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [14 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-197-01-1

197 198

Task Title

Task code

GVI

REAR FAIRINGS

Threshold Interval

I

800 FH

Eff

N

AMM 052190/6 AMT 052190-200-807

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF REAR FAIRINGS (EWIS).

References

Ctrl

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.60 MHrs

1 AF 197 198

ZL-197-02-1

REAR FAIRINGS

GVI

Check : 4C

N

AMM 052190-200-808

ALL

GVI

I

N

AMM 052200-200-802

ALL

GENERAL VISUAL INSPECTION OF ZONE BETWEEN FUSELAGE SKIN AND REAR FAIRINGS (EWIS). Access panels :

197EB

198EB

Total access time :

0.00 Hrs

Skills :

0.60 MHrs

1 AF 200

ZL-200-01-1

UPPER HALF OF FUSELAGE

36 MO

GENERAL VISUAL INSPECTION OF UPPER HALF OF FUSELAGE Skills :

0.50 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [15 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-211-01-1

211 212

Task code

Task Title

COCKPIT

Threshold Interval

GVI

I

GVI

Check : 8C

48 MO

References

Ctrl

Eff

N

AMM 052210-200-801

ALL

N

AMM 052210-200-802

ALL

GENERAL VISUAL INSPECTION OF COCKPIT (EWIS). Access panels :

211JW

211KW

Total access time :

212JW 212KW 0.00 Hrs

831

841

Skills :

0.40 MHrs

1 AF 211 212

ZL-211-02-1

COCKPIT GENERAL VISUAL INSPECTION OF COCKPIT (EWIS). NOTE: THIS TASK PRECLUDES TASK ZL-211-01-1 PREP. : FLOOR PANELS FROM FR 1 TO FR 11; NOTE 1; Access panels :

211AC 211DW 211HC 211LW 212DC 212HC 212NC

211AW 211EC 211HW 211MC 212DW 212HW 212NW

Total access time :

211BC 211EW 211JC 211MW 212EW 212JC 212QW 0.00 Hrs

211BW 211FC 211JW 211PW 212FC 212JW 831

211CC 211FW 211KC 212BC 212FW 212KW 841

211CW 211GC 211KW 212CC 212GC 212LW

211DC 211GW 211LC 212CW 212GW 212MW

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [16 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-221-02-1

221 222

Task Title

FWD CABIN UTILITY AREA

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052220-200-802

ALL

GVI

Check : 8C

N

AMM 052220-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREA (EWIS). PREP. : CREW REST ROOM IF INSTALLED; DOOR FRAME LINING AND PANELS FROM FR 11 TO FR 17; FLOOR PANELS FROM FR 11 TO FR 17; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; SEATS AND FURNISHINGS; Access panels :

831

841

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF 223 224

ZL-223-01-1

FWD CABIN UTILITY AREA OVERHEAD COMPT GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREA OVERHEAD COMPT (EWIS). PREP. : CEILING PANELS; FCRC, GALLEYS AND TOILETS - IF INSTALLED FROM FR 11 TO FR 17; NOTE 1; Access panels :

221AZ

221BZ

Total access time :

222AZ 222BZ 0.00 Hrs

831

841

Skills :

1.00 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [17 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-231-02-1

231 232

Task Title

FWD PASSENGER COMPARTMENT

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052230-200-803

ALL

GVI

Check : 8C

N

AMM 052230-200-805

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FWD PASSENGER COMPARTMENT (EWIS). PREP. : GALLEYS AND TOILETS IF INSTALLED; NOTE 1; SEATS AND FURNISHINGS; SIDEWALL AND FLOOR PANELS FROM FR 17 TO FR 31; Access panels :

831

841

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 233 234

ZL-233-01-1

FWD CABIN OVERHEAD COMPARTMENT GENERAL VISUAL INSPECTION OF FWD CABIN OVERHEAD COMPARTMENT (EWIS). PREP. : CEILING PANELS; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; OVERHEAD STOWAGE BINS FROM FR 17 TO FR 31; Access panels :

831

841

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [18 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-241-02-1

241 242

Task Title

MID CABIN UTILITY AREA

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052240-200-802

ALL

GVI

Check : 8C

N

AMM 052240-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF MID CABIN UTILITY AREA (EWIS). PREP. : GALLEYS AND TOILETS IF INSTALLED; NOTE 1; G AND FLOOR PANELS FROM FR 31 SEATS AND FURNISHINGS; DOOR FRAME LINING AND FLOOR PANELS FROM FR 31 TO FR 36; Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF 243 244

ZL-243-01-1

MID CABIN UTILITY AREA OVERHEAD COMPT GENERAL VISUAL INSPECTION OF MID CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS). PREP. : CEILING PANELS FROM FR 31 TO FR 36; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [19 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-251-02-1

251 252

Task Title

MID CABIN

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052250-200-802

ALL

GVI

Check : 8C

N

AMM 052250-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF MID CABIN (EWIS). PREP. : GALLEYS, TOILETS AND STAIRHOUSE (IF INSTALLED); NOTE 1; SEATS AND FURNISHINGS; SIDEWALL AND FLOOR PANELS FROM FR 36 TO FR 53.5; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

1.40 MHrs

1 AF 253 254

ZL-253-01-1

MID CABIN OVERHEAD COMPARTMENT GENERAL VISUAL INSPECTION OF MID CABIN OVERHEAD COMPARTMENT (EWIS). PREP. : CEILING PANELS; GALLEYS, TOILETS AND STAIRHOUSE (IF INSTALLED) FROM FR36 TO FR53.5; NOTE 1; BINS; OVERHEAD STOWAGE BINS; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

1.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [20 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-261-02-1

261 262

Task Title

AFT CABIN

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052260-200-802

ALL

GVI

Check : 8C

N

AMM 052260-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AFT CABIN (EWIS). PREP. : DOOR FRAME LINING; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; HINGS; SEATS AND FURNISHINGS; FR 53.5 TO FR SIDEWALL AND FLOOR PANELS FROM FR 53.5 TO FR 72; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF 263 264

ZL-263-01-1

AFT CABIN OVERHEAD COMPARTMENT GENERAL VISUAL INSPECTION OF AFT CABIN OVERHEAD COMPARTMENT (EWIS). PREP. : CEILING PANELS; GALLEYS AND TOILETS (IF INSTALLED) FROM FR 53.5 TO FR 72; NOTE 1; BINS; OVERHEAD STOWAGE BINS; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

1.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [21 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-271-02-1

271 272

Task Title


Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052270-200-802

ALL

GVI

Check : 8C

N

AMM 052270-200-804

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREA (EWIS). PREP. : DOOR FRAME LININGS, SIDEWALL AND FLOOR PANELS FROM FR 72 TO FR 80; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; SEATS AND FURNISHINGS; Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

1.20 MHrs

1 AF 273 274

ZL-273-01-1

AFT CABIN UTILITY AREA OVERHEAD COMPT GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREA OVERHEAD COMPT (EWIS). PREP. : CEILING PANELS FROM FR 72 TO FR 80; GALLEYS AND TOILETS IF INSTALLED; NOTE 1; Access panels :

271AZ 843

271BZ

Total access time :

271CZ

272AZ

272BZ

272CZ

833

0.00 Hrs

Skills :

1.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [22 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-300-01-1

300

Task Title

EMPENNAGE AND REAR FUSELAGE

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052300-200-802

ALL

GVI

Check : 1C

N

AMM 052310-200-801

ALL

GVI

Check : 1C

N

AMM 052310-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF EMPENNAGE AND REAR FUSELAGE Skills :

0.30 MHrs

1 AF 311 312

ZL-311-01-1

REAR FUSELAGE SECTION GENERAL VISUAL INSPECTION OF REAR FUSELAGE SECTION (EWIS). Access panels :

312AR

313AL

Total access time :

0.00 Hrs

Skills :

0.60 MHrs

1 AF 313 314

ZL-313-01-1

TAIL CONE APU AIR INTAKE AREA GENERAL VISUAL INSPECTION OF TAIL CONE APU AIR INTAKE AREA (EWIS). Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [23 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-315-01-1

315 316

Task Title

TAIL CONE APU AND ACCESSORY COMPT

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052310-200-803

ALL

GVI

Check : 1C

N

AMM 052310-200-804

ALL

GVI

Check : 8C

N

AMM 052310-200-806

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY COMPT (EWIS) Access panels :

315AL

316AR

Total access time :

0.00 Hrs

Skills :

0.60 MHrs

1 AF 317

ZL-317-01-1

TAIL CONE APU EXHAUST AREA GENERAL VISUAL INSPECTION OF TAIL CONE APU EXHAUST AREA (EWIS). Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF 319

ZL-319-02-2

HORIZONTAL STABILIZER CENTER BOX (INTERN GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER CENTRE BOX (EWIS). Access panels :

312AR

313AL

Total access time :

319DR 319ER 0.00 Hrs

Skills :

0.50 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [24 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-321-01-1

321

Task Title

DORSAL FIN

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052320-200-801

ALL

GVI

Check : 8C

N

AMM 052320-200-802

275

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF DORSAL FIN (EWIS). Access panels :


0.00 Hrs

Skills :

0.10 MHrs

1 AF 322

ZL-322-01-2

VERTICAL STABILIZER LEADING EDGE

294

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER LEADING EDGE (EWIS).

299 366

Skills :

0.30 MHrs

1 AF 322

ZL-322-01-3

VERTICAL STABILIZER LEADING EDGE

GVI

Check : 8C

N

AMM 052320-200-802

943 946

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER LEADING EDGE (EWIS).

962 1019 1256 1266

Access panels :

322AL

322BL

Total access time :

322CL

322EL

0.00 Hrs

Skills :

0.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [25 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-323-01-1

323

Task Title

VERTICAL STABILIZER SPAR BOX

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052320-200-803

ALL

GVI

Check : 8C

N

AMM 052320-200-804

275

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR BOX (EWIS). Access panels :

311AZ

311BZ

Total access time :

312AR 0.00 Hrs

Skills :

0.50 MHrs

1 AF 323

ZL-323-02-2


294

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR BOX, INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND FITTINGS (EWIS). PREP. : PEELABLE HOLE COVERS;

299 366

Access panels :

311AZ 323CL 325RL

311BZ 323DL

Total access time :

312AR 325LL

322AL 325ML

322BL 325NL

322CL 325PL

322DL 325QL

1.60 Hrs

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [26 / 60] ATA

: 00


R

00

GENERAL

Task Number

Zone

ZL-323-02-3

323

Task Title


Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 052320-200-804

Eff 943 946

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR BOX, INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND FITTINGS (EWIS). PREP. : PEELABLE HOLE COVERS;

962 1019 1256 1266

Access panels :

311AZ 323BL 325GL

311BZ 325AL 325HL

Total access time :

312AR 322AL 325BL 325CL 325JL 325KL 0.00 Hrs

322BL 325DL

322CL 325EL

323AL 325FL

Skills :

0.80 MHrs

1 AF 324

ZL-324-01-2

GVI

VERTICAL STABILIZER TIP

Check : 8C

N

AMM 052320-200-805

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TIP (EWIS). Access panels :

324CT Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [27 / 60] ATA

: 00

ALL


00

GENERAL

Task Number

Zone

ZL-325-01-2

325

Task Title

VERTICAL STABILIZER TRAILING EDGE

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052320-200-806

ALL

GVI

Check : 4C

N

AMM 052320-200-807

275

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TRAILING EDGE (EWIS). Access panels :

325NL Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 325

ZL-325-02-2


294

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TRAILING EDGE (EWIS).

299 366

Access panels :

325LL

325ML

Total access time :

325NL 325PL 0.00 Hrs

325QL

325RL

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [28 / 60] ATA

: 00


R

00

GENERAL

Task Number

Zone

ZL-325-02-3

325

Task Title


Task code

Threshold Interval

GVI

Check : 4C

References

Ctrl

N

AMM 052320-200-807

Eff 943 946

GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TRAILING EDGE (EWIS).

962 1019 1256 1266

Access panels :

325LL

325NL

Total access time :

325SL

325TL

325UL

325VL

0.00 Hrs

Skills :

0.00 MHrs

1 AF 326

ZL-326-02-3

GVI

RUDDER

Check : 4C

N

AMM 052320-200-810

294

GENERAL VISUAL INSPECTION OF RUDDER (AREA OF BEARINGS 1 TO 8) (EWIS).

299 366

Access panels :

325ML 326PL

325NL 326QL

Total access time :

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

325PL

325QL

325RL

326ML

326NL

0.00 Hrs

: 01 : 06/09/2014

275

Page : ZNL - 00 [29 / 60] ATA

: 00


R

00

GENERAL

Task Number

Zone

ZL-326-02-4

326

Task Title

RUDDER

Task code

Threshold Interval

GVI

Check : 4C

References

Ctrl

N

AMM 052320-200-810

Eff 943 946

GENERAL VISUAL INSPECTION OF RUDDER (AREA OF BEARINGS 1 TO 8) (EWIS).

962 1019 1256 1266

Access panels :

325NL 326PL

325SL 326RL

Total access time :

325TL 326SL

325UL

325VL

326ML

326NL

0.00 Hrs

Skills :

0.00 MHrs

1 AF 326

ZL-326-03-3

GVI

RUDDER

Check : 8C

N

AMM 052320-200-811

294

GENERAL VISUAL INSPECTION OF RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS VISIBLE) (EWIS).

299 366

Access panels :

324CT 325PL 326ML

325LL 325PR 326NL

Total access time :

325LR 325ML 325QL 325QR 326PL 326QL 0.00 Hrs

325MR 325RL

325NL 325RR

325NR 326AT

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

275

Page : ZNL - 00 [30 / 60] ATA

: 00


R

00

GENERAL

Task Number

Zone

ZL-326-03-4

326

Task Title

RUDDER

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 052320-200-811

Eff 943 946

GENERAL VISUAL INSPECTION OF RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS VISIBLE) (EWIS).

962 1019 1256 1266

Access panels :

324CT 325TL 326ML

325LL 325TR 326NL

Total access time :

325LR 325NL 325UL 325UR 326PL 326RL 0.00 Hrs

325NR 325VL 326SL

325SL 325VR

325SR 326AT

Skills :

0.60 MHrs

1 AF 326

ZL-326-10-1

GVI

RUDDER GENERAL VISUAL INSPECTION OF RUDDER (AREA OF BEARINGS 2, 3, 4 AND 5) (EWIS). NOTE: TASK REPLACE TASK ZL-326-01-2

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

I

24 MO

N

AMM 052320-200-813

See note Check : 1C

Page : ZNL - 00 [31 / 60] ATA

: 00

ALL


00

GENERAL

Task Number

Zone

ZL-331-01-1

331 341

Task Title

HORIZONTAL STABILIZER LEADING EDGE

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052330-200-801

ALL

GVI

Check : 8C

N

AMM 052330-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER LEADING EDGE (EWIS). Access panels :

331AT 341AT

331BT 341BT

Total access time :

331CT 341CT

331DT 341DT

331ET 341ET

333AB 343AB

333AT 343AT

0.00 Hrs

Skills :

0.60 MHrs

1 AF 332 342

ZL-332-01-1

HORIZONTAL STABILIZER TIP GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER TIP (EWIS). Access panels :

332AB

332AT

Total access time :

342AB 342AT 0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [32 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-333-01-1

333 343

Task Title

HORIZONTAL STABILIZER LATERAL BOX

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052330-200-804

ALL

GVI

Check : 1C

N

AMM 052330-200-805

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX (RIB 3 TO RIB 4) (EWIS). Access panels :

331AT 343AB

331BT 343AR

Total access time :

333AB 343AT

333AL

333AT

341AT

341BT

0.00 Hrs

Skills :

0.60 MHrs

2 AF 334 344

ZL-334-01-1

HORIZONTAL STABILIZER TRAILING EDGE GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER TRAILING EDGE (FUSELAGE FAIRING TO RIB 10) (EWIS). Access panels :

334AB

334BB

Total access time :

334CB 344AB 0.00 Hrs

344BB

344CB

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [33 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-334-02-1

334 344

Task Title

HORIZONTAL STABILIZER TRAILING EDGE

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052330-200-806

ALL

GVI

Check : 1C

N

AMM 052330-200-807

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER TRAILING EDGE (FUSELAGE FAIRING TO RIB 21) (EWIS). NOTE: THIS TASK PRECLUDES TASK ZL-334-01-1 Access panels :

334AB 344AB

334BB 344BB

Total access time :

334CB 344CB

334DB 344DB

334EB 344EB

334FB 344FB

334GB 344GB

0.00 Hrs

Skills :

0.80 MHrs

1 AF 335 345

ZL-335-01-1

ELEVATOR GENERAL VISUAL INSPECTION OF ELEVATOR BETWEEN RIB 8 AND RIB 9 (EWIS). Access panels :

334BB 345BB

334CB

Total access time :

334DB

335BB

344BB

344CB

344DB

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [34 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-335-02-1

335 345

Task Title

ELEVATOR

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052330-200-808

ALL

GVI

I

N

AMM 052400/6 AMT 052400-200-802

ALL

N

AMM 052410-200-808

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF ELEVATOR LEADING EDGE STRUCTURE (AS FAR AS VISIBLE) (EWIS). NOTE: THIS TASK PRECLUDES TASK ZL-335-01-1 Access panels :

334AB 335AB 344BB 345BB

334BB 335BB 344CB 345CB

Total access time :

334CB 335CB 344DB 345DB

334DB 335DB 344EB 345EB

334EB 335EB 344FB 345FB

334FB 335FB 344GB

334GB 344AB 345AB

0.00 Hrs

Skills :

0.80 MHrs

1 AF 400

ZL-400-01-1

POWER PLANTS, NACELLES AND PYLONS

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF POWER PLANTS, NACELLES AND PYLONS Skills :

0.20 MHrs

1 AF 411 421

ZL-411-03-2

ENGINE AIR INTAKE AND INTAKE LIP

GVI

Check : 4C

GENERAL VISUAL INSPECTION OF ENGINE AIR INTAKE AND INTAKE LIP (EWIS). Access panels :

411AL

411AR

Total access time :

421AL 421AR 0.00 Hrs

Skills :

0.60 MHrs

1 EN Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [35 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-412-02-2

412 422

Task Title

FAN AND ACCESSORY GEARBOX

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052410-200-810

ALL

GVI

I

N

AMM 052410-200-811

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEARBOX (EWIS). Access panels :

415AL 426BR

415BL

Total access time :

416AR

416BR

425AL

425BL

426AR

0.00 Hrs

Skills :

0.60 MHrs

1 EN 413 423

ZL-413-02-2

HOT SECTION

18 MO

GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS). Access panels :

415AL 425BL

415BL 426AR

Total access time :

416AR 426BR

416BR 427AL

417AL 428AR

418AR

425AL

0.00 Hrs

Skills :

0.60 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [36 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-414-02-2

414 424

Task Title

EXHAUST NOZZLE

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052410-200-812

ALL

GVI

Check : 2C

N

AMM 052410-200-813

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF EXHAUST NOZZLE (EWIS). Access panels :

415BL 428AR

416AR

Total access time :

417AL

418AR

425BL

426AR

427AL

0.00 Hrs

Skills :

0.60 MHrs

1 EN 415 416 425 426

ZL-415-02-2

FAN COWL GENERAL VISUAL INSPECTION OF FAN COWL (EWIS). Access panels :

415AL 425CL

415BL 426AR

Total access time :

415CL 426BR

416AR

416BR

425AL

425BL

0.00 Hrs

Skills :

0.80 MHrs

1 EN

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [37 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-417-02-2

417 418 427 428

Task Title

THRUST REVERSER

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052410-200-814

ALL

GVI

Check : 2C

N

AMM 052450-200-806

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF THRUST REVERSER (EWIS). PREP. : THRUST REVERSER DEPLOYED; Access panels :

415BL 417HL 418JR 427GL 428HR

416BR 418AR 425BL 427HL 428JR

417AL 418BR 426BR 428AR

Total access time :

417DL 418CR 427BL 428BR

417EL 418FR 427DL 428CR

417FL 418GR 427EL 428FR

417GL 418HR 427FL 428GR

0.00 Hrs

Skills :

0.80 MHrs

1 EN 451 461

ZL-451-02-1

PYLON LEADING EDGE GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE (EWIS). Access panels :

451AL 461AL

451BL 461BL

Total access time :

451BR 451CL 461BR 461CL 0.00 Hrs

451CR 461CR

451DL 461DL

451DR 461DR

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [38 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-452-01-1

452 462

Task code

Task Title

UPPER FORWARD PYLON

Threshold Interval

References

Ctrl

Eff

GVI

I

36 MO

N

AMM 052450-200-802

ALL

GVI

I

42 MO

N

AMM 052450-200-831

ALL

GVI

Check : 2C

N

AMM 052450-200-809

ALL

GENERAL VISUAL INSPECTION OF UPPER FORWARD PYLON (EWIS). Access panels :

452AL 462BR

452BL 462CL

Total access time :

452BR 462CR

452CL

452CR

462AL

462BL

0.00 Hrs

Skills :

0.40 MHrs

1 AF ZL-453-03-1

ZL-454-05-2

453 463

LOWER PYLON

454 464

LOWER AND REAR PYLON FAIRINGS

GENERAL VISUAL INSPECTION OF LOWER PYLON (EWIS).

GENERAL VISUAL INSPECTION OF LOWER AND REAR PYLON FAIRINGS (EWIS). Access panels :

454BL 454ML 464JL

454BR 454NR 464KL

Total access time :

454CL 454GL 464BL 464BR 464ML 464NR 0.00 Hrs

454HL 464CL

454JL 464GL

454KL 464HL

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [39 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-454-06-2

454 464

Task Title

LOWER AND REAR PYLON FAIRINGS

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052450-200-810

ALL

GVI

Check : 1C

N

AMM 052500-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF LOWER AND REAR PYLON FAIRINGS (EWIS). Access panels :

454AL 454GR 454MR 464ER 464KR

454BL 454HL 454NR 464GL 464ML

Total access time :

454BR 454HR 464AL 464GR 464MR 0.00 Hrs

454CL 454JL 464BL 464HL 464NR

454EL 454KL 464BR 464HR

454ER 454KR 464CL 464JL

454GL 454ML 464EL 464KL

Skills :

0.60 MHrs

1 AF 500 600

ZL-500-01-1

WING LOWER SURFACE (INCLUDING SLATS AND GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING SLATS AND FLAPS (EWIS). PREP. : FLAPS EXTENDED; SLATS EXTENDED; Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [40 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-500-02-1

500 600

Task Title

WING UPPER SURFACE

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052500-200-803

ALL

GVI

Check : 1C

N

AMM 052520-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF WING UPPER SURFACE INCLUDING SLATS, FLAPS AND SPOILERS (EWIS). PREP. : FLAPS EXTENDED; SLATS EXTENDED; SPOILERS EXTENDED; Skills :

1.20 MHrs

1 AF 521 621

ZL-521-01-1

INBOARD FIXED LEADING EDGE STRUCTURE GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS). PREP. : SLATS EXTENDED; Access panels :

521AB 621AB

521BB 621BB

Total access time :

521CB 621CB

521DB 621DB

521FB 621FB

521GB 621GB

521JB 621JB

0.00 Hrs

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [41 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-522-01-1

522 622

Task Title

CENTER FIXED LEADING EDGE STRUCTURE

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052520-200-802

ALL

GVI

Check : 1C

N

AMM 052520-200-803

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF CENTER FIXED LEADING EDGE STRUCTURE (EWIS). PREP. : SLATS EXTENDED; Access panels :

522AB 522HB 522UB 622EB 622TB

522AT 522JB 622AB 622HB 622UB

Total access time :

522BB 522LB 622AT 622JB

522BT 522NB 622BB 622LB

522CB 522QB 622BT 622NB

522CT 522RB 622CB 622QB

522EB 522TB 622CT 622RB

0.00 Hrs

Skills :

0.40 MHrs

1 AF 523 623

ZL-523-01-1

OUTER FIXED LEADING EDGE STRUCTURE GENERAL VISUAL INSPECTION OF OUTER FIXED LEADING EDGE STRUCTURE (EWIS). PREP. : SLATS EXTENDED; Access panels :

523AT 523NB

523BT 623CB

Total access time :

523CB 523EB 623EB 623GB 0.00 Hrs

523GB 623JB

523JB 623LB

523LB 623NB

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [42 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-531-01-1

531 532 533 534 631 632 633 634

Task Title

FLAP TRACKS AND FLAP TRACK FAIRINGS

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052530-200-801

ALL

GVI

Check : 4C

N

AMM 052530-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FLAP TRACKS AND FLAP TRACK FAIRINGS (INCLUDING RAT ATTACHMENT POINTS, AS FAR AS VISIBLE) (EWIS). PREP. : FLAPS EXTENDED;

Access panels :

531CB 634CB

532CB

Total access time :

533CB

534CB

631CB

632CB

633CB

0.00 Hrs

Skills :

1.60 MHrs

1 AF 531 532 533 534 631 632 633 634

ZL-531-02-1

FLAP TRACKS AND FLAP TRACK FAIRINGS GENERAL VISUAL INSPECTION OF FLAP TRACKS AND FLAP TRACK FAIRINGS (EWIS). PREP. : FLAPS EXTENDED;

Access panels :

531AB 534CB 634AB

531CB 631AB 634CB

Total access time :

532AB 631CB

532CB 632AB

533AB 632CB

533CB 633AB

534AB 633CB

0.00 Hrs

Skills :

2.40 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [43 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-535-01-1

535 635

Task Title

WING TIP

Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052530-200-809

ALL

GVI

Check : 4C

N

AMM 052540-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF WING TIP (EWIS). Access panels :

535AB

535BB

Total access time :

635AB 635BB 0.00 Hrs

Skills :

0.20 MHrs

1 AF 541 641

ZL-541-01-1

INNER FUEL TANK GENERAL VISUAL INSPECTION OF INNER FUEL TANK (AREA BETWEEN RIB 1 AND RIB 7) (EWIS). Access panels :

541AB 641BZ

541BB 641CB

Total access time :

541BZ 541CB 641CZ 0.00 Hrs

541CZ

641AB

641BB

Skills :

0.80 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [44 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-541-02-1

541 641

Task Title

INNER FUEL TANK

Task code

Threshold Interval

GVI

Check : 8C

References

Ctrl

N

AMM 052540-200-802

GENERAL VISUAL INSPECTION OF INNER FUEL TANK (AREA BETWEEN RIB 1 AND RIB 23) (EWIS). Access panels :

541AB 541DZ 541HB 541QB 641CB 641FZ 641MB

541AZ 541EB 541JB 541RB 641CZ 641GB 641NB

Total access time :

541BB 541EZ 541KB 541SB 641DB 641GZ 641PB 0.00 Hrs

541BZ 541FB 541LB 641AB 641DZ 641HB 641QB

541CB 541FZ 541MB 641AZ 641EB 641JB 641RB

541CZ 541GB 541NB 641BB 641EZ 641KB 641SB

541DB 541GZ 541PB 641BZ 641FB 641LB

Skills :

3.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [45 / 60] ATA

: 00

Eff ALL


00

GENERAL

Task Number

Zone

ZL-542-01-1

542 642

Task Title

OUTER FUEL TANK

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052540-200-803

ALL

GVI

Check : 8C

N

AMM 052550-200-802

ALL

References

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Eff

GENERAL VISUAL INSPECTION OF OUTER FUEL TANK (RIB 23 TO RIB 33) (EWIS). PREP. : FIXED FLAP TRACK FAIRING Z534; FIXED FLAP TRACK FAIRING Z634; FUEL TANK DRAINED AND VENTED; Access panels :

542AB 542HB 642DB 660DB

542BB 542JB 642EB

Total access time :

542CB 542KB 642FB

542DB 560DB 642GB

542EB 642AB 642HB

542FB 642BB 642JB

542GB 642CB 642KB

0.00 Hrs

Skills :

4.00 MHrs

1 AF 550 650

ZL-550-01-1

VENT SURGE TANK GENERAL VISUAL INSPECTION OF VENT SURGE TANK (RIB 33 TO RIB 39) (EWIS). Access panels :

550AB 650BB

550BB 650CB

Total access time :

550CB 550DB 650DB 650EB 0.00 Hrs

550EB 650FB

550FB

650AB

Skills :

0.66 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [46 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-571-01-1

571 671

Task Title

MAIN LANDING GEAR WELL

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052570-200-803

ALL

GVI

Check : 4C

N

AMM 052570-200-804

ALL

GVI

Check : 2C

N

AMM 052570-200-805

ALL

References

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Eff

GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR WELL (EWIS). Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.02 MHrs

1 AF 572 672

ZL-572-01-1

SHROUD BOX GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS). Access panels :

572BB

572CB

Total access time :

572EB 672BB 0.00 Hrs

672CB

672EB

Skills :

0.20 MHrs

1 AF 573 673

ZL-573-01-1

INNER TRAILING EDGE FIXED STRUCTURE GENERAL VISUAL INSPECTION OF INNER TRAILING EDGE FIXED STRUCTURE (RIB 6 TO RIB 12) (EWIS). PREP. : FLAPS EXTENDED; Access panels :

573CB

573DB

Total access time :

573GB 673CB 0.00 Hrs

673DB

673GB

Skills :

0.20 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [47 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-574-01-1

574 674

Task Title

CENTER TRAILING EDGE FIXED STRUCTURE

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052570-200-806

ALL

GVI

Check : 2C

N

AMM 052570-200-807

ALL

References

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Eff

GENERAL VISUAL INSPECTION OF CENTRE TRAILING EDGE FIXED STRUCTURE (RIB 12 TO RIB 27) (EWIS). PREP. : FLAPS EXTENDED; Access panels :

574AT

674AT

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 575 675

ZL-575-01-1

OUTER TRAILING EDGE FIXED STRUCTURE GENERAL VISUAL INSPECTION OF OUTER TRAILING EDGE FIXED STRUCTURE (RIB 27 TO RIB 39) (EWIS). Access panels :

575AB 675AT

575AT 675BB

Total access time :

575BB 575BT 675BT 675CB 0.00 Hrs

575CB 675DB

575DB

675AB

Skills :

0.60 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [48 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-591-01-1

591 691

Task Title

INBOARD AILERON

Task code

Threshold Interval

GVI

Check : 2C

N

AMM 052590-200-801

ALL

GVI

Check : 2C

N

AMM 052590-200-802

ALL

GVI

I

N

AMM 052710/6 AMT 052710-200-804

ALL

References

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Eff

GENERAL VISUAL INSPECTION OF INBOARD AILERON (EWIS). Access panels :

575AB 675BB

575BB 691AB

591AB 691BB

Total access time :

591BB 691CB

591CB 691DB

591DB

675AB

0.00 Hrs

Skills :

0.20 MHrs

1 AF 592 692

ZL-592-01-1

OUTBOARD AILERON GENERAL VISUAL INSPECTION OF OUTBOARD AILERON (EWIS) Access panels :

575CB 675DB

575DB 692AB

592AB 692BB

Total access time :

592BB 692CB

592CB 692DB

592DB

675CB

0.00 Hrs

Skills :

0.20 MHrs

1 AF 711

ZL-711-01-1

NOSE LANDING GEAR GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR (EWIS).

800 FH

Check : 1A

Access panels :

713

714

Total access time :

0.00 Hrs

Skills :

0.05 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [49 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-713-01-1

713 714

Task Title

NOSE LANDING GEAR MAIN DOORS

Task code

GVI

Threshold Interval

I

800 FH

Eff

N

AMM 052710/6 AMT 052710-200-807

ALL

N

AMM 052710/6 AMT 052710-200-808

ALL

N

AMM 052730/6 AMT 052730-200-804

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR MAIN DOORS (EWIS).

References

Ctrl

Access panels :

713

714

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 715 716

ZL-715-01-1

NOSE LANDING GEAR AFT DOORS

GVI

I

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR AFT DOORS (EWIS). Access panels :

715

716

Total access time :

0.00 Hrs

Skills :

0.10 MHrs

1 AF 731 741

ZL-731-01-1

GVI

MAIN LANDING GEAR GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR (EWIS).

I

800 FH

Check : 1A

Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.02 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [50 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-732-01-1

732 742

Task Title

MAIN LANDING GEAR - LEG DOORS

Task code

GVI

Threshold Interval

I

800 FH

Eff

N

AMM 052730/6 AMT 052730-200-810

ALL

N

AMM 052730/6 AMT 052730-200-811

ALL

N

AMM 052730/6 AMT 052730-200-812

ALL

N

AMM 052800-200-802

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR - LEG DOORS (EWIS).

References

Ctrl

Skills :

0.10 MHrs

1 AF 733 743

ZL-733-01-1

MAIN LANDING GEAR - HINGE DOOR

GVI

I

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR HINGE DOOR (EWIS). Skills :

0.10 MHrs

1 AF 734 744

ZL-734-01-1

MAIN LANDING GEAR MAIN DOORS

GVI

I

800 FH

Check : 1A

GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR MAIN DOORS (EWIS). Access panels :

734

744

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 800

ZL-800-01-1

GVI

DOORS

Check : 1C

GENERAL VISUAL INSPECTION OF PASSENGER/CREW DOORS, EMERGENCY EXITS, CARGO COMPARTMENTS DOORS, FORWARD AVIONICS COMPARTMENT DOOR Skills :

0.05 MHrs

1 AF Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [51 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-811-01-1

811

Task Title

FORWARD AVIONICS COMPARTMENT DOOR

Task code

Threshold Interval

GVI

Check : 1C

N

AMM 052810-200-801

ALL

GVI

I

N

AMM 052820/6 AMT 052820-200-802

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FORWARD AVIONICS COMPARTMENT DOOR (EWIS). Access panels :

121EF

811

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF 821

ZL-821-01-1

FORWARD CARGO COMPARTMENT DOOR GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR, INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SILL (EWIS).

800 FH

Check : 1A

Access panels :


0.02 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [52 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-821-02-1

821

Task Title


Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052820-200-803

ALL

GVI

Check : 8C

N

AMM 052820-200-808

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) (EWIS). Access panels :

132AR 132HR 821CR

132BR 132JR 821DR

Total access time :

132CR 132KR

132DR 132LR

132ER 821

132FR 821AR

132GR 821BR

0.02 Hrs

Skills :

0.20 MHrs

1 AF 821

ZL-821-03-1

FORWARD CARGO COMPARTMENT DOOR GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR (EWIS). NOTE: THSI TASK PRECLUDES TASK ZL-821-02-1 PREP. : INSULATION; Access panels :

821

821AR

Total access time :

821BR

821CR

821DR

0.02 Hrs

Skills :

1.00 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [53 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-822-01-1

822

Task code

Task Title

GVI


Threshold Interval

I

800 FH

Eff

N

AMM 052820/6 AMT 052820-200-804

ALL

N

AMM 052820-200-805

ALL

Check : 1A

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR, INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SILL (EWIS).

References

Ctrl

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF 822

ZL-822-02-1

GVI


Check : 4C

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) (EWIS). Access panels :

152AR 152HR 822CR

152BR 152JR 822DR

Total access time :

152CR 152KR

152DR 152LR

152ER 822

152FR 822AR

152GR 822BR

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [54 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-822-03-1

822

Task Title


Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052820-200-809

ALL

GVI

I

N

AMM 052820/6 AMT 052820-200-806

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR (EWIS). NOTE: THIS TASK PRECLUDES TASK ZL-822-02-1 PREP. : INSULATION; Access panels :

822

822AR

Total access time :

822BR 822CR 0.00 Hrs

822DR

Skills :

1.00 MHrs

1 AF 823

ZL-823-01-1

BULK CARGO COMPARTMENT DOOR GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR, INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE FRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL (EWIS).

800 FH

Check : 1A

Access panels :


0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [55 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-823-02-1

823

Task Title


Task code

Threshold Interval

GVI

Check : 4C

N

AMM 052820-200-807

ALL

GVI

Check : 1C

N

AMM 052830-200-801

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR (EWIS). PREP. : INSULATION; Access panels :


0.00 Hrs

Skills :

0.70 MHrs

1 AF 831 841

ZL-831-01-1

FWD PASSENGER/CREW DOOR GENERAL VISUAL INSPECTION OF FWD PASSENGER/CREW DOOR, INCLUDING DOOR STOPS ON FUSELAGE SIDE ,DOOR SEALS AND SCUFF PLATES (EWIS). Access panels :

831

841

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [56 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-831-02-1

831 841

Task Title


Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052830-200-802

ALL

GVI

Check : 1C

N

AMM 052830-200-812

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF FWD PASSENGER/CREW DOOR (EWIS). PREP. : INSULATION; Access panels :

831 831GZ 841DZ

831AZ 831HZ 841EZ

Total access time :

831BZ 831JZ 841FZ

831CZ 841 841GZ

831DZ 841AZ 841HZ

831EZ 841BZ 841JZ

831FZ 841CZ

0.00 Hrs

Skills :

0.80 MHrs

1 AF 832 842

ZL-832-01-1

MID PASSENGER / CREW DOOR GENERAL VISUAL INSPECTION OF MID PASSENGER / CREW DOOR (INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SCUFF PLATES) (EWIS). Access panels :

832

842

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [57 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-832-02-1

832 842

Task Title

MID PASSENGER / CREW DOOR

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052830-200-813

ALL

GVI

Check : 1C

N

AMM 052830-200-814

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF MID PASSENGER / CREW DOOR (EWIS). PREP. : INSULATION; Access panels :

832 832GZ 842DZ

832AZ 832HZ 842EZ

Total access time :

832BZ 832JZ 842FZ

832CZ 842 842GZ

832DZ 842AZ 842HZ

832EZ 842BZ 842JZ

832FZ 842CZ

0.00 Hrs

Skills :

0.80 MHrs

1 AF 833 843

ZL-833-01-1

AFT PASSENGER / CREW DOOR GENERAL VISUAL INSPECTION OF AFT PASSENGER / CREW DOOR, INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SCUFF PLATES (EWIS). Access panels :

833

843

Total access time :

0.00 Hrs

Skills :

0.40 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [58 / 60] ATA

: 00


00

GENERAL

Task Number

Zone

ZL-833-02-1

833 843

Task Title

AFT PASSENGER / CREW DOOR

Task code

Threshold Interval

GVI

Check : 8C

N

AMM 052830-200-815

ALL

GVI

Check : 1C

N

AMM 052830-200-809

ALL

References

Ctrl

Eff

GENERAL VISUAL INSPECTION OF AFT PASSENGER / CREW DOOR (EWIS). PREP. : INSULATION; Access panels :

833 833GZ 843DZ

833AZ 833HZ 843EZ

Total access time :

833BZ 833JZ 843FZ

833CZ 843 843GZ

833DZ 843AZ 843HZ

833EZ 843BZ 843JZ

833FZ 843CZ

0.00 Hrs

Skills :

0.80 MHrs

1 AF 834 844

ZL-834-01-1

EMERGENCY EXIT GENERAL VISUAL INSPECTION OF EMERGENCY EXIT (INCLUDING DOOR STOPS ON FUSELAGE SIDE ,DOOR SEALS AND SCUFF PLATES) (EWIS). Access panels :

834

844

Total access time :

0.00 Hrs

Skills :

0.20 MHrs

1 AF

Issue No

:

Date

:

10 01/12/2013

Amendment No Date

: 01 : 06/09/2014

Page : ZNL - 00 [59 / 60] ATA

: 00

AMS A330 I10 A01

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