Airbus 319, A320, A321 Fcom

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318/319/320/321 FCOM VOL.1 REV035

CROSS REFERENCE TABLE

THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE BETWEEN : - THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES - THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS INDUSTRIE. ---------------------------------------------------------------------------MSN REGISTRATION ---------------------------------------------------------------------------1068 1145

OO-SSB OO-SSF

CCM 01 DEC 2002

1.00.70 PAGE : CRT001

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1 20 10

001

103 REV035

24105=(24105+US)

- TECHNICAL AMENDMENT 1)Description updated, to indicate that the aircraft is equipped with one observer seat. 1 20 20

002

001 REV035 - TECHNICAL AMENDMENT Modification of the >Antennas Location> drawing to : 1)Correctly position the TCAS antennas. 2)Add the SATCOM antenna.

1 21 10

015

001 REV035 - TECHNICAL AMENDMENT 1)Deletion of the forward cargo heating note, as the forward cargo heating option is not installed. 2)Minor text modifications for improved technical understanding and FCOM standardization.

1 21 20

007

001 REV035 - TECHNICAL AMENDMENT 1)Deletion of reference to the forward cargo outlet isolation valve, since forward cargo ventilation is not installed.

1 21 20

009

001 REV035 - TECHNICAL AMENDMENT 1)Deletion of reference to the forward cargo outlet isolation valve, since forward cargo ventilation is not installed.

1 21 20

013

001 REV035 - TECHNICAL AMENDMENT 1)Deletion of the forward passenger door airstairs indication, as it is not installed.

1 22 10

012

100 REV028

27256

- INCORPORATION OF MOD 27256 - DELETION OF MOD 27541 1 22 10

016

100 REV026

M:27256=27541=(27256+27541)

- DELETION OF MOD 27541 1 22 20

002

110 REV032

1 22 20

005

110 REV026

CODE 0072

- DELETION OF MOD 30635 CODE 0072

- DELETION OF MOD 30635 01 DEC 2002

CCM

1.00.75

PAGE

1

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035


006

110 REV026

CODE 0072


008

100 REV026

CODE 0072


014

110 REV028

CODE 0207


023

001 REV035

CODE 0358

- TECHNICAL AMENDMENT 1)No technical change. Page covering the Honeywell or Thales-Smiths FMS2 introduction. 1 22 20

025

001 REV035

CODE 0358


026B

001 REV035

CODE 0358

- TECHNICAL AMENDMENT 1)No technical change. New page introduced for repagination purposes. 1 22 20

027

001 REV035

CODE 0358

- TECHNICAL AMENDMENT 1)Page moved for repagination purposes. 2)Information regarding the PERF factor for CFM 56-5B engines has been moved from the previous and next page. 3)Some figures have been corrected for CFM 56-5B engines. 1 22 30

042

205 REV035

CODE 0377

- TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure correct validity to all customers. 1 22 30

051

001 REV035

STD=(20701+23892)


052

001 REV035

CODE 0387

- TECHNICAL AMENDMENT 1)No technical change. Page covering the Honeywell or Thales-Smiths FMS2 introduction.

01 DEC 2002

CCM

1.00.75

PAGE

2

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035


056

115 REV035 -

1 22 30

056A

CODE 0416

INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION

100 REV035

OF OF OF OF OF

MOD MOD MOD MOD MOD

25205 26111 26485 30241 30631

25863

- INCORPORATION OF MOD 25863 - TECHNICAL AMENDMENT 1)No technical change. New page created for repagination purposes. 1 22 30

057

100 REV035

CODE 0379

- INCORPORATION OF MOD 24160 - INCORPORATION OF MOD 24211 - TECHNICAL AMENDMENT 1)No technical change. New page created for repagination purposes. 1 22 30

071

200 REV025

CODE 0389


005

120 REV035 -

1 23 20

005

24215=24588=25534 CFM:ALL

INCORPORATION OF MOD 24215 INCORPORATION OF MOD 25534 VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers.

100 REV035

27699=(27699+31907)

- TECHNICAL AMENDMENT 1)Note added to explain the procedure to couple the DME reception to the ILS or MLS reception. 1 25 00

001

001 REV035 - TECHNICAL AMENDMENT 1)Page updated to reflect the new cockpit door security chapter configuration.

1 25 20

001

001 REV035 - TECHNICAL AMENDMENT 1)Page modified to address the Cockpit Door Surveillance System.

1 26 20

001

005 REV024

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE

01 DEC 2002

CCM

1.00.75

PAGE

3

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035


002

102 REV035

22561=(20067+20069+22561)

- INCORPORATION OF MOD 22561 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers. 1 26 50

003

410 REV035

CODE 0324

- TECHNICAL AMENDMENT 1)Revision of the DISCH light description to emphasize that the amber >DISCH> light does not come on as soon as the DISCH pushbutton is pressed, but takes about 60 seconds, which is the approximate agent bottle discharge time. 1 27 20

008

005 REV023

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 1 27 40

001

001 REV035 - TECHNICAL AMENDMENT 1)Information has been moved from 1-27-40, page 2.

1 27 40

002

001 REV035 - TECHNICAL AMENDMENT 1)Text modified for improved technical understanding and standardization. 2)The description of the pitch trim wheel has been enhanced to highlight the fact that, in flight, the relation between the aircraft CG and trim position displayed on the wheel does not apply. 3)Information has been moved to 1-27-40 p1.

1 27 50

003

001 REV035 - TECHNICAL AMENDMENT 1)Reference to a specific VFE value has been deleted, in order to have a common page for aircraft having higher VFE.

1 28 10

006

105 REV023

1 28 20

012

105 REV023

1 31 10

002

001 REV035

CODE 0106/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE M:20024/CFM ALL


- TECHNICAL AMENDMENT 1)A recommendation is added to point out that the level 2 amber cautions must 01 DEC 2002

CCM

1.00.75

PAGE

4

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------be considered as soon as possible (time and situation permitting), to avoid any further degradation of the affected system. 1 31 25

002

005 REV030

CFM ALL


003

005 REV026

CFM ALL


005

005 REV030

1 31 25

006

005 REV030

1 31 25

007

005 REV030

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CFM

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CFM ALL


004

005 REV026

CFM ALL


015

001 REV035 - TECHNICAL AMENDMENT 1)PFD drawing improved. 2)Page modified to highlight the fact that vertical speed is not only inertial, but based on both inertial and barometric data.

1 31 40

022

100 REV034

1 31 40

028

100 REV034

1 31 45

018

101 REV035

CODE 0331

- INCORPORATION OF MOD 26485 CODE 0331

- INCORPORATION OF MOD 26485 M:26526=(26526+28308+28811)

- TECHNICAL AMENDMENT 1)Text moved to 1-34-70, page 8, and slightly modified for improved technical understanding. 1 31 45

018

200 REV035

M:26526+28308

- TECHNICAL AMENDMENT 1)Text moved to 1-34-70, page 8, and slightly modified for improved technical understanding. 1 31 45

021

200 REV035

CODE 0183

- TECHNICAL AMENDMENT 1)Page modified to include the overflow arrow in the item 9 description. 2)Information has been moved to the next 01 DEC 2002

CCM

1.00.75

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5

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------page to accommodate additional text on this page. 1 31 45

022

100 REV035 -

1 34 10

001

1 34 10

003

009

CODE 0010

INCORPORATION INCORPORATION INCORPORATION INCORPORATION

100 REV023 -

1 34 10

INCORPORATION OF MOD 22536 INCORPORATION OF MOD 23227 INCORPORATION OF MOD 23529 TECHNICAL AMENDMENT 1)Text moved from the previous page to accommodate additional information on page 21.

203 REV023 -

M:22536=23227=23529

MOD MOD MOD MOD

23510 26999 28382 28495

MOD MOD MOD MOD MOD MOD MOD MOD MOD MOD MOD MOD

23885 24075 25205 26111 26485 26999 27646 28382 28495 30241 30631 30635

CODE 0407

INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION

001 REV025

OF OF OF OF

OF OF OF OF OF OF OF OF OF OF OF OF

STD=M:23450=(23450+20406)

- TECHNICAL AMENDMENT MEMO DISPLAY UPDATED 1 34 15

003

110 REV032 -

1 34 30

003

CODE:0101

INCORPORATION OF MOD 27646 DELETION OF MOD 30241 DELETION OF MOD 30631 DELETION OF MOD 30635

200 REV025

CODE 0077

- INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 - DELETION OF MOD 27646 1 34 60

003

100 REV035

CODE 0013

- TECHNICAL AMENDMENT 1)A note has been added to indicate that, if the selected weather radar fails when two weather radars are installed, the PWS function is recovered by selecting the non-failed weather radar on the control panel. 1 34 70

001

109 REV035

CODE 0230

- TECHNICAL AMENDMENT 01 DEC 2002

CCM

1.00.75

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6

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1)Suppression of the Geometric Altitude description that was inadvertently introduced on this page. 2)TAD and TCF have been added to the list of events that can cause the GPWS light to come on. 3)Text modified for improved technical understanding. 1 34 70

002

103 REV035

26526

- TECHNICAL AMENDMENT 1)Page updated to further specify the aircraft definition : GPWS / G/S pushbuttons on the glareshield. 1 34 70

006

001 REV035 - TECHNICAL AMENDMENT 1)The conditions for activating GPWS Modes 4A and 4B have been revised to reflect the actual design. 2)Addition of a note to highlight the fact that the upper operational limit is reduced to 800 feet, when an overflight is detected.

1 34 70

007

103 REV035

M:26526

- TECHNICAL AMENDMENT 1)Page modified to explain that the glideslope alert is normally only triggered with the gear down, except for a few airports. 2)Addition of a note to explain the fact that the upper operational limit of the Mode 4C warning envelope linearly depends on the aircraft speed. 1 34 70

008

100 REV035

MOD 28244 OR (26526 + 28244)

- TECHNICAL AMENDMENT 1)Text moved from 1-31-45 page 18, for improved technical understanding. 1 34 97

001

206 REV035

CODE 0399

- INCORPORATION OF MOD 28382 - INCORPORATION OF MOD 28495 1 34 97

001

206 REV025

CODE 0051


001

206 REV035

CODE 0399

- TECHNICAL AMENDMENT 1)The DDRMI has been moved to the NAVAIDS section for improved technical understanding and standardization. 1 36 10

006

100 REV035

22562=(22562+25888+27609)

- INCORPORATION OF MOD 22562 - TECHNICAL AMENDMENT 1)New page corresponding to the APIC 01 DEC 2002

CCM

1.00.75

PAGE

7

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------APS 3200 APU : The APU bleed valve is operated by fuel pressure. 1 70 00

001

005 REV023

1 70 00

002

005 REV023

1 70 10

001

120 REV028

CFM ALL


- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CODE:0227/CFM 56-5-B


001

005 REV023

CFM ALL


002

105 REV024

MOD.22238/CFM ALL


005

005 REV028

1 70 20

006

005 REV032

1 70 30

001

105 REV023

CFM ALL


- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE MOD.22112/CFM ALL


002

005 REV023

CFM=PW


003

005 REV023

CFM=PW


004

105 REV023

1 70 30

005

005 REV023

1 70 30

006

005 REV023

24035 CFM/PW

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CFM=PW

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE STD=M:27441 CFM ALL


001

105 REV024

CODE:0204/CFM


002

005 REV023

CFM ALL


004

005 REV023

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 01 DEC 2002

CCM

1.00.75

PAGE

8

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035


004

005 REV023

CFM ALL

1 70 40

006

005 REV023

CFM ALL


007

005 REV023

1 70 50

001

005 REV023

1 70 60

001

005 REV023

CFM ALL




002

005 REV023

CFM ALL


001

005 REV023

CFM ALL


003

106 REV028

1 70 80

002

005 REV031

1 70 80

003

005 REV031

M:25404/CFM ALL




004

005 REV023

CFM ALL


006

005 REV023

CFM ALL


001

005 REV023

1 70 90

002

005 REV031

1 70 90

003

005 REV024

CFM ALL




004

005 REV023

CFM ALL


01 DEC 2002

CCM

1.00.75

PAGE

9

318/319/320/321 FCOM

VOL. 1

SYSTEMS DESCRIPTION

HIGHLIGHTS

REV035


005

105 REV033

CODE 0062/CFM ALL


006

025 REV023

CFM56-5-B


007

005 REV033

CFM ALL


008

148 REV033

1 70 90

009

118 REV033

1 70 90

010

107 REV028

22707/CFM 56-5-B

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CODE 0061/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE M:22707/CFM ALL


011

005 REV023

CFM ALL


012

105 REV023

MOD.22707/CFM ALL


014

146 REV035

26017=22634+26017/CFM 56-5-B

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)Correction of the flight phase inhibitions for the ENG 1(2) THR LEVER FAULT procedure. 2)With the FWC E2 Standard, the >ENG REV UNLOCKED> message is only inhibited in flight phase 8. 1 70 90

015

220 REV026

CODE 0042 CFM ALL


01 DEC 2002

CCM

1.00.75

PAGE

10

318/319/320/321 FCOM

VOL.1

(SYSTEMS DESCRIPTION ) LIST OF EFFECTIVE PAGES (LEP) -

-REV 035

M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----------------------------------------------------------------------------------------1 00 00

001

001

REV024

CONTENTS

ALL

1 00 10 1 00 10

001 002

001 001

REV034 REV034

ORGANIZATION OF THE MANUAL

ALL

1 00 10 1 00 10

003 004

001 001

REV024 REV024

ALL

1 00 10

005

001

REV024

R 1 00 20 R 1 00 20

001 002

001 001

REV035 REV035

LIST OF CODES LIST OF CODES

ALL

R 1 00 20 R 1 00 20

003 004

001 001

REV035 REV035


ALL

R 1 00 20 R 1 00 20

005 006

001 001

REV035 REV035


ALL

R 1 00 20 R 1 00 20

007 008

001 001

REV035 REV035


ALL

R 1 00 20 R 1 00 20

009 010

001 001

REV035 REV035


ALL

R 1 00 20 R 1 00 20

011 012

001 001

REV035 REV035


ALL

N 1 00 20 N 1 00 20

013 014

001 001

REV035 REV035


ALL

N 1 00 20 N 1 00 20

015 016

001 001

REV035 REV035


ALL

N 1 00 20

017

001

REV035

LIST OF CODES

ALL

R 1 00 30 R 1 00 30

001 002

001 001

REV027 REV035

LIST OF NORMAL REVISIONS LIST OF NORMAL REVISIONS

ALL

1 00 35

001

001

REV024

RECORD OF TEMPORARY REV.

ALL

R 1 00 36

001

001

REV035

LIST OF EFFECTIVE TR

ALL

1 00 40 1 00 40

001 002

001 001

REV028 REV031

ABBREVIATIONS ABBREVIATIONS

ALL

1 00 40 1 00 40

003 004

001 001

REV031 REV031


ALL

1 00 40 1 00 40

005 006

001 001

REV031 REV031


ALL

1 00 40 1 00 40

007 008

001 001

REV031 REV031


ALL

1 00 40 1 00 40

009 010

001 001

REV031 REV031


ALL

01 DEC 2002

ALL

CCM

1.00.80 PAGE

01

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VOL.1


-REV 035

M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----------------------------------------------------------------------------------------1 00 40 1 00 40

011 012

001 001

REV031 REV031


ALL

1 00 50

001

001

REV023

UNITS CONVERSION TABLE

ALL

1 00 60

001

001

REV023

SYMBOLS

ALL

R 1 00 70

CRT

001

REV035


ALL

R 1 00 75

HL

001

REV035

HIGHLIGHTS

ALL

R 1 00 80

LEP

001

REV035

LIST OF EFFECTIVE PAGES

ALL

R 1 00 85

LOM

001

REV035

LIST OF MODIFICATIONS

ALL

1 20 00

001

001

REV023

R 1 20 10

001

103

REV035

24105=(24105+US)

ALL

R 1 20 20 R 1 20 20

001 002

100 001

REV031 REV035

M:24105

ALL

1 20 20 1 20 20

003 004

206 103

REV030 REV032

M:20268+24105 M:24105

ALL

1 21 00

001

001

REV030

ALL

1 21 10 1 21 10

001 002

001 001

REV023 REV023

ALL

1 21 10 1 21 10

003 004

001 105

REV023 REV028

M:26363

1 21 10 1 21 10

005 006

100 105

REV033 REV028

M:24139=24340=(24139+24340) M:26363

1 21 10 1 21 10

007 008

001 001

REV023 REV024

1 21 10 1 21 10

009 010

100 001

REV034 REV033

26363

ALL

1 21 10 1 21 10

011 012

105 001

REV032 REV033

CODE 0299

ALL

1 21 10 1 21 10

013 014

001 001

REV023 REV023

ALL

R 1 21 10 R 1 21 10

015 016

001 001

REV035 REV023

ALL

1 21 10 1 21 10

017 018

001 001

REV030 REV033

ALL

1 21 10

019

001

REV023

ALL

1 21 20 1 21 20

001 002

001 100

REV032 REV023

01 DEC 2002

ALL

ALL ALL ALL

ALL M:23344

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VOL.1


-REV 035


003 004

001 001

REV033 REV023

1 21 20 1 21 20

005 006

001 001

REV032 REV023

STD=(26251+32221)

R 1 21 20 R 1 21 20

007 008

001 100

REV035 REV032

M:23344

R 1 21 20 R 1 21 20

009 010

001 001

REV035 REV025

ALL

1 21 20 1 21 20

011 012

001 001

REV028 REV024

ALL

R 1 21 20 R 1 21 20

013 014

001 100

REV035 REV026

M:23124

1 21 30 1 21 30

001 002

001 001

REV023 REV023

STD=M:28221=28240

1 21 30 1 21 30

003 004

001 001

REV026 REV026

ALL

1 21 30 1 21 30

005 006

001 001

REV026 REV023

ALL

1 21 30 1 21 30

007 008

001 001

REV023 REV023

STD=M:22190

1 21 30 1 21 30

009 010

001 001

REV023 REV023

STD=M:22190

1 21 30 1 21 30

011 012

001 001

REV023 REV023

STD=M:22190 STD=M:22190

ALL

1 21 30

013

001

REV030

STD=M:22190

ALL

1 21 40 1 21 40

001 002

100 103

REV023 REV023

CODE 0105 20059=30067

ALL

1 21 40 1 21 40

003 004

103 103

REV023 REV023

20059=30067 20059=30067

ALL

1 21 40 1 21 40

005 006

100 110

REV023 REV033

CODE 0082 CODE 0337

ALL

1 21 40 1 21 40

007 008

100 100

REV026 REV023

CODE 0341 M:20057=20059=(20057+20059)

ALL

1 21 50

001

100

REV025

M:21678

ALL

1 22 00 1 22 00

001 002

001 001

REV031 REV025

1 22 10 1 22 10

001 002

001 001

REV032 REV032

01 DEC 2002

ALL ALL ALL

ALL ALL

ALL ALL

ALL ALL CODE 0358

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-REV 035


003 004

001 001

REV025 REV025

1 22 10 1 22 10

005 006

110 001

REV034 REV023

1 22 10 1 22 10

007 008

001 001

REV028 REV024

1 22 10 1 22 10

009 010

001 105

REV024 REV028

M:27541=(27256+27541)

1 22 10 1 22 10

011 012

100 100

REV028 REV028

M:27541=(27256+27541) 27256

1 22 10 1 22 10

013 014

001 001

REV023 REV025

1 22 10 1 22 10

015 016

001 100

REV025 REV026

27256

1 22 10 1 22 10

017 018

100 100

REV034 REV030

23742=(26358+30980) M:23742

1068

1 22 10 1 22 10

017 018

105 100

REV034 REV030

26358 M:23742

1145

1 22 10 1 22 10

019 020

100 100

REV023 REV023

M:23742 M:23742

ALL

1 22 10 1 22 10

021 022

001 200

REV025 REV034

CODE 0177 23742+24414

ALL

1 22 10

023

305

REV034

23585+23742+24414

ALL

1 22 20 1 22 20

001 002

001 110

REV023 REV032

CODE 0378

1 22 20 1 22 20

003 004

110 001

REV034 REV032

CODE 0072

ALL

1 22 20 1 22 20

005 006

110 110

REV026 REV026

CODE 0378 CODE 0378

ALL

1 22 20 1 22 20

007 008

110 100

REV028 REV026

CODE 0016 CODE 0378

ALL

1 22 20 1 22 20

009 010

106 100

REV032 REV032

CODE 0072 CODE 0327

ALL

1 22 20 1 22 20

011 012

100 001

REV027 REV030

CODE 0141

ALL

1 22 20 1 22 20

013 014

100 110

REV025 REV028

CODE 0141 CODE 0207

ALL

1 22 20 1 22 20

015 016

100 001

REV026 REV023

M:24064=24065=24066=24067

ALL

01 DEC 2002

ALL CODE 0296

ALL ALL ALL ALL ALL ALL

ALL

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-REV 035


017 018

001 001

REV025 REV025

1 22 20 1 22 20

019 020

001 001

REV025 REV025

CODE 0358

1 22 20 1 22 20

021 022

001 001

REV027 REV029

CODE 0358

N 1 22 20 N 1 22 20

023 024

001 100

REV035 REV034

CODE 0358 24064=24065=24066=24067

ALL

N 1 22 20 N 1 22 20

025 026

001 001

REV035 REV032

CODE 0358

ALL

N 1 22 20

026B

001

REV035

CODE 0358

ALL

N 1 22 20 N 1 22 20

027 028

001 001

REV035 REV034

CODE 0358

ALL

1 22 20 1 22 20

029 030

100 001

REV030 REV030

M:24035=24160=(24189+24211) CODE 0358

ALL

1 22 30 1 22 30

001 002

100 100

REV033 REV026

24035=24160=24211 M:24035=24160=24211

ALL

1 22 30 1 22 30

003 004

001 215

REV031 REV026

CODE 0001

1 22 30 1 22 30

005 006

100 100

REV025 REV029

M:24035=24160=24189 M:26497

1 22 30 1 22 30

007 008

001 303

REV025 REV034

CODE 0233

1 22 30 1 22 30

009 010

001 001

REV023 REV032

1 22 30 1 22 30

011 012

001 001

REV026 REV025

CODE 0358

1 22 30 1 22 30

013 014

001 001

REV025 REV025

CODE 0358

1 22 30 1 22 30

015 016

100 001

REV033 REV025

24035=24160=24211

1 22 30 1 22 30

017 018

001 100

REV025 REV027

M:24035=24160=24211

1 22 30 1 22 30

019 020

001 001

REV025 REV025

CODE 0358

1 22 30 1 22 30

021 022

001 100

REV032 REV026

M:24035=24160=24211

1 22 30 1 22 30

023 024

001 001

REV025 REV023

01 DEC 2002

ALL ALL ALL

ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

CCM

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05

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-REV 035


025 026

001 001

REV030 REV030

1 22 30 1 22 30

027 028

100 100

REV025 REV026

1 22 30 1 22 30

029 030

001 001

REV025 REV025

1 22 30 1 22 30

031 032

100 100

REV025 REV025

M:24064=24065=24066=24067 M:26497

ALL

1 22 30 1 22 30

033 034

100 105

REV034 REV034

24035=24160=24211 CODE 0243

ALL

1 22 30 1 22 30

035 036

200 100

REV025 REV025

CODE 0109 M:24035=24160=24211

ALL

1 22 30 1 22 30

037 038

300 210

REV026 REV028

CODE 0032 CODE 0236

ALL

1 22 30 1 22 30

039 040

100 105

REV023 REV028

CODE 0374 CODE 0237

ALL

1 22 30

040A

001

REV032

1 22 30

040B

100

REV026

M:24035=24160=24211

ALL

N 1 22 30 N 1 22 30

041 042

203 205

REV028 REV035

CODE:0002 CODE 0377

ALL

1 22 30 1 22 30

043 044

200 200

REV028 REV028

CODE 0234 CODE 0234

ALL

1 22 30 1 22 30

045 046

100 001

REV025 REV025

M:26497

ALL

1 22 30 1 22 30

047 048

200 100

REV025 REV025

CODE 0380 M:24035=24160=24211

ALL

1 22 30 1 22 30

049 050

001 001

REV025 REV030

N 1 22 30 N 1 22 30

051 052

001 001

REV035 REV035

1 22 30

052A

001

REV033

1 22 30 1 22 30

053 054

100 200

REV030 REV027

26017 CODE 0238

N 1 22 30 N 1 22 30

055 056

001 115

REV033 REV035

CODE 0416

N 1 22 30

056A

100

REV035

25863

ALL

N 1 22 30 N 1 22 30

057 058

100 001

REV035 REV025

CODE 0379

ALL

01 DEC 2002

ALL M:24035=24160=24211 M:24035=24160=24211

ALL ALL

ALL

ALL STD=(20701+23892) CODE 0387

ALL ALL ALL ALL

CCM

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-REV 035


059 060

001 001

REV023 REV028

1 22 30 1 22 30

061 062

001 200

REV028 REV031

CODE 0034

1 22 30 1 22 30

063 064

100 100

REV031 REV023

M:24035=24160=24189 M:24035=24160=24211

ALL

1 22 30 1 22 30

065 066

100 001

REV034 REV025

24035=24160=24211 CODE 0358

ALL

1 22 30 1 22 30

067 068

100 100

REV034 REV034

CODE 0388 22013=24105=25225

ALL

1 22 30 1 22 30

069 070

100 106

REV028 REV032

M:24035=24160=24189 M:24035=24160=(24189+24211)

ALL

1 22 30 1 22 30

071 072

200 100

REV025 REV023

CODE 0389 M:24035=24160=24211

ALL

1 22 30 1 22 30

073 074

100 100

REV032 REV023

CODE 0379 M:24035=24160=24211

ALL

1 22 30 1 22 30

075 076

100 100

REV023 REV025

CODE 0026 CODE 0379

ALL

1 22 40 1 22 40

001 002

001 001

REV025 REV025

1 22 40 1 22 40

003 004

110 001

REV026 REV024

M:24105

ALL

N 1 22 40 N 1 22 40

005 006

120 100

REV035 REV025

24215=24588=25534 CFM:ALL M:22249

ALL

1 22 45 1 22 45

001 002

100 100

REV024 REV024

CODE 0017 CODE 0017

ALL

1 22 45 1 22 45

003 004

100 100

REV024 REV024

CODE 0017 CODE 0017

ALL

1 22 45 1 22 45

005 006

100 100

REV024 REV024

CODE 0017 CODE 0017

ALL

1 22 45 1 22 45

007 008

100 100

REV024 REV024

CODE 0017 CODE 0017

ALL

1 22 46 1 22 46

001 002

100 100

REV024 REV024

CODE 0256 CODE 0024

ALL

1 22 60 1 22 60

001 002

200 001

REV032 REV032

CODE 0148

ALL

1 22 75

001

100

REV023

1 23 00 1 23 00

001 002

001 001

REV031 REV030

01 DEC 2002

ALL ALL

ALL

ALL CODE 0192

CCM

ALL

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VOL.1


-REV 035


001 002

001 001

REV023 REV033

ALL

1 23 10 1 23 10

003 004

001 001

REV026 REV026

ALL

1 23 10

005

100

REV023

1 23 20 1 23 20

001 002

001 001

REV023 REV023

ALL

1 23 20 1 23 20

003 004

001 001

REV023 REV028

ALL

R 1 23 20 R 1 23 20

005 006

100 001

REV035 REV026

1 23 20 1 23 20

007 008

001 001

REV023 REV023

ALL

1 23 20 1 23 20

009 010

001 001

REV026 REV028

ALL

1 23 20 1 23 20

011 012

001 001

REV023 REV026

ALL

1 23 20 1 23 20

013 014

001 001

REV023 REV026

ALL

1 23 20 1 23 20

015 016

100 100

REV023 REV032

1 23 20 1 23 20

017 018

001 001

REV029 REV024

ALL

1 23 20 1 23 20

019 020

001 002

REV032 REV024

ALL

1 23 30 1 23 30

001 002

205 001

REV028 REV034

CODE:0168 STD

ALL

1 23 40 1 23 40

001 002

100 100

REV025 REV025

CODE 0075 CODE:0075

ALL

1 23 40 1 23 40

003 004

100 100

REV028 REV028

CODE 0075 CODE 0075

ALL

1 23 40 1 23 40

005 006

100 100

REV025 REV025

CODE 0075 CODE 0075

ALL

1 23 40 1 23 40

007 008

100 100

REV025 REV025

CODE 0075 CODE 0075

ALL

1 23 50

001

001

REV023

ALL

1 23 60

001

001

REV023

ALL

1 24 00

001

001

REV023

ALL

01 DEC 2002

M:20137

27699=(27699+31907)

M:20308=26023=26433=MPK4453 22013=24105=K5070

CCM

ALL

ALL

ALL

1.00.80 PAGE

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-REV 035


001 002

001 001

REV023 REV023

1 24 10 1 24 10

003 004

001 100

REV023 REV031

1 24 10 1 24 10

005 006

001 001

REV023 REV023

ALL

1 24 10 1 24 10

007 008

001 001

REV023 REV023

ALL

1 24 10 1 24 10

009 010

001 001

REV023 REV023

ALL

1 24 10 1 24 10

011 012

001 001

REV023 REV023

ALL

1 24 10 1 24 10

013 014

100 100

REV025 REV023

1 24 10 1 24 10

015 016

001 001

REV023 REV023

ALL

1 24 10 1 24 10

017 018

001 001

REV027 REV023

ALL

1 24 10

019

100

REV025

M:22013=24105=28160

ALL

1 24 20 1 24 20

001 002

200 200

REV028 REV023

M:21230+27498 M:21230+21213

ALL

1 24 20 1 24 20

003 004

001 100

REV023 REV028

M:27498

1 24 20 1 24 20

005 006

001 100

REV023 REV025

M:22013=24105=28160

1 24 20 1 24 20

007 008

001 001

REV023 REV023

ALL

1 24 20 1 24 20

009 010

001 001

REV023 REV023

ALL

1 24 20 1 24 20

011 012

001 001

REV023 REV023

ALL

1 24 20 1 24 20

013 014

001 001

REV023 REV023

ALL

1 24 20 1 24 20

015 016

001 001

REV032 REV023

STD=(IAE ALL+25409)=25409

1 24 20 1 24 20

017 018

001 100

REV023 REV033

25999

R 1 25 00

001

001

REV035

01 DEC 2002

ALL ALL M:22013=24105=28160

M:22013=24105=28160 M:22013=24105=28160

ALL

ALL ALL

ALL ALL ALL

CCM

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-REV 035


001 002

001 001

REV031 REV034

1 25 10 1 25 10

003 004

100 001

REV034 REV033

20047=20255=23577

1 25 10 1 25 10

005 006

001 100

REV033 REV023

M:22941

1 25 10 1 25 10

007 008

001 001

REV028 REV023

ALL

1 25 10 1 25 10

009 010

001 001

REV023 REV023

ALL

1 25 10 1 25 10

011 012

110 110

REV029 REV029

M:27320 M:27320

ALL

1 25 10 1 25 10

013 014

200 206

REV029 REV031

M:22112+27256 CODE 0278

ALL

1 25 10 1 25 10

015 016

001 001

REV023 REV023

1 25 15

001

001

REV032

R 1 25 20

001

001

REV035

1 26 00

001

100

REV034

CODE 0322

ALL

1 26 10

001

100

REV034

MOD 20067=20069=22006

ALL

1 26 20 1 26 20

001 002

005 001

REV024 REV026

CFM ALL

ALL

1 26 20 1 26 20

003 004

100 001

REV033 REV023

23839

ALL

1 26 20 1 26 20

005 006

100 001

REV026 REV023

M:23839

ALL

1 26 20 1 26 20

007 008

001 001

REV024 REV023

ALL

1 26 20 1 26 20

009 010

001 001

REV023 REV023

ALL

1 26 30 1 26 30

001 002

001 001

REV030 REV023

ALL

1 26 30

003

001

REV023

ALL

N 1 26 40 N 1 26 40

001 002

001 102

REV030 REV035

22561=(20067+20069+22561)

1 26 50 1 26 50

001 002

201 300

REV030 REV023

M:20067+20069 CODE 0320

01 DEC 2002

ALL ALL ALL

ALL STD=27229+27230=27229+27540

ALL ALL

ALL

CCM

ALL

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-REV 035

M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----------------------------------------------------------------------------------------R 1 26 50 R 1 26 50

003 004

410 200

REV035 REV023

CODE 0324 CODE:0056

ALL

1 26 60

001

100

REV030

M:21678

ALL

1 27 00

001

001

REV023

ALL

1 27 10 1 27 10

001 002

001 001

REV034 REV023

ALL

1 27 10 1 27 10

003 004

001 001

REV023 REV023

ALL

1 27 10 1 27 10

005 006

100 001

REV024 REV023

M:22013=24105=26334=26335

ALL

1 27 10 1 27 10

007 008

100 001

REV023 REV023

M:21964

ALL

1 27 10 1 27 10

009 010

105 001

REV028 REV030

M:24105 OR 26334 OR 26335

ALL

1 27 10 1 27 10

011 012

405 100

REV027 REV030

M:24105+24511+24745+27276 CODE 0055

ALL

1 27 10 1 27 10

013 014

001 100

REV030 REV024

M:22013=24105=26334=26335

1 27 10 1 27 10

015 016

001 100

REV023 REV024

M:24105

1 27 10

017

001

REV023

1 27 20 1 27 20

001 002

001 100

REV023 REV023

CODE 0054 M:24136

ALL

N 1 27 20 N 1 27 20

003 004

100 001

REV028 REV023

M:27276 STD=24105

ALL

1 27 20 1 27 20

005 006

001 001

REV030 REV030

1 27 20 1 27 20

007 008

100 005

REV024 REV023

M:22013=24105=26334=26335 CFM ALL

1 27 30 1 27 30

001 002

001 100

REV023 REV023

CODE 0058

1 27 30 1 27 30

003 004

001 001

REV023 REV023

ALL

1 27 30 1 27 30

005 006

001 001

REV032 REV023

ALL

1 27 30

007

001

REV023

ALL

N 1 27 40 N 1 27 40

001 002

001 001

REV035 REV035

ALL

01 DEC 2002

ALL ALL ALL

ALL ALL ALL

CCM

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-REV 035


003 004

100 100

REV025 REV023

M:25296 OR 25477 OR 26540 M:26540=25477

1 27 40 1 27 40

005 006

001 100

REV023 REV024

M:22013=24105=26334=26335

1 27 40 1 27 40

007 008

001 001

REV023 REV023

1 27 40 1 27 40

009 010

100 001

REV033 REV032

22013=24105=26334=26335

ALL

1 27 40 1 27 40

011 012

100 201

REV024 REV033

M:22013=24105=26334=26335 CODE 0297

ALL

1 27 40

013

103

REV026

M:22013=24105=26334=26335

ALL

1 27 50 1 27 50

001 002

001 001

REV023 REV023

STD=M:24105 STD=M:24105

ALL

R 1 27 50 R 1 27 50

003 004

001 001

REV035 REV023

STD=M.24105

1 27 50 1 27 50

005 006

050 001

REV023 REV023

IAE ALL

1 27 50 1 27 50

007 008

001 001

REV023 REV023

ALL

1 27 60

001

001

REV023

ALL

1 28 00

001

001

REV023

ALL

1 28 10 1 28 10

001 002

203 100

REV025 REV025

M.20024+20167 M.20024

ALL

1 28 10 1 28 10

003 004

100 100

REV023 REV024

M.20024 M:20024

ALL

1 28 10 1 28 10

005 006

100 105

REV026 REV023

M:20024 CODE 0106/CFM ALL

ALL

1 28 10 1 28 10

007 008

203 001

REV024 REV023

M:20024+20164

ALL

1 28 10

009

001

REV024

1 28 20 1 28 20

001 002

100 100

REV024 REV024

M:20024 M:20024

ALL

1 28 20 1 28 20

003 004

100 100

REV023 REV023

CODE 0163 M:20164

ALL

1 28 20 1 28 20

005 006

001 100

REV023 REV023

M:20164=(20164+22802)

1 28 20 1 28 20

007 008

100 100

REV023 REV023

M:20164 CODE 0064

01 DEC 2002

ALL ALL ALL

ALL ALL

ALL

ALL

CCM

ALL

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VOL.1


-REV 035


009 010

100 100

REV023 REV025

M:20024 M:20024

ALL

1 28 20 1 28 20

011 012

100 105

REV023 REV023

CODE 0064 M:20024/CFM ALL

ALL

1 28 20

013

203

REV026

M:20024+20164

ALL

1 28 30

001

001

REV025

STD=M:20024

ALL

1 29 00

001

001

REV023

1 29 10 1 29 10

001 002

001 100

REV023 REV023

1 29 10 1 29 10

003 004

001 001

REV023 REV023

1 29 10 1 29 10

005 006

100 100

REV033 REV023

1 29 20 1 29 20

001 002

001 001

REV030 REV025

1 29 20 1 29 20

003 004

001 001

REV027 REV030

1 29 20 1 29 20

005 006

001 001

REV023 REV023

1 29 20 1 29 20

007 008

001 001

REV030 REV031

1 29 30

001

001

REV024

ALL

1 30 00

001

001

REV034

ALL

1 30 10

001

001

REV028

CODE 0132

ALL

1 30 20 1 30 20

001 002

010 001

REV034 REV026

CFM ALL

ALL

1 30 20

003

100

REV034

22875=28558

ALL

1 30 30 1 30 30

001 002

110 100

REV034 REV026

20327/CFM ALL M:20327

ALL

1 30 30

003

100

REV034

22875=28558

ALL

1 30 40 1 30 40

001 002

001 001

REV028 REV023

ALL

1 30 50 1 30 50

001 002

001 001

REV026 REV024

ALL

1 30 60 1 30 60

001 002

100 100

REV032 REV032

1 30 60

003

001

REV023

01 DEC 2002

ALL ALL M:22013=24105=26334=26335 ALL CODE 0306 M:22013=24105=26334=26335

ALL ALL

STD=M:21679=(21591+21679)

ALL ALL

STD=M:23795=(23119+23795)

M:20319 M:20319

ALL

ALL ALL

CCM

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-REV 035


001

101

REV024

M:22875

ALL

1 30 80

001

100

REV023

M:21678

ALL

1 31 00 1 31 00

001 002

001 001

REV023 REV033

ALL

1 31 00

003

001

REV026

ALL

1 31 05 1 31 05

001 002

001 001

REV023 REV023

ALL

1 31 05 1 31 05

003 004

001 001

REV028 REV023

ALL

1 31 05 1 31 05

005 006

001 001

REV032 REV026

ALL

R 1 31 10 R 1 31 10

001 002

001 001

REV023 REV035

ALL

1 31 10 1 31 10

003 004

001 100

REV023 REV031

CODE 0012

1 31 10

005

200

REV031

CODE 0182

1 31 15 1 31 15

001 002

001 001

REV026 REV032

1 31 15 1 31 15

003 004

001 100

REV023 REV033

26017

1 31 15

005

100

REV023

25410

ALL

1 31 20 1 31 20

001 002

100 001

REV026 REV033

M:25409=26018=(25409+26018)

ALL

1 31 20 1 31 20

003 004

100 001

REV028 REV024

M:25409=26018=(25409+26018)

ALL

1 31 20 1 31 20

005 006

002 001

REV034 REV023

CODE 0194

1068

1 31 20 1 31 20

005 006

200 001

REV034 REV023

CODE 0309

1145

1 31 25 1 31 25

001 002

001 005

REV026 REV030

CFM ALL

1 31 25 1 31 25

003 004

005 001

REV026 REV024

CFM ALL

ALL

1 31 25 1 31 25

005 006

005 005

REV030 REV030

CFM ALL CFM

ALL

1 31 25

007

005

REV030

CFM ALL

ALL

1 31 30 1 31 30

001 002

001 002

REV033 REV033

01 DEC 2002

ALL ALL ALL ALL

ALL

ALL

CCM

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VOL.1


-REV 035


003 004

001 001

REV032 REV032

ALL

1 31 30

005

001

REV023

ALL

1 31 40 1 31 40

001 002

001 001

REV026 REV032

ALL

1 31 40 1 31 40

003 004

001 005

REV033 REV026

1 31 40 1 31 40

005 006

001 001

REV024 REV024

ALL

1 31 40 1 31 40

007 008

001 001

REV026 REV026

ALL

1 31 40 1 31 40

009 010

001 001

REV023 REV023

ALL

1 31 40 1 31 40

011 012

001 001

REV033 REV028

CODE:0247

1 31 40 1 31 40

011 012

001 201

REV033 REV028

CODE 0145

1 31 40 1 31 40

013 014

001 100

REV023 REV023

M:22707

R 1 31 40 R 1 31 40

015 016

001 001

REV035 REV024

ALL

1 31 40 1 31 40

017 018

001 001

REV023 REV026

ALL

1 31 40 1 31 40

019 020

001 001

REV024 REV029

ALL

1 31 40 1 31 40

021 022

001 100

REV031 REV034

CODE 0331

1 31 40 1 31 40

023 024

100 001

REV026 REV024

M : 24035=24160=24189

1 31 40 1 31 40

025 026

001 200

REV023 REV034

CODE 0078

1 31 40 1 31 40

027 028

100 100

REV032 REV034

M:26018 CODE 0331

ALL

1 31 40

029

200

REV034

CODE 0044

ALL

1 31 45 1 31 45

001 002

001 001

REV028 REV028

ALL

1 31 45 1 31 45

003 004

001 001

REV028 REV028

ALL

01 DEC 2002

ALL CFM ALL

1068 1145 ALL

ALL ALL ALL

CCM

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-REV 035


005 006

001 100

REV024 REV028

1 31 45 1 31 45

007 008

001 001

REV028 REV024

1 31 45 1 31 45

009 010

100 001

REV034 REV023

CODE 0356

1 31 45 1 31 45

011 012

001 100

REV023 REV023

M:22707

1 31 45 1 31 45

013 014

001 001

REV023 REV024

1 31 45 1 31 45

015 016

001 100

REV029 REV031

CODE 0175

R 1 31 45 R 1 31 45

017 018

101 101

REV032 REV035

M:26526 M:26526=(26526+28308+28811)

1068

R 1 31 45 R 1 31 45

017 018

101 200

REV032 REV035

M:26526 M:26526+28308

1145

1 31 45 1 31 45

019 020

002 100

REV024 REV024

CODE 0175

N 1 31 45 N 1 31 45

021 022

200 100

REV035 REV035

CODE 0183 M:22536=23227=23529

ALL

1 31 50 1 31 50

001 002

001 001

REV029 REV029

STD=M:23450=(20406+23450)

1068

1 31 50 1 31 50

001 002

105 001

REV029 REV029

M:26358=(20406+23450+26358)

1145

1 31 50 1 31 50

003 004

100 001

REV030 REV026

M:26526

ALL

1 31 55 1 31 55

001 002

100 110

REV030 REV026

M:27330 MOD.27330=(24351+25901+27330

ALL

1 31 55 1 31 55

003 004

110 110

REV026 REV032

M:27330=(24351+25901+27330) M. 27330=(24351+25901+27330)

ALL

1 31 60 1 31 60

001 002

001 002

REV033 REV033

STD OR 31647

ALL

1 31 60 1 31 60

003 004

100 110

REV033 REV026

20073 M : 20073

ALL

1 31 65 1 31 65

001 002

001 001

REV023 REV023

ALL

1 31 65 1 31 65

003 004

001 001

REV023 REV023

ALL

1 31 67

001

001

REV023

ALL

01 DEC 2002

ALL CODE:0045 ALL ALL ALL ALL ALL

ALL

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001

001

REV023

1 31 70

001

001

REV032

1 31 75

001

100

REV028

1 32 00

001

001

REV023

1 32 10 1 32 10

001 002

001 001

REV026 REV023

STD=M:20139+22129

ALL

1 32 10 1 32 10

003 004

001 001

REV023 REV023

STD=M:20139+22129

ALL

1 32 10 1 32 10

005 006

001 001

REV023 REV023

STD=M:20139+22129

ALL

1 32 10 1 32 10

007 008

001 001

REV023 REV027

STD=M:20139+22129

ALL

1 32 10 1 32 10

009 010

001 100

REV023 REV030

M:22562

1 32 10 1 32 10

011 012

001 001

REV023 REV029

ALL

1 32 10 1 32 10

013 014

001 001

REV023 REV023

ALL

1 32 10 1 32 10

015 016

100 001

REV030 REV030

1 32 10 1 32 10

017 018

001 001

REV023 REV025

1 32 10 1 32 10

019 020

100 001

REV029 REV023

M:28482

ALL

1 32 10 1 32 10

021 022

001 001

REV024 REV023

STD=M:20139+22129

ALL

1 32 10

023

110

REV029

CODE 0125

ALL

1 32 20 1 32 20

001 002

002 002

REV027 REV027

ALL

1 32 20 1 32 20

003 004

001 001

REV023 REV023

ALL

1 32 20

005

100

REV023

M:24612

ALL

1 32 30 1 32 30

001 002

100 001

REV024 REV025

M:23208=24077=(23208+24077) STD=M:(20139+22129)

ALL

1 32 30 1 32 30

003 004

100 001

REV023 REV023

M:24449

ALL

1 32 30 1 32 30

005 006

001 001

REV023 REV023

STD=M:(20139+22129)

01 DEC 2002

ALL ALL M:21678

ALL ALL

ALL

M:22013=24105=28160 STD=M:20139+22129

ALL ALL

ALL

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-REV 035


007 008

001 100

REV023 REV027

1 32 30 1 32 30

009 010

001 001

REV027 REV023

1 32 30 1 32 30

011 012

001 104

REV023 REV024

1 32 50

001

001

REV025

ALL

1 33 00

001

001

REV032

ALL

1 33 10 1 33 10

001 002

001 100

REV023 REV034

23642

1 33 10 1 33 10

003 004

100 103

REV023 REV024

M:24851 M:24851

ALL

1 33 10 1 33 10

005 006

100 001

REV023 REV034

M:23642

ALL

1 33 10

007

100

REV034

23642

ALL

1 33 20 1 33 20

001 002

001 200

REV023 REV025

M.20042+20081

1 33 20 1 33 20

003 004

303 100

REV024 REV023

CODE 0124 M:20081

1 33 30 1 33 30

001 002

001 103

REV031 REV033

24105

1 33 30 1 33 30

003 004

001 001

REV031 REV025

1 33 40 1 33 40

001 002

205 100

REV033 REV034

CODE 0193 20081

ALL

1 33 50 1 33 50

001 002

100 001

REV034 REV023

24851

ALL

1 34 00 1 34 00

001 002

001 001

REV032 REV029

N 1 34 10 N 1 34 10

001 002

203 001

REV023 REV024

CODE 0010

ALL

N 1 34 10 N 1 34 10

003 004

100 100

REV023 REV023

CODE 0407 CODE 0048

ALL

1 34 10 1 34 10

005 006

001 001

REV025 REV031

ALL

1 34 10 1 34 10

007 008

001 001

REV023 REV033

ALL

1 34 10

009

001

REV025

01 DEC 2002

ALL M:20994 ALL CODE 0332 CODE 0334

ALL

ALL

ALL ALL ALL ALL

ALL

STD=M:23450=(23450+20406)

CCM

ALL

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-REV 035


001 002

110 120

REV026 REV026

CODE:0036 CODE:0036

ALL

1 34 15

003

110

REV032

CODE:0101

ALL

1 34 20 1 34 20

001 002

001 001

REV023 REV033

1 34 20

003

001

REV024

1 34 30 1 34 30

001 002

001 001

REV027 REV023

1 34 30 1 34 30

003 004

200 001

REV025 REV023

CODE 0077 STD OR (20210+31003)

ALL

1 34 30 1 34 30

005 006

001 001

REV023 REV023

STD OR(20210+31003)

ALL

1 34 30 1 34 30

007 008

001 001

REV031 REV031

STD OR M:27531

ALL

1 34 30

009

001

REV032

ALL

1 34 40 1 34 40

001 002

002 001

REV024 REV023

ALL

1 34 50 1 34 50

001 002

121 121

REV031 REV024

CODE:0187 CODE:0211

ALL

1 34 60 1 34 60

001 002

100 100

REV028 REV031

CODE 0261 CODE 0261

ALL

R 1 34 60 R 1 34 60

003 004

100 100

REV035 REV026

CODE 0013 CODE 0013

ALL

R 1 34 70 R 1 34 70

001 002

109 103

REV035 REV035

CODE 0230 26526

ALL

1 34 70 1 34 70

003 004

100 109

REV026 REV025

M:26526 M:26526=(22769+26256)

ALL

R 1 34 70 R 1 34 70

005 006

110 001

REV029 REV035

M:26526 OR (22769+26526)

ALL

R 1 34 70 R 1 34 70

007 008

103 100

REV035 REV035

M:26526 MOD 28244 OR (26526 + 28244)

ALL

1 34 70 1 34 70

009 010

100 103

REV030 REV024

M:26526 M:26526

ALL

1 34 70 1 34 70

011 012

100 100

REV030 REV026

M:26526=(22769+26526) M:26526

ALL

1 34 70 1 34 70

013 014

105 101

REV032 REV027

MOD 28244 OR (26526 + 28244) CODE 0104

ALL

1 34 80 1 34 80

001 002

100 100

REV033 REV023

CODE 0095 CODE 0095

ALL

01 DEC 2002

ALL STD=M:21126

ALL ALL

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003 004

100 100

REV023 REV031

CODE 0095 CODE 0095

ALL

1 34 80 1 34 80

005 006

150 150

REV031 REV028

CODE:0245 CODE 0245

ALL

1 34 80 1 34 80

007 008

210 100

REV031 REV031

CODE 0219 CODE:0246

1068

1 34 80 1 34 80

007 008

210 200

REV031 REV031

CODE 0219 CODE 0128

1145

1 34 80 1 34 80

009 010

100 100

REV023 REV031

CODE 0095 CODE 0095

ALL

1 34 80 1 34 80

011 012

100 150

REV030 REV028

CODE 0095 CODE 0245

ALL

1 34 80

013

100

REV024

CODE 0095

ALL

R 1 34 97

001

206

REV035

CODE 0399

ALL

1 35 00

001

001

REV023

ALL

1 35 10

001

001

REV024

ALL

1 35 20 1 35 20

001 002

001 001

REV028 REV034

ALL

1 35 20 1 35 20

003 004

001 001

REV023 REV034

ALL

1 35 20 1 35 20

005 006

001 001

REV031 REV029

ALL

1 35 20 1 35 20

007 008

001 001

REV032 REV025

ALL

1 35 30 1 35 30

001 002

110 001

REV032 REV023

1 35 30

003

001

REV024

1 35 40 1 35 40

001 002

112 112

REV023 REV023

CODE 0158 CODE:0006

ALL

1 35 50

001

001

REV031

STD=M:25110

ALL

1 36 00

001

001

REV023

ALL

1 36 10 1 36 10

001 002

001 001

REV023 REV023

ALL

1 36 10 1 36 10

003 004

001 050

REV023 REV024

M.24105=IAE ALL=(IAE+24105)

N 1 36 10 N 1 36 10

005 006

001 100

REV028 REV035

22562=(22562+25888+27609)

01 DEC 2002

M:26923=27255=27572

ALL ALL

ALL ALL

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007 008

001 001

REV023 REV023

ALL

1 36 10 1 36 10

009 010

001 001

REV023 REV023

ALL

1 36 20 1 36 20

001 002

001 001

REV023 REV023

ALL

1 36 20 1 36 20

003 004

001 100

REV023 REV023

M:24805

1 36 20 1 36 20

005 006

001 100

REV023 REV023

M:24805

1 36 20

007

001

REV023

1 36 30

001

100

REV023

1 38 00

001

001

REV023

1 38 10 1 38 10

001 002

001 100

REV023 REV025

M:21003

1 38 10 1 38 10

003 004

001 100

REV023 REV034

20109

1 38 10

005

100

REV023

M:20109

ALL

1 38 20

001

100

REV034

MOD 20109

ALL

1 45 00

001

001

REV030

1 45 10 1 45 10

001 002

001 001

REV023 REV023

STD OR (27522+28360)

1 45 10 1 45 10

003 004

100 001

REV032 REV023

23119=22013

1 45 10

005

001

REV023

1 45 20 1 45 20

001 002

001 001

REV023 REV023

STD=M:27522+28360

ALL

1 45 20 1 45 20

003 004

200 001

REV032 REV032

20201+24287

ALL

1 45 20 1 45 20

005 006

001 001

REV023 REV023

ALL

1 45 20 1 45 20

007 008

001 001

REV032 REV023

ALL

1 45 20

009

100

REV023

CODE 0004

ALL

1 45 25

001

100

REV030

M:25293

ALL

1 45 30

001

001

REV023

01 DEC 2002

ALL ALL ALL M:21678

ALL ALL ALL ALL

ALL ALL ALL ALL

ALL

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001

001

REV023

1 49 00

001

001

REV023

1 49 10 1 49 10

001 002

100 001

REV023 REV023

M:22562

ALL

1 49 10

003

100

REV023

M:22562OR(22562+25888+27609)

ALL

1 49 20 1 49 20

001 002

100 100

REV023 REV028

CODE 0027 M:22562OR(22562+25888+27609)

ALL

1 49 20 1 49 20

003 004

001 203

REV023 REV024

M:22562+25409

1 49 20 1 49 20

005 006

103 100

REV032 REV023

M:22562OR(22562+25888+27609) M:22562

ALL

1 49 30

001

100

REV032

M:22013 OR 24105 OR 28160

ALL

1 52 00

001

001

REV023

1 52 10 1 52 10

001 002

106 001

REV023 REV023

1 52 10 1 52 10

003 004

001 001

REV023 REV028

1 52 10 1 52 10

005 006

001 103

REV023 REV032

M:24105

1 52 10 1 52 10

007 008

103 001

REV023 REV034

M:24105=(AFR+24105)

1 52 10 1 52 10

009 010

001 103

REV023 REV025

M:24105

1 52 10

011

103

REV034

24105=30020

ALL

1 52 20 1 52 20

001 002

203 100

REV024 REV034

M:24105+22707 MOD 24105

ALL

1 52 30 1 52 30

001 002

001 001

REV023 REV026

STD=M:(20062+22188) STD=M:(20062+22188)

ALL

1 52 40

001

001

REV023

1 70 00 1 70 00

001 002

005 005

REV023 REV023

CFM ALL CFM ALL

ALL

1 70 10

001

120

REV028

CODE:0227/CFM 56-5-B

ALL

1 70 20 1 70 20

001 002

005 105

REV023 REV024

CFM ALL MOD.22238/CFM ALL

ALL

1 70 20 1 70 20

003 004

001 001

REV023 REV023

01 DEC 2002

ALL ALL

ALL

ALL M:24105

ALL ALL ALL ALL ALL

ALL

ALL

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005 006

005 005

REV028 REV032

CFM ALL CFM ALL

ALL

1 70 30 1 70 30

001 002

105 005

REV023 REV023

MOD.22112/CFM ALL CFM=PW

ALL

1 70 30 1 70 30

003 004

005 105

REV023 REV023

CFM=PW 24035 CFM/PW

ALL

1 70 30 1 70 30

005 006

005 005

REV023 REV023

CFM=PW STD=M:27441 CFM ALL

ALL

1 70 40 1 70 40

001 002

105 005

REV024 REV023

CODE:0204/CFM CFM ALL

ALL

1 70 40 1 70 40

003 004

105 005

REV034 REV023

22238/CFM CFM ALL

ALL

1 70 40 1 70 40

005 006

105 005

REV033 REV023

CODE:0204/CFM CFM ALL

ALL

1 70 40

007

005

REV023

CFM ALL

ALL

1 70 50

001

005

REV023

CFM ALL

ALL

1 70 60 1 70 60

001 002

005 005

REV023 REV023

CFM ALL CFM ALL

ALL

1 70 70 1 70 70

001 002

005 110

REV023 REV031

CFM ALL CODE:0018/CFM

ALL

1 70 70

003

106

REV028

M:25404/CFM ALL

ALL

1 70 80 1 70 80

001 002

001 005

REV023 REV031

CFM

1 70 80 1 70 80

003 004

005 005

REV031 REV023

CFM CFM ALL

ALL

1 70 80 1 70 80

005 006

240 005

REV031 REV023

M:22562+27993/CFM CFM ALL

ALL

1 70 80

007

320

REV032

CODE 0295/CFM

ALL

1 70 90 1 70 90

001 002

005 005

REV023 REV031

CFM ALL CFM

ALL

1 70 90 1 70 90

003 004

005 005

REV024 REV023

CFM ALL CFM ALL

ALL

1 70 90 1 70 90

005 006

105 025

REV033 REV023

CODE 0062/CFM ALL CFM56-5-B

ALL

1 70 90 1 70 90

007 008

005 148

REV033 REV033

CFM ALL 22707/CFM 56-5-B

ALL

1 70 90 1 70 90

009 010

118 107

REV033 REV028

CODE 0061/CFM ALL M:22707/CFM ALL

ALL

01 DEC 2002

ALL

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011 012

005 105

REV023 REV023

CFM ALL MOD.22707/CFM ALL

ALL

R 1 70 90 R 1 70 90

013 014

209 146

REV024 REV035

CODE 0060/CFM ALL 26017=22634+26017/CFM 56-5-B

ALL

1 70 90

015

220

REV026

CODE 0042 CFM ALL

ALL

1 70 98

001

001

REV028

STD=M:20165

ALL

01 DEC 2002

CCM

1.00.80 PAGE

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318/319/320/321 FCOM VOLUME : 1 SYSTEMS DESCRIPTION LIST OF MOD/MP/SB AFFECTING THE MANUAL M V REV T

MOD

MP

REVISION : 035

TITLE

SB

VALIDITY

. 034A ...... K0385 ...........

LIGHTS - CABIN - MODIFY SIGN CONTROL OF FSB ALL

. 034A ...... K4453 ...........

COMMUNICATION - INSTALL AN ALL CABIN ATTENDA CALL PUSH BUTTON IN THE FLIGHT COMPARTMENT ALL

. 034A ...... K5043 ...........

COMMUNICATIONS - CIDS - CABIN CONFIGURATION FOR NON-SMOKING FLIGHTS ALL

N 035

COMMUNICATIONS - DATA LINK SYSTEM DEFINE PIN PROGRAMMING ALL

. 034A ...... P2878 ...........

INDICATING RECORDING SYSTEM - SDAC DEFINE A PIN PROGRAM FOR REAR C.C. VENTILATION ALL

. 034A 20024 ...... ...........

FUEL- INSTALL A CENTRE TANK SYSTEMALL

. 034A 20042 ...... ...........

LIGHTS - EXTERNAL LIGHTS - INSTALL LOGO LIGHTS ALL

. 034A 20059 ...... ...........

AIR CONDITIONING - CARGO COMPARTMENT VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT ALL

. 034A 20067 ...... ...........

FIRE PROTECTION - FWD CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM ALL

. 034A 20069 ...... ...........

FIRE PROTECTION - AFT CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM ALL

. 034A 20071 ...... ...........

FIRE PROTECTION - CARGO COMPARTMENT FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM ALL

...... P0164 ...........

CCM 01 DEC 2002

1.00.85 PAGE

1


MOD

MP

REVISION : 035

TITLE

SB

VALIDITY

. 034A 20073 ...... ...........

INDICATING/RECORDING SYSTEMS INSTALL AN AIRCRAFT INTEGRATED DATA SYSTEM ALL

. 034A 20081 ...... ...........

LIGHTS - EXTERIOR LIGHTS - INSTALL SYNCHRONIZED STROBE LIGHTS ALL

. 034A 20109 ...... ...........

WATER/WASTE- INSTALL VACUUM TOILET SYSTEM ALL

. 034A 20137 ...... ...........

COMMUNICATIONS - RADIO MANAGEMENT INSTALL A 3RD RMP ALL

. 034A 20164 ...... ...........

FUEL - REFUEL/DEFUEL SYSTEM INSTALL A FUEL QUANTITY PRE-SELECTOR IN FLIGHT COMPARTMENT ALL

. 034A 20167 ...... ...........

STRUCTURE - REINFORCE STRUCTURE TO ALLOW MTOW 72T-MLW 63T-MZFW 59T DESIGN WEIGHTS ALL

. 034A 20201 ...... ...........

COMMUNICATIONS-INSTALL DATA LINK SYSTEM ALL

. 034A 20230 ...... ...........

LIGHTS - NAVIGATION LIGHTS - INSTALL A SECOND NAVIGATION LIGHT SYSTEM ALL

. 034A 20268 ...... ...........

WINGS-WING TIP FENCES-INTRODUCE WING TIPS INCLUDING FENCESALL

. 034A 20283 ...... ...........

COMMUNICATIONS - PROVIDE >HOT MIKE> RECORDING ALL

. 034A 20319 ...... ...........

ICE AND RAIN PROTECTION-WINDSHIELD RAIN PROTECTION - ADD AN INTERMITTENT FUNCTION ALL CCM

01 DEC 2002

1.00.85 PAGE

2


MOD

MP

REVISION : 035

TITLE

SB

VALIDITY

. 034A 20324 ...... 28-1030 04

FUEL - COUPLING REFUEL/DEFUEL ADD COUPLING ON LH WING (72T MTOW A/C) ALL

. 034A 20327 ...... ...........

MINOR IMPROVEMENTS INTRODUCED FROM A/C 60 - AS ZONE ALL

. 034A 20994 ...... ...........

LANDING GEAR-WHEELS AND BRAKES-INSTALL BSCU STD5ALL

. 034A 21003 ...... ...........

WATER/WASTE - RELOCATE POTABLE WATER TANK ALL

. 034A 21213 ...... ...........

ELECTRICAL POWER - DC GENERATION REVISE >BAT OFF> INDICATION ALL

. 034A 21230 ...... ...........

ELECTRCIAL POWER - DC - IMPROVE BCL ALL

. 034A 21237 ...... ...........

APU - INTRODUCE APU MODE 6 AND ASSOCIATED ECB (GARRETT) ALL

. 034A 21678 ...... ...........

ELECTRICAL POWER-AC/DC ESSENTIAL POWER DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPSALL

. 034A 21679 ...... ...........

HYDRAULIC POWER-MODIFY ELECTRICAL ROUTING OF GREEN LEAKAGE MEASUREMENT ELECTROVALVE CONTROL ALL

. 034A 21964 ...... ...........

FLIGHT CONTROLS - ELAC/EFCS SYSTEM INTRODUCE SOFTWARE L62 ALL

. 034A 22089 ...... ...........

ENGINE FUEL AND CONTROL - EIU/CFM INTRODUCE SOFTWARE 11 ALL

CCM 01 DEC 2002

1.00.85 PAGE

3


MOD

MP

REVISION : 035

TITLE

SB

VALIDITY

. 034A 22112 ...... ...........

MINOR IMPROVEMENTS INTRODUCED FROM A/C 268 - AS ZONE ALL

. 034A 22238 ...... ...........

ENGINE FUEL AND CONTROL - CFM 56 INTRODUCE EIU VERSION 12 AND ADDITIONAL WIRING ALL

. 034A 22249 ...... ...........

AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION ALL

. 034A 22311 ...... ...........

NAVIGATION - TCAS II - INTRODUCE COMPLETE PROVISIONS ALL

. 034A 22536 ...... ...........

NAVIGATION - INSTALL A BENDIX TCAS II COLLISION AVOIDANCE SYSTEM ALL

. 034A 22561 ...... ...........

FIRE PROTECTION - LAVATORY SMOKE DETECTION - INTRODUCE AMBIENT SYSTEM ALL

. 034A 22562 ...... ...........

AIRBORNE AUXILIARY POWER UNIT INTRODUCE APIC APS-3200 ALL

. 034A 22567 ...... ...........

EQUIPMENT/FURNISHINGS - EMERGENCY EQUIPMENT - INTRODUCE PBE DRAEGER IN THE COCKPIT ALL

N 035

LANDING GEAR - MLG - IMPROVE LOOM SEGREGATION ALL

. 034A 22634 ...... ...........

INDICATING/RECORDING SYSTEMS - CENTRAL WARNING SYSTEM - DEFINE STD FWC FOR A321 ALL

22572 ...... ...........

CCM 01 DEC 2002

1.00.85 PAGE

4


MOD

MP

REVISION : 035

TITLE

SB

VALIDITY

. 034A 22706 ...... ...........

INDICATING/RECORDING SYSTEMS - CENTRAL WARNING SYSTEM - INSTALL SDAC A320/321 STANDARD ALL

. 034A 22707 ...... ...........

INDICATING RECORDING SYSTEMS - EIS DEFINE COF A STANDARD FOR A320/A321 DMC ALL

. 034A 22769 ...... ...........

NAVIGATION - GPWS - INSTALL GPWC MARK V WITH INTERFACE WITH CFDS ALL

. 034A 22875 ...... ...........

ICE AND RAIN PROTECTION - ICE DETECTION INSTALL DUAL ADVISORY ICE DETECTION SYSTEM ALL

. 034A 22941 ...... ...........

EQUIPMENT/FURNISHINGS - COCKPIT SEATS INTRODUCE TYPE A340 SEATS ALL

. 034A 23099 ...... ...........

COMMUNICATIONS - ACARS - INSTALL SUNDSTRAND ACARS MANAGEMENT UNIT BFE ALL

. 034A 23119 ...... ...........

HYDRAULIC POWER-BLUE MAIN HYDRAULIC POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR ALL

. 034A 23124 ...... ...........

AIR CONDITIONING - PRESSURIZATION CONTROL - IMPROVE CONTROLLER TO ENABLE USE OF EXTERNAL MODE ALL

. 034A 23208 ...... ...........

LANDING GEAR - WHEELS AND BRAKES INTRODUCE BSCU STD 6 ALL

. 034A 23344 ...... ...........

AIR CONDITIONING - IMPROVE CABIN PRESSURIZATION CONTROL ON 25VU PANEL. ALL

N 035

NAVIGATION - ADIRS - ADAPT SHELVES FOR 4 MCU ADIRS INSTALLATION ALL

23510 ...... ...........

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. 034A 23577 ...... ...........

EQUIPMENT/FURNISHINGS-COCKPIT SEATSINTRODUCE ADDITIONAL BONDING STRIP ON FOURTH CREW MEMBERHS SEAT ALL

. 034A 23585 ...... ...........

AUTO FLIGHT - FCU - INTRODUCE FCU M-9 STD ALL

. 034A 23642 ...... ...........

LIGHTS - COCKPIT ILLUMINATION INTRODUCE IMPROVED COCKPIT LIGHTING ALL

. 034A 23672 ...... ...........

NAVIGATION - ADIRS - INSTALL LITTON 4MCU ON A321 A/C ALL

. 034A 23742 ...... ...........

AUTO FLIGHT - FCU - INTRODUCE FCU STANDARD M10 ALL

. 034A 23795 ...... ...........

HYDRAULIC POWER - INDICATING - REMOVE SENSOR AND ASSOCIATED WIRING FOR BLUE RESERVOIR INDICATION ALL

. 034A 23839 ...... ...........

FIRE PROTECTION - DETECTION - INTRODUCE MODIFIED ENGINE AND APU FIRE PANEL ALL

. 034A 24035 ...... ...........

INDICATING/RECORDING SYSTEMS GENERAL- DEFINE CPIP3 ALL

. 034A 24064 ...... ...........

AUTO FLIGHT-FMS-INTRODUCE FMGC A320/321 B1 STD WITH OPTIONS AND 400 KILOWORDS FOR CFM 56 VERSIONS ALL

. 034A 24077 ...... ...........

LANDING GEAR - BSCU - TWIN WHEEL INTRODUCE A320/A321 STD 6 VERSION 60C ALL

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. 034A 24084 ...... ...........

AUTO FLIGHT - A320/A321 FOR IAE AND CFM ENGINES - INSTALL WIRING PROVISION FOR ENERGY MANAGEMENT ACTIVATION ALL

. 034A 24105 ...... ...........

FUSELAGE - REAR FUSELAGE - ADAPT SECTION 17/19 STRUCTURE TO A319 DEFINITION ALL

. 034A 24106 ...... ...........

FUSELAGE - DEFINE INTERFACES AND ASSEMBLING OF SECTION 14 TO 15/21 TO A319 DEFINITION ALL

. 034A 24136 ...... ...........

FLIGHT CONTROLS - ELAC SYSTEM INTRODUCE A320/A321 ELAC STD ALL

. 034A 24139 ...... ...........

AIR CONDITIONING - COCKPIT AND CABIN TEMPERATURE CONTROL - INTRODUCE ZONE TEMPERATURE CONTROLLER -03 ALL

. 034A 24215 ...... ...........

AUTO FLIGHT - FAC - INSTALL TWO FACS P/N BAM 0509 ALL

. 034A 24287 ...... ...........

INDICATING/RECORDING SYSTEMS - CFDR INTRODUCE CFDIU STD -7 ALL

. 034A 24351 ...... ...........

INDICATING/RECORDING SYSTEMS ELECTRICAL CLOCK - INSTALL A CLOCK SMITHS TYPE 2610 ALL

. 034A 24414 ...... ...........

AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) DELETE >EXPEDITE> FUNCTION FROM FCU ALL

. 034A 24449 ...... ...........

LANDING GEAR - A320/A321 TWIN WHEELS INTRODUCE BSCU STANDARD 7 (70B VERSION) ALL

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. 034A 24511 ...... ...........

FLIGHT CONTROLS -S.E.C. SYSTEM INTRODUCE A320/A321 S.E.C STANDARD P/N BAM0508 ALL

. 034A 24588 ...... ...........

AUTO FLIGHT-FAC-INTRODUCE FAC P/N BAM 510 ALL

. 034A 24612 ...... ...........

INDICATING/RECORDING SYSTEMS - FWC INTRODUCE FWC D2 STD ALL

. 034A 24613 ...... ...........

FLIGHT CONTROLS - ELAC - INTRODUCE ELAC STD P/N L69 ALL

. 034A 24745 ...... ...........

FLIGHT CONTROLS-SEC SYSTEM->PARTIAL LIFT DUMPING> FUNCTION ACTIVATION ALL

. 034A 24805 ...... ...........

PNEUMATIC-ENGINE BLEED AIR SUPPLYINTRODUCE A BLEED AIR MONITORNG COMPUTER STD6 ALL

. 034A 24851 ...... ...........

ICE AND RAIN PROTECTION-ICE DETECTIONPROVIDE ICE DETECTOR ILLUMINATION ALL

N 035

NAVIGATION-ADIRU-INTRODUCE ADIRU P/N -307 ALL

. 034A 24917 ...... ...........

FLIGHT CONTROLS-INTRODUCE ELAC STD L69J ALL

. 034A 25184 ...... ...........

NAVIGATION-TCAS-INSTALL ATC/TCAS CONTROL PANEL SEXTANT P/N 04-AA01. ALL

. 034A 25287 ...... ...........

POWERPLANT - GENERAL - INSTALL ON A319 ENGINE RATED VERSION OF CFM 56-5B6 23500 LBS ALL

24852 ...... ...........

CCM 01 DEC 2002

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. 034A 25293 ...... ...........

INDICATING/RECORDING SYSTEM - INSTALL A PORTABLE DATA LOADER CONNECTOR AND DISK STOWAGE ALL

. 034A 25294 ...... ...........

NAVIGATION - ADIRS - INSTALL HONEYWELL ADIRS CAPABLE OF A319 A/C ALL

. 034A 25295 ...... ...........

AUTOFLIGHT - FMGC - ACTIVATE ACARS INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 034A 25296 ...... ...........

FLIGHT CONTROLS - FCDC SYSTEM - PROVIDE A VISUAL INDICATION FOR SIMULTANEOUS SIDE STICK ACTION ALL

. 034A 25335 ...... ...........

FLIGHT CONTROLS-ELAC-INTRODUCE A319 EIS L77 SOFTWARE STDALL

. 034A 25336 ...... ...........

NAVIGATION-ADIRS-INTRODUCE AIRU LITTON P/N -308 ALL

. 034A 25345 ...... ...........

AUTOFLIGHT-FCU-INTRODUCE F.C.U. STANDARD M11 ALL

. 034A 25346 ...... ...........

AUTOFLIGHT-FCU-INTRODUCE FCU STANDARD M11 WITHOUT EXPEDITE FUNCTION ALL

. 034A 25381 ...... ...........

AUTOFLIGHT - FMGC - ACTIVATE PRINTER INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 034A 25404 ...... ...........

EXHAUST-THRUST REVERSER CONTROL AND INDICATING-ACTIVATE ADDITIONAL THRUST REVERSER LOCK CONTROL ALL

CCM 01 DEC 2002

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. 034A 25409 ...... ...........

INDICATING RECORDING SYSTEMS-DMCINTRODUCE D.M.C. V31 STANDARD ALL

. 034A 25410 ...... ...........

INDICATING RECORDING SYSTEM-FWCINTRODUCE F.W.C. E1 STANDARD ALL

. 034A 25419 ...... ...........

ICE AND RAIN PROTECTION-WINDSHIELD RAIN PROTECTION-DESACTIVATION OF RAIN REPELLENT SYSTEM ALL

. 034A 25440 ...... ...........

NAVIGATION - GENERAL - CHANGE EQUIPMENTS TO COMPLY WITH MARCH 95 SPECS. ALL

. 034A 25529 ...... ...........

NAVIGATION - WEATHER RADAR SYSTEM ACTIVATE PREDICTIVE WINDSHEAR FUNCTION ALL

. 034A 25530 ...... ...........

ENGINE - COMBUSTION SECTION INTRODUCE DOUBLE ANNULAR COMBUSTOR ON CFM56-5B6 (CFM56-5B6/2) ALL

. 034A 25863 ...... ...........

AUTO FLIGHT - FCU - DEFINE FLIGHT DIRECTOR ENGAGEMENT IN CROSSED BARS AT GO AROUND ALL

. 034A 25871 ...... ...........

ENGINE FUEL AND CONTROL-CONTROLLINGINTRODUCE ECU SOFTWARE 5DH FOR CFM56-5B (DAC -DAC/P) ENGINES ALL

. 034A 25894 ...... ...........

FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ELAC SOFTWARE STD L78 ALL

. 034A 25901 ...... ...........

INDICATING/RECORDING SYSTEMS-ELECTRICAL CLOCK- INSTALL SEXTANT CLOCK IN PLACE OF SMITHS BASIC CLOCK OO-SSB

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. 034A 25999 ...... ...........

ELECTRICAL POWER-DC GENERATIONMODIFY TRANSFORMER RECTIFIER OVERHEAT PROTECTION ALL

. 034A 26000 ...... ...........

NAVIGATION-ADIRS-INTRODUCE HONEYWELL ADIRU 4 MCU STD WITH HARDWARE P/N AD09 ALL

. 034A 26001 ...... ...........

NAVIGATION-ADIRS-INTRODUCE HONEYWELL 4 MCU P/N AC09 ALL

. 034A 26002 ...... ...........

NAVIGATION-ADIRS-INTRODUCE LITTON ADIRU 4 MCU STD WITH P/N-309 (AIME FUNCTION) ALL

. 034A 26017 ...... ...........

INDICATING/RECORDING SYSTEMS-FLIGHT WARNING COMPUTER (FWC)-INTRODUCE FWC ST2 E2 ALL

. 034A 26018 ...... ...........

INDICATING/RECORDING SYSTEMS-DISPLAY MANAGEMENT COMPUTER (DMC)-INTRODCUE DMC V32 STD ALL

. 034A 26194 ...... ...........

NAVIGATION - WEATHER RADAR SYSTEM ALLIED SIGNAL CONFIGURATION AND FULL PROVISION FOR A SECOND TRANSCEIVER ALL

. 034A 26203 ...... ...........

COMMUNICATIONS - SSCVR - INSTALL SSCVR ALLIED SIGNAL P/N 980-6022-001 ALL

. 034A 26250 ...... ...........

WATER/WASTE-TOILET SYSTEM-INTRODUCE MODIFIED TOILET ASSY ALL

. 034A 26274 ...... ...........

NAVIGATION - ADF - INSTALL A SECOND ADF RECEIVERS ALL

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. 034B 26275 ...... ...........

NAVIGATION-WEATHER RADAR SYSTEMINSTALL FULL PROVISION FOR 2ND TRANSCEIVER OO-SSF

. 034B 26358 ...... ...........

AUTOFLIGHT-FLIGHT CONTROL UNIT(FCU) INTRODUCE SEXTANT MODULAR FCU OO-SSF

. 034A 26363 ...... ...........

AIR CONDITIONING-AIR COOLING SYSTEMINTRODUCE MODIFIED RAM AIR OUTLET ALL

. 034A 26497 ...... ...........

AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL SPEED PROTECTION AND F/D DISENGAGEMENT UPON SPEED CONSTRAINTS ALL

. 034A 26526 ...... ...........

NAVIGATION - GPWS - ACTIVATE ENHANCED FUNCTIONS OF THE EGPWS ALL

. 034A 26540 ...... ...........

INDICATING/RECORDING SYSTEMS - FWC PROVIDE NEW SYNTHETIC VOICE >DUAL INPUT> ALL

. 034A 26923 ...... ...........

OXYGEN-PASSENGER OXYGEN-INTRODUCE MODIFIED CHEMICAL OXYGEN CONTAINER (DRAEGER) P/N -0004 ALL

. 034A 26963 ...... ...........

ICE AND RAIN PROTECTION-WINSHIELD RAIN PROTECTION-ACTIVATION OF RAIN REPELLENT SYS.(FLUID COMPATIBLE WITH OZONE RULES) ALL

. 034A 26968 ...... ...........

AUTO FLIGHT-FMGC-INTRODUCE FMGC CAM0102 FOR A319 AUTOLAND AND GPS/ACARS FOR CFM ENGINES ALL

. 034B 26999 ...... ...........

NAVIGATION - MMR - INSTALL COLLINS MMR PROVIDING ILS AND GPS FUNCTION OO-SSF CCM

01 DEC 2002

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. 034A 27014 ...... ...........

HYDRAULIC POWER-AUXILIARY HYDRAULIC POWER-INTRODUCE MODIFIED SUNDSTRAND RAM AIR TURBINE ALL

. 034A 27255 ...... ...........

OXYGEN - PASSENGER OXYGEN SYSTEM INTRODUCE OXYGEN CONTAINER DRAGER P/N -0003 ALL

. 034A 27256 ...... ...........

AUTO FLIGHT - MULTIPURPOSE CONTROL AND DISPLAY UNIT (MCDU) - INTRODUCE MCDU HONEYWELL 2ND GENERATION (P/N -980) ALL

. 034A 27276 ...... ...........

FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ELAC SOFTWARE >L80> ALL

. 034A 27285 ...... ...........

NAVIGATION-ATC MODE>S>-INTRODUCE ATC/TCAS CONTROL UNIT P/N C12404AB02 ALL

. 034A 27320 ...... ...........

INFORMATION SYSTEM-AIR TRAFFIC AND INFO MANAGEMENT SYS(ATIMS)-COCKPIT-INTRODUCE SYS PROVISIONS FOR FANS >A>(ATSU-2DCDU) ALL

. 034A 27330 ...... 31-1133 05

INDICATING/RECORDING SYSTEMS ELECTRICAL CLOCK- INSTALL AIR PRECISION P/N APE5100-1 CAPABLE OF GPS TIME ALL

. 034A 27498 ...... ...........

ELECTRICAL POWER - GENERAL - AC-DC MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS ALL

. 034B 27522 ...... ...........

INFORMATION SYSTEM - AIR TRAFFIC AND INFORMATION SYSTEM (ATIMS) - INSTALL ATSU COMPUTER FOR ACARS OO-SSF

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. 034A 27541 ...... ...........

AUTO FLIGHT - MCDU - INSTALL AN MCDU 2ND GENERATION HONEYWELL FMS (MCDU WITH A340 KEYBOARD) ALL

. 034A 27572 ...... ...........

OXYGEN-PASSENGER OXYGEN-INTRODUCE MODIFIED CHEMICAL OXYGEN CONTAINER -15 MIN- PURITAN ALL

. 034A 27646 ...... ...........

NAVIGATION - MMR - INSTALL SEXTANT MMR PROVIDING ILS (FM IMMUNE) ALL

. 034A 27698 ...... 34-1177 10

NAVIGATION - TCAS - INSTALL ALLIED SIGNAL TCAS COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0) ALL

. 034A 27699 ...... ...........

COMMUNICATIONS - AUDIO MANAGEMENT SYSTEM - INSTALL SATCOM AMU AND ACP ALL

. 034A 27993 ...... ...........

AIR CONDITIONING - PACK COOLING AIR CONTROL - INTRODUCE LOGIC RELAY FOR CONTROL PACK CLOSURE AT ENGINE START ALL

. 034A 28218 ...... ...........

NAVIGATION-ADIRS-INTRODUCE LITTON ADIRU 4 MCU STD-312 ALL

. 034A 28244 ...... 34-1193 17

NAVIGATION-GPWS-INTRODUCE EGPWS P/N 206-206 AND INHIBIT AUTOMATIC DEACTIVATION ENHANCED FUNCTIONS ALL

. 034B 28293 ...... ...........

NAVIGATION - WEATHER RADAR SYSTEM REINSTALL A SINGLE WEATHER RADAR CONFIGURATION OO-SSF

. 034B 28308 ...... ...........

INDICATING RECORDING SYSTEM-DMCINTRODUCE DMC V40 STANDARD OO-SSF

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. 034B 28360 ...... ...........

INFORMATION SYSTEMS-ATIMS-REMOVE ATSU INSTALLATION BACK TO ACARS PROVISIONS OO-SSF

. 034B 28369 ...... ...........

INDICATING/RECORDING SYSTEMS - DMC DISPLAY ALTITUDE IN METRIC UNITS ON THE PRIMARY FLIGHT DISPLAY (PFD) OO-SSF

. 034A 28382 ...... ...........

NAVIGATION - MMR - ACTIVATE GPS PRIMARY FUNCTION (HYBRID) IN SEXTANT MMR (WITH HONEYWELL OR LITTON ADIRU) ALL

. 034A 28482 ...... ...........

LANDING GEAR-NOSE LANDING GEAR WHEELS-REMOVE RUBBING STRIPS ALL

. 034B 28495 ...... ...........

NAVIGATION - MMR - REMOVE COLLINS MMR PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION (PREVIOUS SPEC.) OO-SSF

CCM 01 DEC 2002

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318/319/320/321 FCOM VOL.2 REV033



F-GTFM F-GYJM

CCM 01 MAR 2003

2.00.70 PAGE : CRT001

318/319/320/321 FCOM

VOL. 2

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HIGHLIGHTS

REV033


001

001 REV033 - TECHNICAL AMENDMENT 1)Table of content is updated.

2 01 30

003

200 REV033

CODE 0033

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during refueling are moved to FCOM 2.01.30 p 10a. 2 01 30

007

100 REV033

M:20024

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during defueling are moved to FCOM 2.01.30 p 10a. 2 01 30

008

100 REV033

20024

- TECHNICAL AMENDMENT 1)Procedures for APU start/shutdown during refueling are moved to FCOM 2.01.30 p 10a. 2 01 30

010A

001 REV033 - TECHNICAL AMENDMENT 1)The policy on APU operation during refueling/defueling is modified to allow APU start attempt and shutdown during refueling/defueling. However : -no start attempt is authorized following an automatic shutdown or a failed start -a manual APU shutdown is requested in the event of a fuel spill during refueling/defueling.

2 01 30

011

100 REV033

MOD:20024

- TECHNICAL AMENDMENT 1)Page modified to clarify use of MMIs. 2 01 30

011A

001 REV033 - TECHNICAL AMENDMENT 1)Page created to clarify use of MMIs.

2 01 30

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- INCORPORATION OF MOD 20024 - TECHNICAL AMENDMENT 1)Page created to clarify use of MMIs. 2 01 30

013

001 REV033

CODE 0029

- TECHNICAL AMENDMENT 1)Fuel quantities units are added. 2)Table values are updated. 2 01 30

014

001 REV033

CODE 0029

- TECHNICAL AMENDMENT 01 MAR 2003

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- TECHNICAL AMENDMENT 1)Fuel quantities units are added. 2 01 30

021

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- INCORPORATION OF MOD 20024 - TECHNICAL AMENDMENT 1)Fuel quantities units are added. 2 02 14

008

100 REV033

22013=24105

- TECHNICAL AMENDMENT 1)Update of minimum speeds check. 2 02 20

008

100 REV033

22013=24105

- TECHNICAL AMENDMENT 1)To replace the check of V2 only, by the check of all speeds versus minimum speeds (VMC and VMU). To replace the check of all speeds versus minimum speeds (VMC and VMU) by the check of V2 only versus VMU. 2 03 10

001

001 REV026

CODE 0081

- INCORPORATION OF MOD 27773 2 03 20

001

001 REV033 - TECHNICAL AMENDMENT

01 MAR 2003

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REV033

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1)Removal of the recommendations for the use of the autobrake system. Refer to FCOM 3.03 S.O.P. 2 04 10

002

100 REV033

22013=24105

- TECHNICAL AMENDMENT 1)To clarify the conditions of use of the performance corrections in the CAUTION note. 2 05 70

001

135 REV033 -

2 05 70

002

2 05 70

003

004

2 05 70

005

2 05 70

006

CODE 0093/56-5-B5/B6

INCORPORATION OF MOD 25530 INCORPORATION OF MOD 25800 INCORPORATION OF MOD 27727 VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE TECHNICAL AMENDMENT 1)To provide fuel tankering data for A319-111/-112.

135 REV033 -

CODE 0093/56-5-B5/B6


135 REV033 -

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2 05 70


135 REV033 -

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- INCORPORATION OF MOD 25530 - INCORPORATION OF MOD 25800 - INCORPORATION OF MOD 27727 01 MAR 2003

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006

135 REV033

CODE 0093/56-5-B5/B6

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007

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CODE 0093/56-5-B5/B6

CODE 0093/56-5-B5/B6


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CODE 0081

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2 04 10

015

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REV026

M:20268 CFM 56-5-B6

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001

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001 001

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003 004

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005 006

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CODE 0023/CFM 56-5-B5/6 CODE 0023/CFM 56-5-B5/6

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009 010

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REV029 REV029


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011 012

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REV023 REV031

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001 001

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001 001

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005 006

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26249 26017/CFM ALL

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01 MAR 2003

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100

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CODE 0018 CFM 56-5-B5/B6 CODE 0018 CFM 56-5-B5/B6

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001 002

025 025

REV023 REV023

CFM 56-5-B1/B2/B3/B4/B5/B6 CFM 56-5-B1/B2/B3/B4/B5/B6

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CODE 0023/CFM 56-5-B5/6

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001 002

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CODE 0023/CFM 56-5-B5/6 CODE 0023/CFM 56-5-B5/B6/T=L

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003

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REV021

MOD 24105

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REV027 REV027

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021 022

220 220

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CODE:0023/56-5-B5/B6 CODE:0023/56-5-B5/B6

ALL

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023 024

220 220

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CODE 0023/CFM 56-5-B5/B6 CODE 0023/CFM 56-5-B5/B6

ALL

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001 002

235 220

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M:24105+25800/CFM B5/B6/B7 CODE 0023/CFM 56-5-B5/B6

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220 220

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ALL

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220 220

REV027 REV027


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007 008

220 220

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009 010

220 220

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ALL

2 05 40 2 05 40

011 012

220 220

REV027 REV027


ALL

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001 002

235 220

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M:24105+25800/56-5-B5/B6/B7 CODE:0023/56-5-B5/B6

ALL

2 05 50

003

220

REV027

CODE:0023/56-5-B5/B6

ALL

2 05 60 2 05 60

001 002

001 001

REV021 REV023

2 05 60 2 05 60

003 004

150 150

REV021 REV021

MOD:24105 MOD:24105

ALL

N 2 05 70 N 2 05 70

001 002

135 135

REV033 REV033

CODE 0093/56-5-B5/B6 CODE 0093/56-5-B5/B6

ALL

01 MAR 2003

ALL

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318/319/320/321 FCOM

VOL.2


-REV 033

M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----M V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------EFFECTIVITY----------------------------------------------------------------------------------------N 2 05 70 N 2 05 70

003 004

135 135

REV033 REV033

CODE 0093/56-5-B5/B6 CODE 0093/56-5-B5/B6

ALL

N 2 05 70 N 2 05 70

005 006

135 135

REV033 REV033

CODE 0093/56-5-B5/B6 CODE 0093/56-5-B5/B6

ALL

N 2 05 70 N 2 05 70

007 008

135 135

REV033 REV033

CODE 0093/56-5-B5/B6 CODE 0093/56-5-B5/B6

ALL

01 MAR 2003

CCM

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318/319/320/321 FCOM VOLUME : 2 FLIGHT PREPARATION LIST OF MOD/MP/SB AFFECTING THE MANUAL M V REV T

MOD

MP

REVISION : 033

TITLE

SB

VALIDITY

. 032A 20024 ...... ...........


. 032A 20164 ...... ...........

FUEL - REFUEL/DEFUEL SYSTEM INSTALL A FUEL QUANTITY PRE-SELECTOR IN FLIGHT COMPARTMENT ALL

. 032A 20167 ...... ...........

STRUCTURE - REINFORCE STRUCTURE TO ALLOW MTOW 72T-MLW 63T-MZFW 59T DESIGN WEIGHTS ALL

. 032A 20268 ...... ...........


. 032A 21103 ...... ...........

EQUIPMENT/FURNISHINGS - CARGO COMPARTMENT - REARRANGE COMPARTMENT 4 INTO TWO ZONES ALL

. 032A 21329 ...... ...........

DOORS-CARGO COMPT DOORS-MODIFY LOCKING INDICATION ALL

. 032A 21897 ...... ...........

EQUIPMENT/FURNISHINGS-FWD CARGO COMPTINSTALL CLS AND FULL BULK COMPONENTS F-GTFM

. 032A 21898 ...... ...........

EQUIPMENT/FURNISHINGS-AFT CARGO COMPTINSTALL CLS AND FULL BULK COMPONENTS F-GTFM

. 032A 23124 ...... ...........

AIR CONDITIONING - PRESSURIZATION CONTROL - IMPROVE CONTROLLER TO ENABLE USE OF EXTERNAL MODE ALL

. 032A 23320 ...... ...........

DOORS-CARGO COMPARTMENT DOOR HYDRAULIC SYSTEM-INTRODUCE MODIFIED DOOR SELECTOR VALVE ALL

CCM 01 MAR 2003

2.00.85 PAGE

1


MOD

MP

REVISION : 033

TITLE

SB

VALIDITY

. 032A 23779 ...... ...........

MINOR IMPROVEMENTS INTRODUCED FROM A/C 508 (ST2) TO A/C 521 (ST2) ALL

. 032A 24105 ...... ...........


. 032A 24373 ...... ...........

FUEL - TANK LEVEL SENSING - INTRODUCE MODIFIED LOW FUEL PRESSURE WARNING CONTROL ALL

. 032A 24821 ...... ...........

EQUIPMENT/FURNISHINGS : AFT CARGO COMPARTMENT PROVIDE ADDITIONAL CONTAINER CAPABILITY F-GTFM

. 032A 24946 ...... ...........

LANDING GEAR - MLG - MESSIER INTRODUCE BRAKES P/N C202253 ALL

. 032A 25141 ...... ...........

NACELLES/PYLONS-PYLON STRUCTUREADAPT PRIMARY STRUCTURE TO A321-200 VERSION ALL

. 032A 25287 ...... ...........


. 032A 25530 ...... ...........


. 032A 25800 ...... ...........

POWER PLANT-GENERAL-INTRODUCE CFM56-5B/P ALL

. 032A 26017 ...... ...........

INDICATING/RECORDING SYSTEMS-FLIGHT WARNING COMPUTER (FWC)-INTRODUCE FWC ST2 E2 ALL CCM

01 MAR 2003

2.00.85 PAGE

2


MOD

MP

REVISION : 033

TITLE

SB

VALIDITY

. 032A 26018 ...... ...........


. 032A 26249 ...... ...........

AIR CONDITIONING-FLOW CONTROL AND INDICATING INTRODUCE MODIFIED AIR CONDITIONING FLOW CONTROL ALL

. 032A 26645 ...... ...........

AUTO-FLIGHT-FAC INTRODUCE FAC STD BAM 0513 ALL

. 032A 26968 ...... ...........


. 032A 27276 ...... ...........

FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ELAC SOFTWARE GL80G ALL

. 032A 27727 ...... ...........

ENGINE -COMBUSTION SECTIONINTRODUCE CFM56-5B DAC II PIP ENGINES ALL

. 032A 28164 ...... ...........

LANDING GEAR - WHEELS AND BRAKES INSTALL CARBON BRAKES TYPE SEPCARB III PLUS - MESSIER BUGATTI ALL

N 033

FLIGHT CONTROLS - ELAC SYSTEM INTRODUCE ELAC STD L81 ALL

31395 ...... 27-1135 02

CCM 01 MAR 2003

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318/319/320/321 FCOM VOL.3 REV036



F-GTFM OO-SSF

CCM 01 MAR 2003

3.00.70 PAGE : CRT001

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


003

105 REV036

CODE 0358

- TECHNICAL AMENDMENT 1)Page updated to indicate the maximum wind speed for cargo door operation, in order to be consistent with the AMM : Cargo doors must not be opened, if the wind exceeds 40 knots, and must be closed before the wind exceeds 65 knots. 3 01 21

001

001 REV034 - TECHNICAL AMENDMENT 1)Page created to reflect the cabin pressure graphic, when the max operational altitude is 39800 feet.

3 01 22

001

002 REV036

STD=M:24105=US=(24105/US)

- TECHNICAL AMENDMENT 1)The FLIGHT MANAGEMENT FUNCTION item was moved to the next page, for repagination purposes. 3 01 22

002

105 REV036 -

3 01 22

002A

3 01 22

003

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 TECHNICAL AMENDMENT 1)The FLIGHT MANAGEMENT FUNCTION item, which was moved from the previous page, has been reviewed to be in line with the AFM. 2)The FMGS is also certified for navigation within PRNAV airspace. This is now reflected on this page.

100 REV036 -

CODE 0535

CODE 0538

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28382 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 TECHNICAL AMENDMENT 1)The USE OF NAV AND FINAL APP MODES FOR NON PRECISION APPROACH item has been reviewed to be in line with the AFM, and this page has been created for repagination purposes.

108 REV036

M:24105/CFM/IAE

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)No technical change. The sequence 01 MAR 2003

CCM

3.00.75

PAGE

1

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------number was changed to ensure the correct validation for all customers. 3 01 22

004

115 REV036

24105/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE - TECHNICAL AMENDMENT 1)Additional information to precise the required VAPP in autoland. 2)Automatic landing in CAT1 or better conditions is moved to p 4a. 3 01 22

004A

100 REV036

24105=22013

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure the correct validity for all customers. 3 01 32

001

040 REV035

3 01 34

001

100 REV036

STD OR (25951+32239)CFM ENG

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CODE 0427

- TECHNICAL AMENDMENT 1)EGPWS limitations updated to be in accordance with the existing Flight Manual. 3 01 70

001

050 REV033

3 02 00

003

001 REV036

STD OR US/CFM 56-5-B


- TECHNICAL AMENDMENT 1)Page revised to reflect the correct pagination for the fire protection chapter. 3 02 00

007

001 REV036 - TECHNICAL AMENDMENT 1)The Table of Contents has been updated to reflect FCOM revisions and take into account various pagination changes.

3 02 00

009

025 REV030

3 02 10

002

100 REV036

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE M:26017

- INCORPORATION OF MOD 26017 - TECHNICAL AMENDMENT 1)Introduction of the FWC E2 : With this standard, the DENG REV UNLOCKEDD message is only inhibited in flight phase 8. It may appear at takeoff. 01 MAR 2003

CCM

3.00.75

PAGE

2

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


003

001 REV036 - TECHNICAL AMENDMENT 1)PA call information revised for standardization purposes, and to be in accordance with training.

3 02 10

005

200 REV036

CODE 0396

- TECHNICAL AMENDMENT 1)Recommendations for rotation technique have been harmonized with the 3.02.10 P4 : At VR, rotate the aircraft to 12.5 deg. and, after lift off, follow Speed Reference System (SRS) orders. 3 02 21

004

001 REV036 - TECHNICAL AMENDMENT 1)Deletion of DFWD CRG HEATD from the inoperative system list, as forward cargo heating is not installed.

3 02 21

006

110 REV036

MOD:22561

- TECHNICAL AMENDMENT 1)Deletion of DFWD CRG HEATD, from the inoperative system list, as forward cargo heating is not installed. 2)LAV DET is removed from the DLAV+ GALLEY FAN FAULTD INOP SYS list because the ambient lavatory detectors (Mod 22561) are not lost in case of DLAV+GALLEY FAN FAULTD failure. 3 02 22

002

001 REV036 - TECHNICAL AMENDMENT 1)Addition of information to indicate that following a RUD TRV LIM SYS fault at slatsF extension, full rudder travel authority may be recovered, depending on the cause of the failure.

3 02 22

004

240 REV036

CODE 0589

- TECHNICAL AMENDMENT 1)Addition of information to indicate that following a FAC 1 + 2 FAULT at slatsF extension, full rudder travel authority is recovered. 3 02 23

001

001 REV036 - TECHNICAL AMENDMENT 1)Page revised to reflect the fact that, in case of continuous emission, the onside ACP must not be used for emission. A part of the note has been removed since the recommendation appeared not to be appropriate.

01 MAR 2003

CCM

3.00.75

PAGE

3

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


003

008 REV029

CFM ALL


005

108 REV032

CODE 0008/CFM ALL


006

205 REV036

M:21678+26377

- TECHNICAL AMENDMENT 1)Page revised to delete the DANTI ICE CAPT AOAD line, since this alarm is not triggered by an DAC ESS BUS FAULTD. 3 02 24

006

215 REV036

CODE:0554

- TECHNICAL AMENDMENT 1)Page revised to delete the DANTI ICE CAPT AOAD line, since this alarm is not triggered by an DAC ESS BUS FAULTD. 3 02 24

009

205 REV036

CODE:0555

- INCORPORATION OF MOD 27646 - TECHNICAL AMENDMENT 1)If installed, the CDLS (Cockpit Door Locking System) is inoperative, in case of a DC BUS 2 FAULT. The list of inoperative systems has been updated accordingly. 2)The sequence number was changed to ensure the correct page validation for all customers. 3 02 24

013

205 REV036

21678+24105

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers. 3 02 24

014

400 REV036

CODE 0426

- TECHNICAL AMENDMENT 1)SDCU2 has been removed from the list of INOP SYS displayed on the ECAM. 2)The inoperative system list has been updated to reflect the fact that, if installed, the Cockpit Door Locking System (CDLS) is inoperative, in case of a DC BUS 1+2 FAULT. 3 02 24

018

215 REV036

24105+25404 CFM=IAE

- TECHNICAL AMENDMENT 1)The sequence number was changed to correct validation problems on the page.

01 MAR 2003

CCM

3.00.75

PAGE

4

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


019

100 REV036

M:22013=24105=28160

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 28160 - TECHNICAL AMENDMENT 1)Modification of the DELEC ESS BUSES ON BATD note for improved technical understanding. 2)The sequence number has been changed to ensure the correct page validation for all customers. 3 02 24

026

110 REV030

3 02 24

027

100 REV030

3 02 26

005

100 REV036

M:24105=28160=30020

- INCORPORATION OF MOD 30020 M:22013=24105=28160=30020

- INCORPORATION OF MOD 30020 20057=20059=30067

-

INCORPORATION OF MOD 20057 INCORPORATION OF MOD 20059 INCORPORATION OF MOD 30067 TECHNICAL AMENDMENT 1)When both BLOWER and EXTRACT pushbuttons are in the OVRD position, a single pack may not be able to keep the cabin pressure. So, to avoid depressurization, it is asked to switch the BLOWER and the EXTRACT pushbuttons to the AUTO position before setting the single pack operation of the smoke procedure. If smoke still persists after the single - ADDITIONAL INFORMATION pack operation, once both packs are switched back ON, BLOWER and EXTRACT pushbuttons should be set to OVRD again. 3 02 26

007

300 REV036

CODE 0475

- TECHNICAL AMENDMENT 1)Page modified to reflect the exact aircraft definition : Aircraft not powered by IAE engines. 3 02 26

008

300 REV032

24105+25410+26017


010

001 REV036 - TECHNICAL AMENDMENT 1)The procedure has been harmonized with the Long Range family. In order to open the cockpit window (if necessary), the differential pressure should be zero (no residual pressure). Consequently, it is requested, at FL100 or MEA, to switch both packs OFF, set the pressure MODE SEL to MAN, and set the MAN V/S CTL to FULL UP.

01 MAR 2003

CCM

3.00.75

PAGE

5

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------2)Fwd (aft) cargo smoke warning (if - ADDITIONAL INFORMATION previously contained on this page) has been moved to next page for standardization purposes. 3 02 26

011

400 REV036

CODE:0357

- TECHNICAL AMENDMENT 1)The DFWD (AFT) CARGO SMOKED warning has been moved from the previous page for standardization purposes. 2)The DLAV + CRG DET FAULTD warning has been moved to 3.02.26, page 12, for standardization purposes. 3)Introduction of the C/BsF panel location in the FWD (AFT) CARGO SMOKE procedure. 3 02 26

012

210 REV036 -

3 02 27

002

CODE 0530

INCORPORATION OF MOD 20059 INCORPORATION OF MOD 20067 INCORPORATION OF MOD 20069 TECHNICAL AMENDMENT 1)The DLAV + CRG DET FAULTD warning has been moved from page 11 to this page, for standardization purposes.

405 REV032

CODE 0415


008

410 REV036

24105+24511+25410+26017

- TECHNICAL AMENDMENT 1)Correction of the landing coefficient, when two SECs are affected, to be in accordance with the DLDG CONF-APPR SPD-LDG DIST CORRECTIONS FOR FAILURESD table (FCOM 3.02.80). 3 02 28

006

100 REV026

3 02 28

008

001 REV036

CODE 0359/CFM ALL


- TECHNICAL AMENDMENT 1)The Fuel leak section has been updated to : a) Indicate an additional method of detecting a fuel leak. b) Specify that, in case of leak from an engine, the crossfeed valve may be used, as required. 3 02 28

009

110 REV036

20024

- TECHNICAL AMENDMENT 1)The presentation of the procedure has been changed to clarify that, except in the case of leak from an engine, the crossfeed valve must remain closed. 01 MAR 2003

CCM

3.00.75

PAGE

6

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


010

100 REV036

20024

- TECHNICAL AMENDMENT 1)Procedure modified to prevent opening the crossfeed valve, in case of fuel leak. 3 02 29

001

105 REV036

M:22013=24105

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers. 3 02 29

011

310 REV034

3 02 29

016

105 REV036

CODE 0464

- INCORPORATION OF MOD 31395 M:22013=24105

- INCORPORATION OF MOD 22013 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all customers. 3 02 32

003

110 REV036

24645

- TECHNICAL AMENDMENT 1)Reference to DBRAKES SYS 1(2) FAULTD has been corrected to read : DBRAKES BSCU CH 1(2) FAULTD to reflect the actual ECAM wording. 3 02 32

010

110 REV036

M:24105=(22013+24044)

- INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)No technical change, the sequence number was changed to ensure correct page validation for all customers. 3 02 34

005

001 REV036 - TECHNICAL AMENDMENT 1)Addition of information to further enhance the ADR 1 + 2 + 3 FAULT paper procedure : Since the Rudder Travel Limiter is lost, DRUD WITH CARE ABV 160 KTD will be displayed on the ECAM. 2)Minor editorial change for improved technical understanding.

3 02 34

009

300 REV036

CODE 0198

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the correct page validation for all 01 MAR 2003

CCM

3.00.75

PAGE

7

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------customers. 3 02 34

010

100 REV036

CODE:0382

- TECHNICAL AMENDMENT 1)Information moved to improve technical understanding. 3 02 34

012

001 REV036 - TECHNICAL AMENDMENT 1)Page modified to clarify that the LOC mode is available via the FCU LOC pushbutton, in case of a double Radio Altimeter fault.

3 02 34

015

100 REV036

M:26526

- TECHNICAL AMENDMENT 1)The heading has been shaded to indicate that this is not an ECAM procedure (for some batches of printed pages, the shading was inadvertently omitted). 3 02 36

003

001 REV036 - TECHNICAL AMENDMENT 1)Deletion of the note advising that the forward cargo isolation valve should be closed to minimize the rate at which the cabin altitude increase is removed, since forward cargo ventilation is not installed.

3 02 36

005

200 REV036

MOD:22562+24105

- TECHNICAL AMENDMENT 1)FCOM page amended to specify that the crossbleed valve must be opened, when wing anti-ice is used, and if one bleed is inoperative. 3 02 70

001

120 REV030

3 02 70

002

130 REV030

3 02 70

003

035 REV024

M:28307=27725/CFM 56-5-B

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CODE:0046/56-5-B

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CFM 56-5-B


004

150 REV028

CODE 0020


005

020 REV024

CFM ALL


006

010 REV026

CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 01 MAR 2003

CCM

3.00.75

PAGE

8

318/319/320/321 FCOM

VOL. 3

FLIGHT OPERATIONS

HIGHLIGHTS

REV036


006

010 REV026

CFM ALL

3 02 70

007

020 REV032

CFM


008

010 REV032

3 02 70

009

020 REV030

3 02 70

010

110 REV029

CFM


- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE CODE 0145/CFM 56-5-B


011

035 REV032

CFM ALL


016

230 REV034

CODE 0312/CFM ALL


018

020 REV024

3 02 70

019

030 REV024

3 02 70

022

130 REV024

CODE 0361 CFM ALL




023

120 REV033

CODE 0314/CFM ALL


024

120 REV024

M:24035=24160=24189 CFM ALL


025

020 REV026

3 02 70

026

020 REV024

3 02 80

003

001 REV036

CFM ALL



- TECHNICAL AMENDMENT 1)The DDITCHINGD procedure has been revised to recommend that bleed sources be switched OFF, before setting the DITCHING pushbutton ON, in order to be in accordance with the DON GROUND DE-ICINGD procedure. 2)Rewording of the ditching pushbutton 01 MAR 2003

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------description to be in line with the FCOM 1.21.20 p 7. 3 02 80

005

100 REV036

26526

- TECHNICAL AMENDMENT 1)Procedure enhanced to specify that, if the engines are not running, the landing gear is extended by gravity. 3 02 80

016

025 REV027

CFM ALL


018

302 REV036

23208+24077+24105

- TECHNICAL AMENDMENT 1)Addition of the Ddelta VREFD and landing coefficient when there is a DREVERSE UNLOCKEDD warning, and when the landing is performed in CONF 3. 3 02 90

005

001 REV036 - TECHNICAL AMENDMENT 1)Page revised to reflect the fact that the described procedure is applicable to aircraft fitted with the slide, not the slide-raft. 2)Addition of a note to clarify that doors, equipped with slides, should be given priority for use in case of evacuation.

3 03 04

005

001 REV036 - TECHNICAL AMENDMENT 1)Due to several cases of activation of autobrake at taxi, the crew should check that the SPEED BRAKE lever is retracted and disarmed. 2)Addition of information to warn pilots that, before turning ON the APU bleed, they should check with the ground crew and should also check the ECAM BLEED page to ensure that HP ground air unit is not connected.

3 03 04

007

110 REV030

3 03 05

003

105 REV036

M:22013=24105=24701/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 22199=24105

- INCORPORATION OF MOD 22199 - INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)Page created to remove the DWing leading edge ventilation intakeD item, as it is not applicable. 3 03 06

002

100 REV036

CODE 0435

- INCORPORATION OF MOD 21946 - TECHNICAL AMENDMENT 1)No technical change. The sequence 01 MAR 2003

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------number was changed to ensure the correct page validation for all customers. 3 03 06

006

100 REV036

MOD 22031=25440

- INCORPORATION OF MOD 22031 - INCORPORATION OF MOD 25440 - TECHNICAL AMENDMENT 1)A note has been added to highlight the fact that the Flight Number should be exactly entered on the MCDU INIT page, with the same syntax as the one shown in the ICAO flight plan. Indeed, an inexactly entered flight number can cause the communication and identification with the ATC to fail. 3 03 07

002

001 REV036 - TECHNICAL AMENDMENT 1)The check of the red circle on the window handle has been removed, since this feature is not necessarily installed on all A320 family aircraft.

3 03 08

002

020 REV032

CFM ALL


001

020 REV029

CFM ALL


002

025 REV030

CFM ALL


006

105 REV036

24105

- TECHNICAL AMENDMENT 1)The schematic and wording have been clarified to reflect that the 2 meters of reference, are before the runway edge. 3 03 11

001

040 REV024

CODE:0187

- DELETION OF MOD 25530 - VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 3 03 11

001

040 REV036

CODE:0504/CFM

- TECHNICAL AMENDMENT 1)The benefits of bleed selections for takeoff are clarified and standardized to be in accordance with the A330 SOP. 3 03 12

002

120 REV025

3 03 12

003

001 REV036

CODE 0189 CFM ALL


- TECHNICAL AMENDMENT 1)Modification of the pilot rotation 01 MAR 2003

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------technique to achieve a continuous rotation rate. The aim is to avoid pitch PIO (Pilot Induced Oscillations) and obtain a similar aircraft rotation for all the Airbus fly-by-wire aircraft family. Recommendations regarding lateral inputs on ground and during the rotation have also been amended. 3 03 13

001

001 REV036 - TECHNICAL AMENDMENT 1)FCOM page amended to clarify that icing conditions may be expected, when temperatures are at (or below) 10 deg. C, in order to be in accordance with the Flight Manual.

3 03 15

002

001 REV036 - TECHNICAL AMENDMENT 1)Page modified to include an additional recommendation, in case the cockpit oxygen mask has been used. The mask should be stowed, as per the FCOM 1.35.20, in order to avoid potential risk of oxygen depletion.

3 03 16

002

001 REV036 - TECHNICAL AMENDMENT 1)Page modified to reflect that the correct QRH page reference is 2.31, not 2.41.

3 03 17

003

100 REV036

CODE:0189

- TECHNICAL AMENDMENT 1)The recommendation concerning the use of the EGPWS TERR on ND display has been modified : Depending on operational conditions, the EGPWS TERR display or the weather radar display may be selected on both sides. However, if both weather radar and EGPWS TERR displays are needed, it is recommended to select the weather radar display on the PF side and the - ADDITIONAL INFORMATION EGPWS TERR display on the PNF side. 3 03 18

001

200 REV027

3 03 18

002

210 REV036

M:26018+26398

- INCORPORATION OF MOD 26398 CODE:0578

- TECHNICAL AMENDMENT 1)The legends of the NAV accuracy table have been clarified for improved technical understanding. 3 03 18

003

100 REV036

CODE:0511

- TECHNICAL AMENDMENT 01 MAR 2003

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1)Page revised to introduce ALAR program recommendations. 3 03 18

006

001 REV036 - TECHNICAL AMENDMENT 1)Information has been moved to the FCOM 3.03.18, page 7, for pagination purposes.

3 03 18

007

001 REV036 - TECHNICAL AMENDMENT 1)Information has been moved from the previous page, and some information has been moved to the next page, for pagination purposes. 2)Page modified to add the recommendations given in OIT/FOT 999.0108/02/BB. After landing gear extension, additional guidelines are given to prevent undue flight crew action, in case of brakesF residual - ADDITIONAL INFORMATION pressure. Particularly, the antiskid and nosewheel steering must be kept ON.

3 03 18

008

001 REV036 - TECHNICAL AMENDMENT 1)Information has been moved from the previous page, for pagination purposes.

3 03 18

009

001 REV036 - TECHNICAL AMENDMENT 1)Information has been moved from the previous page, for pagination purposes.

3 03 19

001

105 REV036

CODE 0535

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 30631 - TECHNICAL AMENDMENT 1)DNON RNAVD approaches has been included in the title. RNAV approaches are described further in this chapter. 2)Additional references to Airbus operational documentation, regarding NAV database validation, is included. 3)Now, it is requested to check the lateral and vertical F-PLN against the IAP approach, before starting the approach. - ADDITIONAL INFORMATION 4)New indications are given on how to deal with a GPS PRIMARY loss, or a FM/GPS POS DISAGREE caution. 3 03 19

002

001 REV036 - TECHNICAL AMENDMENT 1)Addition of information on approach

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------guidance for RNAV approaches. 3 03 19

003

120 REV036

CODE 0543

- INCORPORATION OF MOD 24105 - INCORPORATION OF MOD 25294 - TECHNICAL AMENDMENT 1)Addition of information on approach guidance for RNAV approaches. 3 03 19

004

105 REV036

CODE 0546

- INCORPORATION OF MOD 26398 - TECHNICAL AMENDMENT 1)Page created to include information that was moved from a previous page, for repagination purposes. 2)Introduction of the ALAR program recommendations. 3 03 19

005

001 REV036 - TECHNICAL AMENDMENT 1)Information was moved from a previous page, for repagination purposes.

3 03 19

006

200 REV036

CODE 0549

-

INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28244 INCORPORATION OF MOD 28382 INCORPORATION OF MOD 28495 TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)The legends of the NAV accuracy table have been clarified for improved technical understanding. 3)A note is added to advise that, if during an overlay approach to a conventional radio procedure, the raw data indicates that the managed guidance is unsatisfactory, the crew - ADDITIONAL INFORMATION must revert to selected guidance. 3 03 19

007

100 REV036 -

3 03 19

007

01 MAR 2003

INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION

100 REV032 -

CODE 0538 OF OF OF OF OF OF OF OF

MOD MOD MOD MOD MOD MOD MOD MOD

25205 26111 26485 26999 28382 28495 30241 30631

CODE 0042

DELETION DELETION DELETION DELETION

OF OF OF OF

MOD MOD MOD MOD

24064 24065 24066 24067

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007

100 REV036

CODE 0538

- TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)Specific procedure lines for RNAV approaches have been added to ensure the required navigation accuracy for the approach. It is also reminded that the RNAV approaches without GPS are subject to specific operational approval. 3 03 19

008

001 REV036 - TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)Page modified to add the recommendations given in OIT/FOT 999.0108/02/BB. After landing gear extension, additional guidelines are given to prevent undue flight crew action in case of brakes residual pressure. Particularly, the antiskid and nose wheel steering must be kept - ADDITIONAL INFORMATION ON.

3 03 19

009

001 REV036

STD=M:24105

- INCORPORATION OF MOD 24105 - TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes. 2)New indications for the POSITION and FLIGHT PATH monitoring and adjusting, regarding the RNAV approaches and approaches overlay to a conventional radio navaid procedure. 3 03 19

010

001 REV036 - TECHNICAL AMENDMENT 1)Information was moved from a previous page for repagination purposes.

3 03 19

011

100 REV036 -

3 03 19

012

M:24064=24065=24066=24067

INCORPORATION OF MOD 24064 INCORPORATION OF MOD 24065 INCORPORATION OF MOD 24066 INCORPORATION OF MOD 24067 TECHNICAL AMENDMENT 1)Information was moved from page 7 for repagination purposes.

100 REV036

M:23742

- INCORPORATION OF MOD 23742 - TECHNICAL AMENDMENT 1)Information was moved from page 8 for repagination purposes.

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013

001 REV036 - TECHNICAL AMENDMENT 1)Information was moved from page 9 for repagination purposes.

3 03 20

001

100 REV035

3 03 22

004

105 REV036

26398

- INCORPORATION OF MOD 26398 M:24105

- TECHNICAL AMENDMENT 1)Page modified to include attitude monitoring during flare. Attitude monitoring is done by the PNF and its aim is to avoid tailstrike, or wingtip or engine scrape during the flare maneuver. 3 03 23

001

110 REV036

25863

- TECHNICAL AMENDMENT 1)Information has been moved to the next page for pagination and standardization purposes. 3 03 23

002

001 REV036 - TECHNICAL AMENDMENT 1)- Information has been moved from page 1. - Addition of a conditional procedure, to manually disengage GO-Around SRS Mode by pulling the FCU ALT knob, should the target speed not automatically increase when climbing through GO Acceleration Altitude.

3 03 23

004

100 REV036

M:25863

- INCORPORATION OF MOD 25863 - TECHNICAL AMENDMENT 1)Blank page moved from previous page to this page for pagination and standardization purposes. 3 03 25

001

020 REV035

3 03 25

003

170 REV035

3 04 00

001

203 REV036

CODE 0186/CFM ALL

- VERSION AND/OR ENGINE INCORPORATION, DELETION OR CHANGE 22013=23119/CFM ALL


- TECHNICAL AMENDMENT 1)The title of the SUPPLEMENTARY TECHNIQUESF FLIGHT CONTROLS chapter has been modified to indicate that it also contains flying techniques. 2)AIRCRAFT TRIMMING is moved to page 12.

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002

115 REV028

M:24105/CFM ALL=IAE ALL


001

001 REV036 - TECHNICAL AMENDMENT 1)Simplification of the note concerning noisy frequencies.

3 04 23

001A

001 REV036 - TECHNICAL AMENDMENT 1)Page created to harmonize pagination changes.

3 04 24

004

103 REV036

24771

- INCORPORATION OF MOD 24771 - TECHNICAL AMENDMENT 1)Addition of a CIDS reset procedure in case of uncommanded EVAC horn actuation. 2)Some information has been moved to the next page, to accommodate additional information on page 4, and ensure the correct page validation for all customers. 3 04 24

005

101 REV036

24613=22013+24613

- INCORPORATION OF MOD 24613 - TECHNICAL AMENDMENT 1)Some information has been moved from page 4 to this page, and some information has been moved to page 6, to accommodate additional information page 4 and ensure the correct page validation for all customers. 3 04 24

006

001 REV036 - TECHNICAL AMENDMENT 1)Page created to accommodate additional information on page 4 and ensure the correct page validation for all customers.

3 04 27

002

001 REV036 - TECHNICAL AMENDMENT 1)Sidestick position indication on PFD may be monitored by the crew, not only when in crosswind condition. References to crosswind conditions have consequently been removed from our recommendations regarding the use of the sidestick position indication. 2)A crossreference to the SOP 3.03.12 has been added, since this chapter contains some additional information - ADDITIONAL INFORMATION on takeoff technique.

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003

001 REV036 - TECHNICAL AMENDMENT 1)Recommendations regarding lateral inputs on ground and during the rotation have been amended : Lateral inputs on ground and during the rotation should be minimized to avoid spoiler extension. Spoiler deflection starts to become significant with more than one third sidestick deflection.

3 04 27

004

001 REV036 - TECHNICAL AMENDMENT 1)Recommendations for crosswind landing technique, have been harmonized with the SOP 3.03.22.

3 04 27

005

001 REV036 - TECHNICAL AMENDMENT 1)Introduction of recommendations, in case of bounce at landing. 2)Some text has been moved to page 6.

3 04 27

006

001 REV036 - TECHNICAL AMENDMENT 1)The DBACKUP CONTROLD chapter has been renamed DMECHANICAL BACKUPD for improved understanding of the meaning of this term. 2)Some text has been moved from page 5, and the illustration to page 7, to accomodate additional info on page 5.

3 04 27

007

001 REV036 - TECHNICAL AMENDMENT 1)Some text has been moved from page 6, and some to page 8, to accomodate additional info on page 5.

3 04 27

008


3 04 27

009


3 04 27

010


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011


3 04 27

012

001 REV036 - TECHNICAL AMENDMENT 1)New page created : Some text has been moved from page 11, to accomodate info on page 5.

3 04 70

003

020 REV026

CFM ALL


005

100 REV029

CODE 0145/CFM ALL


006

020 REV033

3 04 70

007

020 REV028

3 04 70

008

007 REV030

CFM ALL




001

020 REV024

CFM ALL


002

020 REV035

CFM ALL


004

001 REV036 - TECHNICAL AMENDMENT 1)No technical change. Information has been moved to the next page for pagination purposes.

3 04 91

005

001 REV036 - TECHNICAL AMENDMENT 1)No technical change. Information has been moved from the previous page for pagination purposes.

3 04 91

007

001 REV036 - TECHNICAL AMENDMENT 1)Introduction of the Doutflow valve check ditchingD Temporary Revision : A recommendation has been added to check that no external air is supplied to the aircraft via the low or high pressure ground connectors, before

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REV036

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------starting the de-icing procedure. 2)Minor editorial changes have been made to reflect the fact that the aircraft can be de-iced with the APU and the - ADDITIONAL INFORMATION engines running. 3)The note concerning the DITCHING pushbutton has been updated to reflect the fact that the avionic ventilation inlet valve is also closed. 3 04 91

008

001 REV036 - TECHNICAL AMENDMENT 1)Introduction of TR 734-1 : A recommendation has been added within the de-icing procedure, to check that the outflow valve is indicated open, after completion of this procedure. 2)The sequence number was changed to ensure the correct page validation for all customers.

3 04 92

001

001 REV036 - TECHNICAL AMENDMENT Page revised : 1)To indicate that pilots must check the version of F.O.V.E. installed on their PCs, not the version of each module, as previously stated. 2)For improved technical understanding and standardization.

3 04 92

002

001 REV036 - TECHNICAL AMENDMENT Page revised to indicate that : 1)Pilots must check the version of F.O.V.E. installed on their PCs, not the version of each module, as previously stated. 2)The DAircraft LoadingD module has been replaced by the DWeight and BalanceD module.

3 04 92

004

001 REV036 - TECHNICAL AMENDMENT Page revised to : 1)Replace the DAircraft LoadingD module by the DWeight and BalanceD module. 2)Introduce the description of the LPCFs Weight and Balance (W & B) module. 3)Delete the reference to the ECAM CG, as there is no ECAM CG on the A320 aircraft family.

3 04 92

005

001 REV036 - TECHNICAL AMENDMENT 1)Page created to introduce the description of the LPCFs Weight and Balance (W & B) module.

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001 REV036 - TECHNICAL AMENDMENT 1)Page created to introduce the description of the LPCFs Weight and Balance (W & B) module.

3 05 35

001

100 REV036

M:22013=24105

- TECHNICAL AMENDMENT 1)In note 2, replace VLS by VREF for CONF FULL. VLS is for CONF 3.

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24105+26017 21678+24105+26017

ALL

N 3 02 24 N 3 02 24

013 014

205 400

REV036 REV036

21678+24105 CODE 0426

ALL

3 02 24 3 02 24

015 016

200 220

REV026 REV035

CODE 0393 CODE 0393

ALL

N 3 02 24 N 3 02 24

017 018

250 215

REV033 REV036

CODE:0350 24105+25404 CFM=IAE

ALL

N 3 02 24 N 3 02 24

019 020

100 210

REV036 REV033

M:22013=24105=28160 MOD 21678+21706

ALL

3 02 24 3 02 24

021 022

100 230

REV035 REV027

21678 CODE 0476

ALL

3 02 24 3 02 24

023 024

310 200

REV031 REV032

M:21285+21678+25404/CFM CODE 0239

ALL

3 02 24 3 02 24

025 026

303 110

REV029 REV030

CODE 0552 M:24105=28160=30020

ALL

3 02 24 3 02 24

027 028

100 001

REV030 REV032

M:22013=24105=28160=30020

ALL

3 02 26 3 02 26

001 002

001 001

REV032 REV033

3 02 26 3 02 26

003 004

001 100

REV033 REV035

27498=31891

N 3 02 26 N 3 02 26

005 006

100 001

REV036 REV035

20057=20059=30067

ALL

R 3 02 26 R 3 02 26

007 008

300 300

REV036 REV032

CODE 0475 24105+25410+26017

ALL

N 3 02 26 N 3 02 26

009 010

001 001

REV032 REV036

01 MAR 2003

ALL ALL

ALL

CCM

3.00.80 PAGE

04

318/319/320/321 FCOM

VOL.3


-REV 036


011 012

400 210

REV036 REV036

CODE:0357 CODE 0530

ALL

3 02 27 3 02 27

001 002

200 405

REV024 REV032

24612+26017 CODE 0415

ALL

3 02 27 3 02 27

003 004

110 400

REV028 REV032

CODE 0183 20024+24105+25410+26017

ALL

3 02 27 3 02 27

005 006

100 001

REV024 REV033

MOD:24612

ALL

R 3 02 27 R 3 02 27

007 008

220 410

REV027 REV036

CODE 0392 24105+24511+25410+26017

ALL

3 02 27 3 02 27

009 010

100 215

REV026 REV032

MOD:26017 CODE 0229

ALL

3 02 27 3 02 27

011 012

110 100

REV031 REV025

25410 MOD:26017

ALL

3 02 27 3 02 27

013 014

300 200

REV028 REV024

24105+25410+26017 MOD 24105+26017

ALL

3 02 27 3 02 27

015 016

310 240

REV024 REV033

24105+25410+26017 M:21964+22087

ALL

3 02 27 3 02 27

017 018

110 001

REV025 REV024

26017=(25410+26017)

ALL

3 02 27 3 02 27

019 020

001 200

REV024 REV028

CODE 0045

3 02 27 3 02 27

021 022

001 001

REV024 REV024

3 02 28 3 02 28

001 002

100 002

REV033 REV033

M:20024

ALL

3 02 28 3 02 28

003 004

100 001

REV028 REV024

MOD 20024

ALL

3 02 28 3 02 28

005 006

001 100

REV026 REV026

CODE 0359/CFM ALL

R 3 02 28 R 3 02 28

007 008

100 001

REV024 REV036

MOD 20024

ALL

R 3 02 28 R 3 02 28

009 010

110 100

REV036 REV036

20024 20024

ALL

N 3 02 29 N 3 02 29

001 002

105 001

REV036 REV024

M:22013=24105

ALL

3 02 29 3 02 29

003 004

110 001

REV032 REV024

MOD:26017

ALL

3 02 29 3 02 29

005 006

110 001

REV033 REV025

26017

ALL

01 MAR 2003

ALL ALL

ALL

CCM

3.00.80 PAGE

05

318/319/320/321 FCOM

VOL.3


-REV 036


007 008

002 230

REV024 REV024

3 02 29 3 02 29

009 010

001 001

REV024 REV024

3 02 29 3 02 29

011 012

310 001

REV034 REV024

CODE 0464

ALL

3 02 29 3 02 29

013 014

200 100

REV034 REV034

24105+26017 26017

ALL

N 3 02 29 N 3 02 29

015 016

100 105

REV033 REV036

26017 M:22013=24105

ALL

3 02 30 3 02 30

001 002

100 001

REV030 REV024

25410=26017

ALL

3 02 30 3 02 30

003 004

001 001

REV027 REV024

3 02 30 3 02 30

005 006

100 001

REV025 REV027

MOD:22875

3 02 30 3 02 30

007 008

001 205

REV024 REV028

M:24105+26017

3 02 31 3 02 31

001 002

001 001

REV024 REV032

ALL

3 02 31 3 02 31

003 004

001 001

REV024 REV033

ALL

3 02 32 3 02 32

001 002

001 001

REV030 REV034

STD=31897=31896

ALL

R 3 02 32 R 3 02 32

003 004

110 002

REV036 REV033

24645 STD=(20139+22129)

ALL

3 02 32 3 02 32

005 006

001 001

REV024 REV032

ALL

3 02 32 3 02 32

007 008

001 001

REV031 REV035

ALL

N 3 02 32 N 3 02 32

009 010

105 110

REV035 REV036

24105 M:24105=(22013+24044)

ALL

3 02 32

011

001

REV033

STD=27979

ALL

3 02 34 3 02 34

001 002

001 223

REV024 REV030

CODE:0294 CODE 0095

ALL

3 02 34 3 02 34

003 004

100 205

REV033 REV033

26526 M:26017+26526

ALL

R 3 02 34 R 3 02 34

005 006

001 105

REV036 REV033

26017=(25410+26017)

01 MAR 2003

ALL CODE 0355 ALL

ALL ALL ALL

ALL

CCM

3.00.80 PAGE

06

318/319/320/321 FCOM

VOL.3


-REV 036


007 008

200 105

REV035 REV031

CODE 0172 CODE 0383

ALL

N 3 02 34 N 3 02 34

009 010

300 100

REV036 REV036

CODE 0198 CODE:0382

ALL

R 3 02 34 R 3 02 34

011 012

100 001

REV033 REV036

MOD:26017

ALL

3 02 34 3 02 34

013 014

105 105

REV035 REV035

CODE 0614 22769

ALL

R 3 02 34 R 3 02 34

015 016

100 100

REV036 REV025

M:26526 M:26526

ALL

3 02 34 3 02 34

017 018

105 100

REV033 REV035

CODE:0205 26017

ALL

3 02 34 3 02 34

019 020

001 001

REV035 REV035

ALL

3 02 34 3 02 34

021 022

001 001

REV035 REV035

ALL

3 02 34 3 02 34

023 024

035 035

REV035 REV035

56-5-B5/B6/B7 56-5-B5/B6/B7

ALL

3 02 34

025

035

REV035

56-5-B5/B6/B7

ALL

3 02 36 3 02 36

001 002

001 001

REV024 REV034

R 3 02 36 R 3 02 36

003 004

001 200

REV036 REV028

M:22562+24105

R 3 02 36 R 3 02 36

005 006

200 001

REV036 REV024

MOD:22562+24105

ALL

3 02 36

007

100

REV025

M:24105

ALL

3 02 49

001

001

REV024

3 02 52

001

001

REV024

CODE 0188

ALL

3 02 70 3 02 70

001 002

120 130

REV030 REV030

M:28307=27725/CFM 56-5-B CODE:0046/56-5-B

ALL

3 02 70 3 02 70

003 004

035 150

REV024 REV028

CFM 56-5-B CODE 0020

ALL

3 02 70 3 02 70

005 006

020 010

REV024 REV026

CFM ALL CFM ALL

ALL

3 02 70 3 02 70

007 008

020 010

REV032 REV032

CFM CFM

ALL

3 02 70 3 02 70

009 010

020 110

REV030 REV029

CFM ALL CODE 0145/CFM 56-5-B

ALL

01 MAR 2003

ALL ALL

ALL

CCM

3.00.80 PAGE

07

318/319/320/321 FCOM

VOL.3


-REV 036


011 012

035 200

REV032 REV030

CFM ALL M:25404+26017

ALL

3 02 70 3 02 70

013 014

100 105

REV033 REV035

MOD:25410 MOD 24105

ALL

3 02 70 3 02 70

015 016

040 230

REV035 REV034

CFM ENG:ALL CODE 0312/CFM ALL

ALL

3 02 70 3 02 70

017 018

220 020

REV026 REV024

CODE 0050 CODE 0361 CFM ALL

ALL

3 02 70 3 02 70

019 020

030 150

REV024 REV028

CFM ALL M:26017 CFM 56-5-B4/B5/B6/B7

ALL

3 02 70 3 02 70

021 022

020 130

REV034 REV024

CFM 56-5-A4/A5/B5/B6/B7 CODE 0106

ALL

3 02 70 3 02 70

023 024

120 120

REV033 REV024

CODE 0314/CFM ALL M:24035=24160=24189 CFM ALL

ALL

3 02 70 3 02 70

025 026

020 020

REV026 REV024

CFM ALL CFM ALL

ALL

3 02 80 3 02 80

001 002

001 100

REV035 REV031

M:26526

R 3 02 80 R 3 02 80

003 004

001 001

REV036 REV024

R 3 02 80 R 3 02 80

005 006

100 001

REV036 REV035

26526

3 02 80 3 02 80

007 008

001 065

REV034 REV029

CODE:0109/T=L

3 02 80 3 02 80

009 010

001 001

REV025 REV034

ALL

3 02 80

010A

001

REV031

ALL

3 02 80

011

001

REV035

ALL

3 02 80

011A

001

REV034

ALL

3 02 80

012

001

REV034

ALL

3 02 80 3 02 80

013 014

001 001

REV030 REV033

ALL

3 02 80 3 02 80

015 016

100 025

REV032 REV027

MOD:22562 CFM ALL

ALL

N 3 02 80 N 3 02 80

017 018

110 302

REV035 REV036

24105 23208+24077+24105

ALL

3 02 80 3 02 80

019 020

100 100

REV035 REV035

22249 25529=25819=26117=26270

ALL

01 MAR 2003

ALL ALL ALL ALL

CCM

3.00.80 PAGE

08

318/319/320/321 FCOM

VOL.3


-REV 036


001 002

001 105

REV028 REV030

3 02 90 3 02 90

003 004

001 001

REV033 REV028

ALL

R 3 02 90

005

001

REV036

ALL

3 03 00

001-2

001

REV027

ALL

3 03 01 3 03 01

001 002

001 001

REV035 REV035

ALL

3 03 01 3 03 01

003 004

001 001

REV034 REV034

ALL

3 03 01

005

001

REV024

ALL

3 03 02 3 03 02

001 002

001 001

REV034 REV025

ALL

3 03 03

001

001

REV024

ALL

3 03 04 3 03 04

001 002

001 001

REV024 REV025

ALL

3 03 04 3 03 04

003 004

100 001

REV028 REV033

22373=(22373+25072+28897)

R 3 03 04 R 3 03 04

005 006

001 100

REV036 REV025

MOD 22013 OR 24105 OR 24701

3 03 04 3 03 04

007 008

110 001

REV030 REV024

M:22013=24105=24701/CFM ALL CODE 0462

3 03 05 3 03 05

001 002

001 001

REV024 REV024

N 3 03 05 N 3 03 05

003 004

105 001

REV036 REV024

3 03 05 3 03 05

005 006

001 001

REV033 REV032

N 3 03 06 N 3 03 06

001 002

001 100

REV024 REV036

CODE 0435

3 03 06 3 03 06

003 004

100 105

REV033 REV032

24852=25336=27917=28218 M:24373

N 3 03 06 N 3 03 06

005 006

001 100

REV031 REV036

MOD 22031=25440

3 03 06 3 03 06

007 008

001 001

REV025 REV033

STD=31896=31897

3 03 06 3 03 06

009 010

001 001

REV024 REV024

STD=31896=31897

01 MAR 2003

ALL 24105=30203

ALL ALL ALL ALL

22199=24105


CCM

ALL

3.00.80 PAGE

09

318/319/320/321 FCOM

VOL.3


-REV 036


011 012

001 100

REV035 REV034

21946

3 03 06 3 03 06

013 014

001 001

REV030 REV030

STD OR 24588 OR(24215+24588)

3 03 06 3 03 06

015 016

001 001

REV028 REV029

ALL

R 3 03 07 R 3 03 07

001 002

001 001

REV033 REV036

ALL

3 03 07

003

001

REV033

3 03 08 3 03 08

001 002

020 020

REV034 REV032

CFM56-5-A1/A3/A4/A5/B5/B6/B7 CFM ALL

ALL

3 03 08

003

040

REV030

CFM56-5-B1/B2/B3/B4/B5/B6/B7

ALL

3 03 09 3 03 09

001 002

020 025

REV029 REV030

CFM ALL CFM ALL

ALL

3 03 10 3 03 10

001 002

001 001

REV034 REV034

3 03 10 3 03 10

003 004

200 001

REV024 REV033

MOD:21964+22087 STD=31896=31897

ALL

R 3 03 10 R 3 03 10

005 006

001 105

REV026 REV036

STD=31896=31897 24105

ALL

R 3 03 11 R 3 03 11

001 002

040 100

REV036 REV035

CODE:0504/CFM 20081

ALL

3 03 12 3 03 12

001 002

001 120

REV030 REV025

CODE 0189 CFM ALL

R 3 03 12 R 3 03 12

003 004

001 100

REV036 REV032

CODE 0189

3 03 12 3 03 12

005 006

001 001

REV033 REV035

CODE 0092

R 3 03 13

001

001

REV036

3 03 14 3 03 14

001 002

100 100

REV027 REV027

CODE 0189 MOD:24035 OR 24160 OR 24211

ALL

R 3 03 15 R 3 03 15

001 002

001 001

REV035 REV036

CODE 0603

ALL

R 3 03 16 R 3 03 16

001 002

001 001

REV024 REV036

STD OR M:28238+28719

ALL

3 03 16

003

001

REV035

CODE 0230

ALL

3 03 17 3 03 17

001 002

100 001

REV025 REV024

CODE 0036 STD=CODE 0211

ALL

01 MAR 2003

ALL ALL

ALL

ALL

ALL ALL ALL ALL

CCM

3.00.80 PAGE

10

318/319/320/321 FCOM

VOL.3


-REV 036


003 004

100 100

REV036 REV034

CODE:0189 24404=24405=25416=25530

ALL

N 3 03 18 N 3 03 18

001 002

200 210

REV027 REV036

M:26018+26398 CODE:0578

ALL

R 3 03 18 R 3 03 18

003 004

100 100

REV036 REV030

CODE:0511 CODE 0001

ALL

R 3 03 18 R 3 03 18

005 006

001 001

REV030 REV036

ALL

R 3 03 18 R 3 03 18

007 008

001 001

REV036 REV036

ALL

N 3 03 18

009

001

REV036

ALL

R 3 03 19 R 3 03 19

001 002

105 001

REV036 REV036

CODE 0535

ALL

N 3 03 19 N 3 03 19

003 004

120 105

REV036 REV036

CODE 0543 CODE 0546

ALL

N 3 03 19 N 3 03 19

005 006

001 200

REV036 REV036

CODE 0549

N 3 03 19 N 3 03 19

007 008

100 001

REV036 REV036

CODE 0538

ALL

N 3 03 19 N 3 03 19

009 010

001 001

REV036 REV036

STD=M:24105

ALL

N 3 03 19 N 3 03 19

011 012

100 100

REV036 REV036

M:24064=24065=24066=24067 M:23742

ALL

N 3 03 19

013

001

REV036

N 3 03 20 N 3 03 20

001 002

100 001

REV035 REV024

3 03 21

001

001

REV024

3 03 22 3 03 22

001 002

035 035

REV032 REV032

56-5-B5/B6/B7 56-5-B5/B6/B7

ALL

R 3 03 22 R 3 03 22

003 004

105 105

REV035 REV036

24105 M:24105

ALL

3 03 22 3 03 22

005 006

001 001

REV033 REV027

N 3 03 23 N 3 03 23

001 002

110 001

REV036 REV036

25863

ALL

N 3 03 23 N 3 03 23

003 004

100 100

REV036 REV036

MOD:25863=(ACA/25863) M:25863

ALL

3 03 24 3 03 24

001 002

100 001

REV035 REV034

20081 STD=(25951+32239)

ALL

01 MAR 2003

ALL

ALL 26398

ALL ALL

ALL

CCM

3.00.80 PAGE

11

318/319/320/321 FCOM

VOL.3


-REV 036


001 002

020 001

REV035 REV035

CODE 0186/CFM ALL

ALL

3 03 25

003

170

REV035

22013=23119/CFM ALL

ALL

3 03 26

001

100

REV030

CODE 0213

ALL

3 03 90 3 03 90

001 002

001 001

REV035 REV034

ALL

3 03 90 3 03 90

003 004

001 001

REV027 REV027

ALL

3 03 90 3 03 90

005 006

001 001

REV027 REV030

ALL

3 03 90

007

001

REV033

ALL

R 3 04 00 R 3 04 00

001 002

203 001

REV036 REV032

3 04 00

003

001

REV033

3 04 10 3 04 10

001 002

001 115

REV024 REV028

M:24105/CFM ALL=IAE ALL

3 04 10 3 04 10

003 004

001 100

REV024 REV024

MOD:22013 OR 24105

3 04 21 3 04 21

001 002

001 001

REV032 REV024

ALL

N 3 04 23

001

001

REV036

ALL

N 3 04 23

001A

001

REV036

ALL

N 3 04 23

002

100

REV024

20137=(20137+28360+30239)

ALL

3 04 23

003

100

REV024

CODE 0317

ALL

3 04 24 3 04 24

001 002

001 001

REV035 REV033

N 3 04 24 N 3 04 24

003 004

001 103

REV033 REV036

24771

N 3 04 24 N 3 04 24

005 006

101 001

REV036 REV036

24613=22013+24613

R 3 04 27 R 3 04 27

001 002

001 001

REV028 REV036

ALL

R 3 04 27 R 3 04 27

003 004

001 001

REV036 REV036

ALL

R 3 04 27 R 3 04 27

005 006

001 001

REV036 REV036

ALL

01 MAR 2003

CODE 0501

ALL ALL ALL ALL

ALL ALL

CCM

ALL

3.00.80 PAGE

12

318/319/320/321 FCOM

VOL.3


-REV 036


007 008

001 001

REV036 REV036

ALL

R 3 04 27 R 3 04 27

009 010

001 001

REV036 REV036

ALL

N 3 04 27 N 3 04 27

011 012

001 001

REV036 REV036

ALL

3 04 28

001

100

REV024

MOD:20024

ALL

3 04 30 3 04 30

001 002

100 001

REV034 REV024

22013=24105

ALL

3 04 31 3 04 31

001 002

001 001

REV024 REV024

3 04 32 3 04 32

001 002

001 001

REV031 REV031

3 04 32

003

001

REV034

3 04 34 3 04 34

001 002

001 100

REV030 REV032

3 04 34 3 04 34

003 004

001 001

REV031 REV035

ALL

3 04 34 3 04 34

005 006

001 001

REV026 REV032

ALL

3 04 34 3 04 34

007 008

001 001

REV031 REV034

CODE 0058

ALL

3 04 34 3 04 34

009 010

100 001

REV034 REV024

23672=24581=24785=25108

ALL

3 04 34 3 04 34

011 012

100 120

REV024 REV024

CODE 0063 CODE 0063

ALL

3 04 34 3 04 34

013 014

105 105

REV029 REV029

CODE 0264 CODE 0264

ALL

3 04 34 3 04 34

015 016

120 001

REV024 REV029

CODE 0063

ALL

3 04 34 3 04 34

017 018

001 001

REV026 REV026

3 04 34 3 04 34

019 020

001 001

REV028 REV028

CODE 0258

ALL

3 04 34

021

100

REV031

M:26526

ALL

3 04 70 3 04 70

001 002

001 110

REV024 REV024

M:22013=24035=24160=24189

3 04 70 3 04 70

003 004

020 100

REV026 REV033

CFM ALL CODE 0145 CFM ALL

01 MAR 2003

ALL ALL STD OR (25951 + 32239) ALL ALL CODE:0317

ALL

ALL

CCM

ALL

3.00.80 PAGE

13

318/319/320/321 FCOM

VOL.3


-REV 036


005 006

100 020

REV029 REV033

CODE 0145/CFM ALL STD=M:30439+31040/CFM

ALL

3 04 70 3 04 70

007 008

020 007

REV028 REV030

CFM ALL CFM ALL

ALL

3 04 70 3 04 70

009 010

001 001

REV030 REV030

ALL

3 04 80 3 04 80

001 002

001 001

REV030 REV032

ALL

3 04 80

003

001

REV032

N 3 04 90 N 3 04 90

001 002

020 020

REV024 REV035

CFM ALL CFM ALL

ALL

3 04 91 3 04 91

001 002

110 265

REV033 REV028

24105=(20268+24105) M:20268+24917 CFM 56-5-B5/B6

ALL

R 3 04 91 R 3 04 91

003 004

100 001

REV025 REV036

M:24917

ALL

R 3 04 91 R 3 04 91

005 006

001 001

REV036 REV026

ALL

N 3 04 91 N 3 04 91

007 008

001 001

REV036 REV036

ALL

3 04 91

008A

001

REV033

ALL

3 04 91 3 04 91

009 010

001 001

REV035 REV028

ALL

3 04 91 3 04 91

011 012

001 001

REV028 REV028

ALL

3 04 91 3 04 91

013 014

100 001

REV028 REV028

3 04 91

015

001

REV028

ALL

R 3 04 92 R 3 04 92

001 002

001 001

REV036 REV036

ALL

R 3 04 92 R 3 04 92

003 004

001 001

REV033 REV036

ALL

N 3 04 92 N 3 04 92

005 006

001 001

REV036 REV036

ALL

3 05 00 3 05 00

001 002

001 001

REV025 REV024

ALL

3 05 05 3 05 05

001 002

001 001

REV024 REV025

ALL

3 05 05 3 05 05

003 004

001 001

REV024 REV024

ALL

01 MAR 2003

ALL

M:21729

CCM

ALL

3.00.80 PAGE

14

318/319/320/321 FCOM

VOL.3


-REV 036


005 006

001 001

REV032 REV024

3 05 06 3 05 06

001 002

020 080

REV024 REV025

CODE:0517 CFM 56-5-B6

ALL

3 05 06 3 05 06

003 004

080 001

REV025 REV024

CFM 56-5-B6

ALL

3 05 06 3 05 06

005 006

078 075

REV027 REV027

CFM 56-5-B6 CFM 56-5-B6

ALL

3 05 06 3 05 06

007 008

075 075

REV025 REV025

CFM 56-5-B5/B6 CFM 56-5-B5/B6

ALL

3 05 06 3 05 06

009 010

075 020

REV025 REV025

CODE:0513/56-5-B5/B6 STD=M:28238/CFM ALL/T=L

ALL

3 05 10 3 05 10

001 002

115 280

REV027 REV031

M:25800/CFM 56-5-B1 TO B7 CODE:0380/56-5-B5/B6

ALL

3 05 10 3 05 10

003 004

280 280

REV031 REV031

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 10 3 05 10

005 006

280 280

REV031 REV031

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 10 3 05 10

007 008

280 280

REV031 REV031

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 10

009

280

REV031

CODE:0380/56-5-B5/B6

ALL

3 05 15 3 05 15

001 002

130 080

REV030 REV030

CODE:0515/56-5-B5/B6 CODE:0513/56-5-B5/B6

ALL

3 05 15 3 05 15

003 004

080 080

REV030 REV030

CODE:0513/56-5-B5/B6 CODE:0513/56-5-B5/B6

ALL

3 05 15 3 05 15

005 006

280 280

REV035 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6/T=L

ALL

3 05 15 3 05 15

007 008

280 110

REV030 REV025

CODE:0380/56-5-B5/B6 MOD:24105

ALL

3 05 15 3 05 15

009 010

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 15 3 05 15

011 012

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 15 3 05 15

013 014

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 15 3 05 15

015 016

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 15 3 05 15

017 018

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

01 MAR 2003

ALL

CCM

3.00.80 PAGE

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318/319/320/321 FCOM

VOL.3


-REV 036


019 020

280 280

REV030 REV030

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 20 3 05 20

001 002

250 280

REV030 REV030

M:24105+25800/56-5-B5/B6/B7 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

003 004

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

005 006

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

007 008

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

009 010

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

011 012

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

013 014

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20 3 05 20

015 016

280 280

REV030 REV030

CODE:0380 56-5-B5/B6 CODE:0380 56-5-B5/B6

ALL

3 05 20

017

280

REV030

CODE:0380 56-5-B5/B6

ALL

3 05 25 3 05 25

001 002

140 280

REV027 REV031

M:25800/56-5-B1 TO B7 CODE:0380/56-5-B5/B6

ALL

3 05 25 3 05 25

003 004

280 280

REV031 REV031

CODE:0380/56-5-B5/B6 CODE:0380/56-5-B5/B6

ALL

3 05 25

005

280

REV031

CODE:0380/56-5-B5/B6

ALL

3 05 30 3 05 30

001 002

120 280

REV027 REV030

M:25800/56-5-B CODE:0380 56-5-B5/B6

ALL

3 05 30

003

280

REV030

CODE 0380/CFM 56-5-B5/B6

ALL

R 3 05 35 R 3 05 35

001 002

100 135

REV036 REV025

M:22013=24105 M:20268/CFM 56-5-B6

ALL

3 05 35 3 05 35

003 004

135 001

REV025 REV026

MOD:20268 CFM 56-5-B6

ALL

3 05 35 3 05 35

005 006

145 001

REV026 REV026

MOD 20268 CFM 56-5-B6

ALL

3 05 35 3 05 35

007 008

145 001

REV026 REV026

MOD 20268 CFM 56-5-B6

ALL

3 05 35 3 05 35

009 010

001 001

REV029 REV029

ALL

3 05 35 3 05 35

011 012

001 001

REV029 REV029

ALL

01 MAR 2003

CCM

3.00.80 PAGE

16

318/319/320/321 FCOM

VOL.3


-REV 036


001 002

250 280

REV030 REV030

M:24105+25800/56-5-B5/B6/B7 CODE:0380 56-5-B5/B6

ALL

3 05 40

003

280

REV030

CODE:0380 56-5-B5/B6

ALL

3 05 50 3 05 50

001 002

001 001

REV025 REV026

3 05 50 3 05 50

003 004

110 110

REV025 REV025

3 06 00

001

001

REV024

3 06 10 3 06 10

001 002

125 001

REV027 REV024

M:25800/56-5-B

ALL

3 06 20

001

225

REV035

CODE 0380 CFM 56-5-B5/B6

ALL

3 06 30 3 06 30

001 002

125 280

REV027 REV030

M:25800/56-5-B1 TO B7 CODE 0380 CFM 56-5-B5/B6

ALL

3 06 30 3 06 30

003 004

280 280

REV030 REV030

CODE 0380/CFM 56-5-B5/B6 CODE 0380 CFM 56-5-B5/B6

ALL

3 06 30 3 06 30

005 006

280 280

REV030 REV030


ALL

3 06 30 3 06 30

007 008

280 280

REV030 REV030


ALL

3 06 30 3 06 30

009 010

280 280

REV030 REV030


ALL

3 06 30 3 06 30

011 012

280 235

REV030 REV030

CODE 0380 CFM 56-5-B5/B6 M:24105+25800/56-5-B5/B6/B7

ALL

3 06 30

013

280

REV030

CODE 0380 CFM 56-5-B5/B6

ALL

3 06 40 3 06 40

001 002

125 280

REV032 REV030

M:25800/56-5-B1 TO B7 CODE 0380/CFM 56-5-B5/B6

ALL

3 06 40 3 06 40

003 004

280 280

REV030 REV030


ALL

3 06 40 3 06 40

005 006

280 280

REV030 REV030


ALL

3 06 40

007

001

REV024

3 06 50 3 06 50

001 002

125 280

REV027 REV030

M:25800/56-5-B CODE 0380/CFM 56-5-B5/B6

ALL

3 06 50 3 06 50

003 004

280 280

REV030 REV030

CODE 0380/CFM 56-5-B5/B6 CODE 0380/CFM 56-5-B5/B6

ALL

3 06 50 3 06 50

005 006

280 280

REV030 REV030


ALL

01 MAR 2003

ALL MOD 24105 MOD 24105

ALL ALL

ALL

CCM

3.00.80 PAGE

17

318/319/320/321 FCOM

VOL.3


-REV 036


007 008

280 280

REV030 REV030


ALL

3 06 50 3 06 50

009 010

280 280

REV030 REV030


ALL

3 06 50 3 06 50

011 012

280 280

REV030 REV030


ALL

3 06 50 3 06 50

013 014

235 280

REV030 REV030

M:24105+25800/56-5-B5/B6/B7 CODE 0380 CFM 56-5-B5/B6

ALL

3 06 50

015

280

REV030

CODE 0380 CFM 56-5-B5/B6

ALL

3 06 55

001

280

REV030

CODE 0380/CFM 56-5-B5/B6

ALL

3 06 60

001

280

REV030

CODE 0380/CFM 56-5-B5/B6

ALL

3 06 70 3 06 70

001 002

002 110

REV024 REV024

MOD:24105

3 06 70

003

001

REV026

ALL

3 07 00

001-2

001

REV024

ALL

3 07 10

001-2

001

REV024

ALL

3 07 20

001

001

REV030

3 07 30 3 07 30

001 002

001 001

REV025 REV025

01 MAR 2003

ALL

LIST OF EFFECTIVE OEBS

ALL ALL

CCM

3.00.80 PAGE

18

318/319/320/321 FCOM VOLUME : 3 FLIGHT OPERATIONS LIST OF MOD/MP/SB AFFECTING THE MANUAL M V REV T

MOD

MP

TITLE

SB

...... P0164 ...........

REVISION : 036

VALIDITY

N 036

COMMUNICATIONS - DATA LINK SYSTEM DEFINE PIN PROGRAMMING ALL

. 035A 20024 ...... ...........


. 035A 20059 ...... ...........

AIR CONDITIONING - CARGO COMPARTMENT VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT ALL

. 035A 20063 ...... ...........

OXYGEN - FLIGHT CREW SYSTEM - INSTALL A 77.1 CU/FT BOTTLE IN COMPOSITE MATERIAL ALL

. 035A 20067 ...... ...........

FIRE PROTECTION - FWD CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM ALL

. 035A 20069 ...... ...........

FIRE PROTECTION - AFT CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM ALL

. 035A 20071 ...... ...........

FIRE PROTECTION - CARGO COMPARTMENT FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM ALL

. 035A 20081 ...... ...........

LIGHTS - EXTERIOR LIGHTS - INSTALL SYNCHRONIZED STROBE LIGHTS ALL

. 035A 20137 ...... ...........

COMMUNICATIONS - RADIO MANAGEMENT INSTALL A 3RD RMP ALL

. 035A 20268 ...... ...........


N 036

NAVIGATION - ADIRU - PROVIDE COMMUNITY FOR CFM AND IAE ENGINES ALL

21206 ...... ...........

CCM 01 MAR 2003

3.00.85 PAGE

1


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 21285 ...... ...........

ENGINE CONTROLS-MODIFY POWER SUPPLY FOR HP FUEL SOLENOID ALL

. 035A 21678 ...... ...........

ELECTRICAL POWER-AC/DC ESSENTIAL POWER DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPSALL

. 035A 21706 ...... ...........

AIR CONDITIONING - VENTILATION CONT. ISOLATION VALVES - CHANGE POWER SUPPLY FOR ETOPS ALL

. 035A 21729 ...... ...........

AIR CONDITIONING -AVIONICS VENTILATIONIMPROVE ACCURANCY OF SKIN TEMPERATURE READING ALL

. 035A 21812 ...... ...........

ICE AND RAIN PROTECTION WING ANTI-ICING - INSTALL MODIFIED VALVES ALL

. 035A 21899 ...... ...........

AIR CONDITIONING-AVIONICS VENTILATIONINSTALL A NRV AT AIR INLET ALL

. 035A 21946 ...... ...........

OXYGENE - COCKPIT - INSTALL MODIFIED LP OXYGEN SUPPLY SOLENOID VALVE ALL

. 035A 21964 ...... ...........

FLIGHT CONTROLS - ELAC/EFCS SYSTEM INTRODUCE SOFTWARE L62 ALL

. 035A 21988 ...... ...........

FUEL - IMPROVE LOW LEVEL WARNING ALL

. 035A 21992 ...... ...........

INDICATING/RECORDING SYSTEMS INTRODUCE CFDIU BATCH 2 ALL

N 036

NAVIGATION - INSTALL BENDIX TYPE TRA 67A ATC TRANSPONDERS (BFE) ALL

22031 ...... ...........

CCM 01 MAR 2003

3.00.85 PAGE

2


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 22087 ...... ...........

FLIGHT CONTROLS - FCDC - INSTALL SOFTWARE L45 ALL

N 036

WINGS - REMOVE LEADING EDGE VENTILATION SYSTEM ALL

. 035A 22249 ...... ...........

AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION ALL

. 035A 22373 ...... ...........

ELECTRICAL POWER - DC GENERATION INTRODUCE IMPROVED BCL ALL

. 035A 22450 ...... ...........

ICE AND RAIN PROTECTION - WING ICE PROTECTION - INTRODUCE AN IMPROVED LOW PRESSURE WARNING SWITCH ALL

. 035A 22536 ...... ...........

NAVIGATION - INSTALL A BENDIX TCAS II COLLISION AVOIDANCE SYSTEM ALL

. 035A 22561 ...... ...........

FIRE PROTECTION - LAVATORY SMOKE DETECTION - INTRODUCE AMBIENT SYSTEM ALL

. 035A 22562 ...... ...........

AIRBORNE AUXILIARY POWER UNIT INTRODUCE APIC APS-3200 ALL

. 035A 22707 ...... ...........

INDICATING RECORDING SYSTEMS - EIS DEFINE COF A STANDARD FOR A320/A321 DMC ALL

. 035A 22769 ...... ...........

NAVIGATION - GPWS - INSTALL GPWC MARK V WITH INTERFACE WITH CFDS ALL

. 035A 22875 ...... ...........

ICE AND RAIN PROTECTION - ICE DETECTION INSTALL DUAL ADVISORY ICE DETECTION SYSTEM ALL

22199 ...... ...........

CCM 01 MAR 2003

3.00.85 PAGE

3


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 23119 ...... ...........

HYDRAULIC POWER-BLUE MAIN HYDRAULIC POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR ALL

. 035A 23208 ...... ...........

LANDING GEAR - WHEELS AND BRAKES INTRODUCE BSCU STD 6 ALL

. 035A 23661 ...... ...........

ENGINE FUEL AND CONTROL - CFM 56 EIU - INTRODUCE VERSION 13 ALL

. 035A 23672 ...... ...........

NAVIGATION - ADIRS - INSTALL LITTON 4MCU ON A321 A/C ALL

. 035A 23698 ...... ...........

AUXILIARY POWER UNIT - CONTROL AND MONITORING - INTRODUCE A NEW ECB ALL

. 035A 23699 ...... ...........

AUXILIARY POWER UNIT - CONTROL AND MONITORING - MODIFY WIRE HARNESSES FOR NEW ECB 817-1 ALL

. 035A 23742 ...... ...........


. 035A 23779 ...... ...........

MINOR IMPROVEMENTS INTRODUCED FROM A/C 508 (ST2) TO A/C 521 (ST2) ALL

. 035A 23901 ...... ...........

LANDING GEAR - WHEELS AND BRAKES INTRODUCE MODIFIED ALTERNATE BRAKE DISTRIBUTION DUAL VALVE ALL

. 035A 24035 ...... ...........


CCM 01 MAR 2003

3.00.85 PAGE

4


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 24064 ...... ...........


. 035A 24077 ...... ...........

LANDING GEAR - BSCU - TWIN WHEEL INTRODUCE A320/A321 STD 6 VERSION 60C ALL

. 035A 24105 ...... ...........


. 035A 24215 ...... ...........

AUTO FLIGHT - FAC - INSTALL TWO FACS P/N BAM 0509 ALL

. 035A 24373 ...... ...........

FUEL - TANK LEVEL SENSING - INTRODUCE MODIFIED LOW FUEL PRESSURE WARNING CONTROL ALL

. 035A 24440 ...... ...........

LANDING GEAR-NOSE LANDING GEARSHOCK ABSORBER-INTRODUCE MODIFIED THROTTLING ROD GUIDE ALL

. 035A 24449 ...... ...........

LANDING GEAR - A320/A321 TWIN WHEELS INTRODUCE BSCU STANDARD 7 (70B VERSION) ALL

. 035A 24498 ...... ...........

APU - STORAGE AND DISTRIBUTION MODIFY APU COMMON LUBRICATION SYSTEM ALL

. 035A 24511 ...... ...........

FLIGHT CONTROLS -S.E.C. SYSTEM INTRODUCE A320/A321 S.E.C STANDARD P/N BAM0508 ALL

. 035A 24588 ...... ...........

AUTO FLIGHT-FAC-INTRODUCE FAC P/N BAM 510 ALL

CCM 01 MAR 2003

3.00.85 PAGE

5


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 24612 ...... ...........

INDICATING/RECORDING SYSTEMS - FWC INTRODUCE FWC D2 STD ALL

. 035A 24613 ...... ...........

FLIGHT CONTROLS - ELAC - INTRODUCE ELAC STD P/N L69 ALL

. 035A 24642 ...... ...........

ELECTRICAL POWER - AC AUXILIARY GENERATION (APU GENERATOR) - INTRODUCE MODIFIED GENERATOR ALL

. 035A 24645 ...... ...........

LANDING GEAR-MLG-LGCIU-INTRODUCTION OF STANDARD UNIT P/N A4C ALL

N 036

COMMUNICATIONS-CIDS-INTRODUCE MODIFIED DIRECTOR POWER SUPPLY PRINCIPLE ALL

. 035A 24783 ...... ...........

ENGINE FUEL AND CONTROL-FUNCTIONAL INTERFACE-INTRODUCE EIU VERSION 14 ON CFM56 ENGINES ALL

. 035A 24794 ...... ...........

AIR CONDITIONING-COCKPIT AND CABIN TEMPERATURE CTRL-INTRODUCE MODIFIED TEMPERATURE SENSOR P/N-02.ON MIXER UNIT ALL

. 035A 24805 ...... ...........

PNEUMATIC-ENGINE BLEED AIR SUPPLYINTRODUCE A BLEED AIR MONITORNG COMPUTER STD6 ALL

. 035A 24852 ...... ...........

NAVIGATION-ADIRU-INTRODUCE ADIRU P/N -307 ALL

. 035A 24917 ...... ...........

FLIGHT CONTROLS-INTRODUCE ELAC STD L69J ALL

24771 ...... ...........

CCM 01 MAR 2003

3.00.85 PAGE

6


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 24946 ...... ...........

LANDING GEAR - MLG - MESSIER INTRODUCE BRAKES P/N C202253 ALL

. 035A 24955 ...... ...........

AIRBORNE AUXILIARY POWER-ENGINEAPIC APS 3200-INTRODUCE MODIFIED PRESS REGULATOR ON FCU ALL

. 035A 25199 ...... ...........

FLIGHT MANAGEMENT AND GUIDANCE SYSTEMINSTALL FMGC ON A320/321 (CFM 56-5A/5B) ALL

. 035A 25241 ...... ...........

COMMUNICATIONS - RADIO MANAGEMENT INSTALL A NEW STD RMP1 AND RMP2 WITH VHS SPACING 8, 33KHZ ALL

. 035A 25242 ...... ...........

COMMUNICATIONS - RADIO MANAGEMENT INSTALL A NEW STD RMP3 (3⁰) WITH VHF SPACING 8, 33KHZ ALL

. 035A 25287 ...... ...........


. 035A 25294 ...... ...........


. 035A 25335 ...... ...........

FLIGHT CONTROLS-ELAC-INTRODUCE A319 EIS L77 SOFTWARE STDALL

. 035A 25336 ...... ...........

NAVIGATION-ADIRS-INTRODUCE AIRU LITTON P/N -308 ALL

. 035A 25360 ...... ...........

FLIGHT CONTROLS-SLATS/FLAPS-ELECTRICAL CONTROL AND MONITORING INTRODUCE SFCC P/N 07 ON A319 A/C AND A321 AIRCRAFT ALL

CCM 01 MAR 2003

3.00.85 PAGE

7


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 25404 ...... ...........

EXHAUST-THRUST REVERSER CONTROL AND INDICATING-ACTIVATE ADDITIONAL THRUST REVERSER LOCK CONTROL ALL

. 035A 25410 ...... ...........

INDICATING RECORDING SYSTEM-FWCINTRODUCE F.W.C. E1 STANDARD ALL

. 035A 25419 ...... ...........

ICE AND RAIN PROTECTION-WINDSHIELD RAIN PROTECTION-DESACTIVATION OF RAIN REPELLENT SYSTEM ALL

N 036

NAVIGATION - GENERAL - CHANGE EQUIPMENTS TO COMPLY WITH MARCH 95 SPECS. ALL

. 035A 25529 ...... ...........

NAVIGATION - WEATHER RADAR SYSTEM ACTIVATE PREDICTIVE WINDSHEAR FUNCTION ALL

. 035A 25530 ...... ...........


. 035A 25800 ...... ...........

POWER PLANT-GENERAL-INTRODUCE CFM56-5B/P ALL

. 035A 25863 ...... ...........


. 035A 25871 ...... ...........

ENGINE FUEL AND CONTROL-CONTROLLINGINTRODUCE ECU SOFTWARE 5DH FOR CFM56-5B (DAC -DAC/P) ENGINES ALL

N 036

NAVIGATION-ADIRS-INTRODUCE HONEYWELL ADIRU 4 MCU STD WITH HARDWARE P/N AD09 ALL

25440 ...... ...........

26000 ...... ...........

CCM 01 MAR 2003

3.00.85 PAGE

8


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 26001 ...... ...........

NAVIGATION-ADIRS-INTRODUCE HONEYWELL 4 MCU P/N AC09 ALL

. 035A 26002 ...... ...........


. 035A 26017 ...... ...........

INDICATING/RECORDING SYSTEMS-FLIGHT WARNING COMPUTER (FWC)-INTRODUCE FWC ST2 E2 ALL

. 035A 26018 ...... ...........


. 035A 26187 ...... ...........

NAVIGATION - VOR - INSTALL VOR RECEIVERS ALLIED SIGNAL QUANTUM LINE P/N 066-50012-0202 ALL

. 035A 26363 ...... ...........

AIR CONDITIONING-AIR COOLING SYSTEMINTRODUCE MODIFIED RAM AIR OUTLET ALL

. 035A 26377 ...... ...........

NAVIGATION - ILS - INSTALL ADDITIONAL WIRING PROVISIONS FOR MMR INSTALLATION ALL

N 036

ADDITIONAL CERTIFICATION ITEMS LANDING WITH A 15 KNOT TAILWIND ALL

. 035B 26443 ...... ...........

NAVIGATION - VOR/MARKER - INSTALL TWO VOR/MARKER RECEIVERS 900 COLLINS P/N 822-0297-020 OO-SSF

. 035A 26457 ...... ...........

GENERAL - DESIGN WEIGHTS - INCREASE MAXIMUM TAKE-OFF WEIGHT (MTOW) TO 68T ALL

26398 ...... 00-1043 06

CCM 01 MAR 2003

3.00.85 PAGE

9


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 26526 ...... ...........

NAVIGATION - GPWS - ACTIVATE ENHANCED FUNCTIONS OF THE EGPWS ALL

. 035A 26642 ...... ...........

ENGINE -CONTROLLING-CFM56-5B/2 FADEC SYSTEM-INTRODUCE ECU STD 5DK ALL

. 035A 26645 ...... ...........

AUTO-FLIGHT-FAC INTRODUCE FAC STD BAM 0513 ALL

. 035A 26726 ...... ...........

INDICATING/RECORDING SYSTEM-SDACINTRODUCE SDAC (NEW TECHNOLOGY ) ALL

. 035A 26785 ...... ...........

PNEUMATIC-ENG BLEED AIR SYS-INTRODUCE A TEMP THERMOSTAT WITH MODIFIED LIMITATION SETTINGS (P/N 341E020000) ALL

. 035A 26792 ...... ...........

AIR CONDITIONING-PACK TEMPERATURE CTRLINTRODUCE MODIFIED PACK TEMPERATURE CONTROLLER ALL

. 035A 26963 ...... ...........

ICE AND RAIN PROTECTION-WINSHIELD RAIN PROTECTION-ACTIVATION OF RAIN REPELLENT SYS.(FLUID COMPATIBLE WITH OZONE RULES) ALL

. 035A 26968 ...... ...........


. 035B 26999 ...... ...........

NAVIGATION - MMR - INSTALL COLLINS MMR PROVIDING ILS AND GPS FUNCTION OO-SSF

. 035A 27276 ...... ...........

FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ELAC SOFTWARE DL80D ALL

CCM 01 MAR 2003

3.00.85 PAGE 10


MOD

MP

REVISION : 036

TITLE

SB

VALIDITY

. 035A 27498 ...... ...........

ELECTRICAL POWER - GENERAL - AC-DC MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS ALL

. 035B 27522 ...... ...........


. 035A 27572 ...... ...........

OXYGEN-PASSENGER OXYGEN-INTRODUCE MODIFIED CHEMICAL OXYGEN CONTAINER -15 MIN- PURITAN ALL

. 035A 27646 ...... ...........

NAVIGATION - MMR - INSTALL SEXTANT MMR PROVIDING ILS (FM IMMUNE) ALL

. 035A 27698 ...... 34-1177 10

NAVIGATION - TCAS - INSTALL ALLIED SIGNAL TCAS COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0) ALL

. 035A 27723 ...... ...........

PNEUMATIC-ENGINE BLEED AIR SUPPLY SYSTEM-INTRODUCE NEW TEMPERATURE CTL THERMOSTATS (SERIAL AND RETROFIT) ALL

. 035A 27725 ...... ...........

ENGINE FUEL AND CONTROL-FADEC SYSTEMINTRODUCE ECU SOFTWARE 5DM FOR CFM56-5B DAC ENGINE ALL

. 035A 27727 ...... ...........

ENGINE -COMBUSTION SECTIONINTRODUCE CFM56-5B DAC II PIP ENGINES ALL

. 035A 27866 ...... 34-1178 06

NAVIGATION - WEATHER RADAR SYSTEM INSTALL ALLIED SIGNAL WEATHER RADAR TRANSCEIVER P/N 066-50008-0405 ALL

CCM 01 MAR 2003

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TITLE

SB

VALIDITY

. 035A 27952 ...... ...........

PNEUMATIC-ENGINE BLEED AIR SYSTEMINTRODUCE TLT P/N 341E030000 ALL

. 035A 28009 ...... 21-1116 04

AIR CONDITIONING-PRESSURE CONTROL AND MONITORING-INTRODUCE PRESSURE CONTROLLER P/N 9022-15702-10 ALL

. 035A 28164 ...... ...........

LANDING GEAR - WHEELS AND BRAKES INSTALL CARBON BRAKES TYPE SEPCARB III PLUS - MESSIER BUGATTI ALL

. 035A 28218 ...... ...........


. 035A 28244 ...... 34-1193 18

NAVIGATION-GPWS-INTRODUCE EGPWS P/N 206-206 AND INHIBIT AUTOMATIC DEACTIVATION ENHANCED FUNCTIONS ALL

. 035A 28284 ...... ...........

NAVIGATION-ILS-INSTALL SEXTANT MMR PROVIDING ILS (FM IMMUNE) P/N TLS 755.01.0101B ALL

. 035B 28360 ...... ...........


. 035A 28377 ...... ...........

ICE AND RAIN PROTECTION-WINSHIELDRAIN PROTECTION-INTRODUCE MODIFIED GAGE ASSY -P/N 4020W35-2 ALL

. 035A 28382 ...... ...........


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. 035A 28488 ...... ...........

AIR CONDITIONING-PACK TEMP.CTRL INTRODUCE MODIFIED PACK TEMP. CTRL P/N 759D0000-02 ALL

. 035B 28495 ...... ...........


. 035A 28667 ...... ...........

ICE AND RAIN PROTECTION-WINDSHIELD RAIN PROTECTION-INTRODUCE MODIFIED GAGE ASSY WITH INPUT VALUE FUNCTION SUPPRESSED ALL

. 035B 28669 ...... ...........

NAVIGATION-VOR/MARKER-REINTRODUCE COLLINS 700 VOR/MARKER RECEIVERS (PREVIOUS A/C STANDARD SPECIFICATION) OO-SSF

. 035B 30239 ...... 46-1009 06

INFORMATION SYSTEM - ATIMS - MODIFY ATSU AIRCRAFT INTERFACE SOFTWARE ACCORDING TO SERVICE PROVIDERS LIST OO-SSF

N 036

FLIGHT CONTROLS - ELAC SYSTEM INTRODUCE ELAC STD L81 ALL

31395 ...... 27-1135 02

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318/319/320/321 FCOM VOL.4 REV014



OO-SSB OO-SSF

CCM 01 DEC 2002

4.00.70 PAGE : CRT001

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014


002

100 REV014 -

4 02 20

003

4 02 20

006

007

4 02 20

009

OF OF OF OF

MOD MOD MOD MOD

26485 28495 30631 30635

CODE 0056

INCORPORATION OF MOD 31364 INCORPORATION OF MOD 31365 DELETION OF MOD 25240 DELETION OF MOD 25274

100 REV011 -

CODE:0101

INCORPORATION INCORPORATION INCORPORATION INCORPORATION

100 REV011 -

4 02 20

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)+Required+ and +Estimated+ navigation accuracy values have be revised to reflect more realistic Enroute values on the MCDU, in accordance with the EFIS ND display.

100 REV008 -

CODE:0101

CODE 0056

INCORPORATION OF MOD 31364 INCORPORATION OF MOD 31365 DELETION OF MOD 25240 DELETION OF MOD 25274

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)The missing reference to the LATERAL FUNCTIONS chapter 4.04 has been added. 4 02 20

011

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)Switching conditions from the CRUISE phase to the DESCENT phase are modified to reflect the actual behavior of the A320 FMS Legacy. 4 02 20

014

100 REV006

CODE 0002

- DELETION OF MOD 25240 - DELETION OF MOD 25274 4 02 20

014

100 REV014

CODE 0056

- TECHNICAL AMENDMENT 1)The CG is not considered for the BEST TARGET SPEED computation.

01 DEC 2002

CCM

4.00.75

PAGE

1

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VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014


015

100 REV007

CODE 0002


015

100 REV014

CODE 0056

- TECHNICAL AMENDMENT 1)Addition of a note regarding the OPTIMUM FLIGHT LEVEL (OPT FL) computed by the FMS : differences between the FCOM/QRH and the FMS value may be observed, and wind entries made at different altitudes may affect the FMS-computed OPTIMUM FLIGHT LEVEL. . 4 02 20

016

100 REV012 -

4 02 20

018

CODE 0056

INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION INCORPORATION

001 REV014

OF OF OF OF OF OF

MOD MOD MOD MOD MOD MOD

26968 27831 28283 28711 31364 31365

CODE 0055


022

001 REV014 - TECHNICAL AMENDMENT 1)Reference to required distance to land and direct distance to destination have been removed, as they are already described in the corresponding MCDU DES PROG page description section.

4 02 30

002

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)Addition of a note for selecting the LOC* and LOC modes by using the FCU)s LOC pushbutton, rather than the APPR pushbutton, in case of a LOC only approach. 4 02 30

007

100 REV006

CODE 0002


007

100 REV014

CODE 0056

- TECHNICAL AMENDMENT 1)Page revised to clarify the DESCENT SPEED PROFILE definition.

01 DEC 2002

CCM

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2

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014


010

001 REV014 - TECHNICAL AMENDMENT 1)When in a holding pattern, the aircraft will respect the altitude constraints as well as the FCU selected altitude.

4 02 30

012

001 REV014 - TECHNICAL AMENDMENT 1)The APPROACH MODES have been clarified to introduce the precision and non-precision approach concept. Furthermore, the LOC and LOC B/C approach types are clarified to highlight that the APPR pushbutton is not used to arm the LOC guidance mode, but the LOC pushbutton is.

4 03 00

001

001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)Contents update. 4 03 10

002

110 REV014

CODE 0033

- TECHNICAL AMENDMENT 1)Addition of information to reflect that the PFD)s altitude display in metric units is an +as installed+ item. 4 03 20

003

100 REV011

CODE 0002


004

100 REV006

CODE 0002


005

100 REV011

CODE 0002


008

100 REV006

CODE 0002


009

100 REV011

CODE 0002


010

100 REV006

CODE 0002

- DELETION OF MOD 25240 - DELETION OF MOD 25274

01 DEC 2002

CCM

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3

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VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014


011

100 REV008

CODE 0002


012

001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)After first engine start, the FMGS computes predictions based on the FQI FOB (FAC as backup), and not on the BLOCK entry. 4 03 20

014

100 REV008

CODE 0002


015

100 REV006

CODE 0002


026

001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensured correct page validation for all customers. 4 03 20

032

105 REV011

CODE 0096

- INCORPORATION OF MOD 28283 - DELETION OF MOD 25240 - DELETION OF MOD 25274 4 03 20

033

100 REV007

CODE 0002


052

100 REV014 -

4 03 20

053

01 DEC 2002

INCORPORATION OF MOD 26485 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)Page updated to further specify the aircraft definition : GPS PRIMARY Function is installed.

100 REV011 -

CODE:0101

CODE:0101

INCORPORATION OF MOD 25025 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 DELETION OF MOD 23885 DELETION OF MOD 24075 DELETION OF MOD 25205

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PILOT)S GUIDE

HIGHLIGHTS

REV014


054

100 REV014 -

4 03 20

055

CODE:0101

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28382 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)Page created to further specify the aircraft definition : The +DESELECT/ SELECT GPS 5L+ key is installed.

105 REV009

CODE:0102

- INCORPORATION OF MOD 26485 - INCORPORATION OF MOD 28495 - INCORPORATION OF MOD 30631 4 03 20

056

100 REV014

CODE 0082


060

100 REV014

CODE 0082

- TECHNICAL AMENDMENT 1)Information has been moved to the next page for pagination purposes. 4 03 20

061

100 REV014

CODE 0082

- TECHNICAL AMENDMENT 1)Information has been moved from the previous page for pagination purposes. 2)If the uplinked TOW/TOCG differs from an already existing TOW/TOCG, the INSERT UPLINK* prompt is not displayed. 4 03 20

071

001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)Clarification of the conditions for displaying or blanking the MCDU PERF fields. 4 03 20

072

100 REV006

CODE 0002


073

100 REV006

CODE 0002

- DELETION OF MOD 25240 - DELETION OF MOD 25274

01 DEC 2002

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5

318/319/320/321 FCOM

VOL. 4

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HIGHLIGHTS

REV014


080

100 REV014 -

4 03 20

081

4 03 20

082

083

4 03 20

084

CODE:0101

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)The +Required+ navigation accuracy field has been revised to reflect more realistic TERMINAL area values on the MCDU PROG page.

100 REV014 -

CODE:0056

INCORPORATION OF MOD 27831 INCORPORATION OF MOD 28283 INCORPORATION OF MOD 28711 INCORPORATION OF MOD 31364 INCORPORATION OF MOD 31365 TECHNICAL AMENDMENT 1)Page revised to indicate that the maximum REC MAX value is FL391 instead of FL390.

100 REV014 -

4 03 20

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)The +Required+ and +Estimated+ navigation accuracy values have been changed on the PROG CRUISE and PROG DES pages to be consistent with the current navigation mode (GPS PRIMARY) in the Enroute area.

100 REV014 -

CODE:0101

CODE:0101

INCORPORATION OF MOD 25205 INCORPORATION OF MOD 26111 INCORPORATION OF MOD 26485 INCORPORATION OF MOD 26999 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30241 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)Reference to the FCOM Volume 1 replaces previous reference to the FCOM Volume 4.

100 REV006

CODE:0114

- INCORPORATION OF MOD 24105 - INCORPORATION OF MOD 25294 01 DEC 2002

CCM

4.00.75

PAGE

6

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014


084

100 REV006

CODE:0114

- INCORPORATION OF MOD 28495 - DELETION OF MOD 25205 - DELETION OF MOD 30241 4 03 20

085

100 REV006 -

4 03 20

089

CODE:0114

INCORPORATION OF MOD 24105 INCORPORATION OF MOD 25294 INCORPORATION OF MOD 28495 DELETION OF MOD 25205 DELETION OF MOD 30241

105 REV006

CODE 0002


001

001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)The conditions for displaying the +ALIGN IRS+ message have been clarified. 4 04 00

001

001 REV006

CODE 0055

- TECHNICAL AMENDMENT 1)Index tailored to FMS2 Thales/Smiths (rev 1). 4 04 10

014

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)The MCDU screens have been changed to reflect the actual holding pattern and correct display. Text has also been modified for improved technical understanding. 4 04 10

015

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)When in a holding pattern, the aircraft will respect the altitude constraints as well as the FCU selected altitude. 4 04 10

021

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)Page modified for better technical understanding. 4 04 10

022

001 REV014

CODE 0055


030

001 REV014 - TECHNICAL AMENDMENT 1)The PROG page displayed as an

01 DEC 2002

CCM

4.00.75

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7

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------example was amended to show a more realistic situation. 4 04 20

003

100 REV006

CODE 0002


004

100 REV006

CODE 0002


005

100 REV006

CODE 0002


006

100 REV011

CODE 0002


007

100 REV006

CODE 0002


008

100 REV006

CODE 0002


003

001 REV014 - TECHNICAL AMENDMENT 1)+PROCEDURES+ item has been modified : if there is an AMSL Altitude constraint above the transition altitude in the departure procedure, the crew must convert it into STD before insertion in the MCDU. 2)The sequence number was changed to ensure the correct page validation for all customers.

4 04 30

010

001 REV014

CODE 0055


017

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)The reference to +Multifunction Control and Display Unit+ has been amended to read +MCDU+. 4 04 30

018

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number was changed to ensure the 01 DEC 2002

CCM

4.00.75

PAGE

8

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------correct page validation for all customers. 4 04 30

021

001 REV014

CODE 0055

- TECHNICAL AMENDMENT 1)The reference to +Multifunction Control and Display Unit+ has been amended to read +MCDU+. 4 05 10

003

100 REV006

CODE 0002


004

100 REV006

CODE 0002


007

100 REV006

CODE 0002


008

100 REV006

CODE 0002


010

100 REV007

CODE 0002


010

100 REV014

CODE 0056

- TECHNICAL AMENDMENT 1)The note about altitude constraint entries has been clarified. 4 05 10

014

001 REV014

CODE 0055


021

100 REV014

CODE 0058

- TECHNICAL AMENDMENT 1)During cockpit preparation, the PERF CLB page is accessed by pressing the +NEXT PHASE+ prompt on the PERF TAKEOFF page, not by the MCDU +NEXT PAGE+ key. 4 05 10

022

100 REV014

CODE 0058

- TECHNICAL AMENDMENT 1)Access to the PERF CRZ page has been clarified. 4 05 30

006

001 REV014 - TECHNICAL AMENDMENT 1)No technical change. The sequence

01 DEC 2002

CCM

4.00.75

PAGE

9

318/319/320/321 FCOM

VOL. 4

PILOT)S GUIDE

HIGHLIGHTS

REV014

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------number was changed to ensure the correct page validation for all customers. 4 05 40

001

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INCORPORATION OF MOD 26485 INCORPORATION OF MOD 28495 INCORPORATION OF MOD 30631 INCORPORATION OF MOD 30635 TECHNICAL AMENDMENT 1)FCOM page revised to reflect the correct MCDU display corresponding to the procedure.

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- TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure correct validity for all customers. 4 05 70

001

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001 REV014 - TECHNICAL AMENDMENT 1)A caution is added to advise the crew not to select the APPR pushbutton for

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006

001 REV014

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007

001 REV014

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- TECHNICAL AMENDMENT 1)No technical change. The sequence number has been changed to ensure correct validity for all customers. 4 06 20

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001 REV014

CODE:0055

- TECHNICAL AMENDMENT 1)No technical change. The sequence number has changed to ensure correct validity for all customers.

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REV011 REV006

CODE 0055 CODE 0055

ALL

01 DEC 2002

ALL M:24035=24160=24211 ALL

ALL

CCM

4.00.80 PAGE

10

318/319/320/321 FCOM

VOL.4


) PAGES (LEP) -

-REV 014


015

01 DEC 2002

001

REV006

CODE 0055

CCM

ALL

4.00.80 PAGE

11

318/319/320/321 FCOM VOLUME : 4 PILOT)S GUIDE LIST OF MOD/MP/SB AFFECTING THE MANUAL M V REV T

MOD

MP

REVISION : 014

TITLE

SB

VALIDITY

. 013A 23353 ...... ...........

AUTO FLIGHT - FMS - PROVIDE FMS CROSS LOAD ALL

N 014

AUTO FLIGHT - MCDU 1 AND 2 - SOFTWARE UPGRADED (CI-20) ALL

. 013A 23742 ...... ...........


. 013A 24035 ...... ...........


. 013A 24064 ...... ...........


. 013A 24105 ...... ...........


. 013A 24309 ...... ...........

AUTO FLIGHT - FMGC - PROVIDE TIME CONSTRAINT AND TEN CHARACTERS RTE IDENT FUNCTIONS ALL

. 013A 24414 ...... ...........

AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) DELETE +EXPEDITE+ FUNCTION FROM FCU ALL

. 013A 24735 ...... ...........

AUTOFLIGHT-FCU- INTRODUCE MODIFIED PIN/SOCKET CONNECTOR ON FCU WITH EXPEDITE FUNCTION DELETED (FCU BBM10) ALL

N 014

COMMUNICATIONS-INTERPHONEINTRODUCE IDENTIFICATION LABEL FOR INTERPHONE JACKS 1RJ/2RJ ALL

23593 ...... ...........

25025 ...... ...........

CCM 01 DEC 2002

4.00.85 PAGE

1


MOD

MP

TITLE

SB

25294 ...... ...........

REVISION : 014

VALIDITY

N 014


. 013A 25295 ...... ...........

AUTOFLIGHT - FMGC - ACTIVATE ACARS INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 013A 25345 ...... ...........

AUTOFLIGHT-FCU-INTRODUCE F.C.U. STANDARD M11 ALL

. 013A 25346 ...... ...........

AUTOFLIGHT-FCU-INTRODUCE FCU STANDARD M11 WITHOUT EXPEDITE FUNCTION ALL

. 013A 25381 ...... ...........

AUTOFLIGHT - FMGC - ACTIVATE PRINTER INTERFACE IN FMS (CFM AND IAE ENGINES) ALL

. 013A 25863 ...... ...........


. 013A 26002 ...... ...........


N 014

26495 ...... ...........

WINGS-INBOARD FLAP-MODIFY SLIDING PANEL DRIVING MECHANISM ALL

. 013A 26497 ...... ...........

AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL SPEED PROTECTION AND F/D DISENGAGEMENT UPON SPEED CONSTRAINTS ALL

. 013A 26968 ...... ...........


CCM 01 DEC 2002

4.00.85 PAGE

2


MOD

MP

REVISION : 014

TITLE

SB

VALIDITY

. 013B 26999 ...... ...........

NAVIGATION - MMR - INSTALL COLLINS MMR PROVIDING ILS AND GPS FUNCTION OO-SSF

. 013A 27256 ...... ...........

AUTO FLIGHT - MULTIPURPOSE CONTROL AND DISPLAY UNIT (MCDU) - INTRODUCE MCDU HONEYWELL 2ND GENERATION (P/N -980) ALL

. 013B 27522 ...... ...........


. 013A 27541 ...... ...........

AUTO FLIGHT - MCDU - INSTALL AN MCDU 2ND GENERATION HONEYWELL FMS (MCDU WITH A340 KEYBOARD) ALL

. 013A 28218 ...... ...........


. 013B 28360 ...... ...........


N 014

28381 ...... ...........

ELECTRIC/ELECTRONIC COMMON INSTALLATION - MODIFY CONNECTOR INTERFACE PLATE FOR ELECTRICAL CONVERTIBLE SEATS ALL

. 013A 28382 ...... ...........


N 014


28495 ...... ...........

CCM 01 DEC 2002

4.00.85 PAGE

3

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Airbus 319, A320, A321 Fcom

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