A350 Avionics

MAINTENANCE T R A I N I N G H A N D B O O K

PART 2 : ELECTRO - MECHANICAL SYSTEMS FOR TRAINING ONLY - V01T0MTH

JULY 2014

This document must be used for training purposes only

Under no circumstances should this document be used as a reference

It will not be updated.

© Airbus SAS 2014. All rights reserved. Confidential and proprietary document. No part of this manual may be reproduced in any form, by photostat, microfilm, retrieal system, or any other means, without the prior written permission of AIRBUS S.A.S.

AIRBUS Environmental Recommendation Please consider your envrionmental responsability before printing this document.

SUMMARY

Training by Airbus

- GENERAL - AVIONICS - AIRFRAME - POWERPLANT Gl.

COMPUTER & C/B LOCATIONS

EXTERNAL PANELS

CHECK LIST - WALK AROUND & COCKPIT

P. 49

P. 23

P. 8

ATA 24 - ELECTRICAL POWER ATA 42 - INTEGRATED MODULAR AVIONICS AND AVIONICS DATA COMMUNICATION NETWORK ATA 31 - INDICATING / RECORDING SYSTEMS ATA 46 - INFORMATION SYSTEMS ATA 45 - ONBOARD MAINTENANCE SYSTEM ATA 34 - NAVIGATION ATA 22 - AUTO FLIGHT ATA 23 - COMMUNICATIONS ATA 44 - CABIN SYSTEMS

ATA 30 - ICE & RAIN PROTECTION

ATA 47 - INERT GAS SYSTEM

ATA 21 - AIR CONDITIONING

ATA 36 - PNEUMATIC

ATA 70 - STANDARD PRACTICES - ENGINES

ATA 49 - AIRBORNE AUXILIARY POWER

ATA 26 - FIRE PROTECTION SYSTEMS

ATA 28 - FUEL

ATA 38 - WATER AND WASTE

ATA 35 - OXYGEN

ATA 27 - FLIGHTS CONTROLS

ATA 25/50 - EQUIPMENT & FURNISHING AND CARGO & ACCESSORY COMP.

ATA 52 - DOORS

ATA 51 - STANDARD PRACTICES AND STRUCTURES

ATA 32 - LANDING GEARS

ATA 29 - HYDRAULIC POWER

P. 610

P. 593

P. 590

P. 530

P. 520

P. 487

P. 473

P. 449

P. 428

P. 416

P. 409

P. 384

P. 371

P. 356

P. 349

P. 305

P. 289

ATA 33 - LIGHTS

CONVERSION TABLE, LIST ABBREVIATION & SYMBOLS CARD

REF TO PART 1: ELECTRO - AVIONICS SYSTEMS

Training by Airbus

GENERAL CHECK LIST - WALKAROUND & COCKPIT

P. 8

EXTERNAL PANELS

P. 23

COMPUTER & C/B LOCATIONS

P. 49

© Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

CHECK LIST - WALKAROUND & COCKPIT

EXTERIOR WALKAROUND Training by Airbus

2

1

- FUSELAGE / DOORS................................................... CHECK CONDITION - WING AND ENGINE SCAN LIGHTS............................ CHECK CONDITION - STATIC PROBES.......................................................... CLEAR - NEGATIVE PRESSURE VALVE................................... CLOSED - CREW OXYGEN DISCHARGE INDICATOR................ GREEN - CAMERA LIGHT .......................................................... CHECK CONDITION (if installed) - AVIONICS COMPARTMENT DOOR............................. CLOSED - BATTERY EXHAUST (YELLOW DISK)…………...…... CHECK CONDITION - STAND-BY STATIC PROBES....................................... CLEAR - STAND-BY PITOT PROBE........................................... CHECK CONDITION - MULTI-FUNCTIONS PROBE (MFP)…......................... CHECK CONDITION - AOA PROBE................................................................. CHECK CONDITION - ICE DETECTOR PROBE……………............................ CHECK CONDITION

3

1

4 5

22

7

23 24

8

6

21

9 12

18 13

20

LH FWD FUSELAGE :

10

2 NOSE SECTION : 19

11

14

17

- FUSELAGE................................................................... CHECK CONDITION - RADOME....................................................CHECK CONDITION / LATCHED - SIDESLIP PROBES...................................................... CHECK CONDITION - ICE DETECTION VISUAL INDICATORS...................... CHECK CONDITION - WIPERS......................................................................... CHECK CONDITION

CHECK CONDITION : NO DAMAGE, NO DENT, NO IMPACT MARK, NO DEFORMATION, NO CRACK, NO FOD PRESENCE, NO MISSING ELEMENT, NO LEAK.

15

16

Page 8 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ch List

EXTERIOR WALKAROUND Training by Airbus 2

3 NOSE L/G : - FUSELAGE................................................................... CHECK CONDITION - CHOCKS....................................................................... IN PLACE - WHEEL WELL / DOORS.............................................. CHECK CONDITION - TAKEOFF, TAXI AND TURN OFF LIGHTS ................. CHECK CONDITION - NOSE GEAR STRUCTURE.......................................... CHECK CONDITION - HYD AND ELEC LINES AND EQUIPMENT.................. CHECK CONDITION - DOWNLOCK SPRINGS................................................ CHECK CONDITION - WHEELS AND TIRES................................................... CHECK CONDITION - OAT PROBES............................................................... CHECK CONDITION - GROUND ELECTRICAL POWER DOOR (IF NOT REQUIRED)..... CLOSED - WATER DRAIN VALVE................................................. NO LEAK

3

1

4 5

22

7

23 24

8

6

21

9 12

18

4 RH FWD FUSELAGE :

13

20

10

19

11

14

17

15

16

- FUSELAGE / DOORS................................................... CHECK CONDITION - STAND-BY STATIC PROBES....................................... CLEAR - MULTI-FUNCTIONS PROBES (MFP)…....................... CHECK CONDITION - ICE DETECTOR PROBE……………............................ CHECK CONDITION - NLG DOOR OPENING HANDLE……..………………... STOWED - BATTERY EXHAUST (YELLOW DISK)…..……...….... CHECK CONDITION - CAMERA LIGHT .......................................................... CHECK CONDITION - CARGO DOOR............................................................. CLOSED - ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED - NEGATIVE PRESSURE VALVE................................... CLOSED - STATIC PROBES.......................................................... CLEAR - WING AND ENGINE SCAN LIGHTS............................ CHECK CONDITION - CREW OXYGEN DISCHARGE INDICATOR................ GREEN



Ch List


5 LOWER CENTER FUSELAGE :

3

1

4 5

22

7

23 24

8

6

21

9 12

18 13

20

10

19

11

14

- FUSELAGE................................................................... CHECK CONDITION - ANTENNAS................................................................... CHECK CONDITION - AVIONICS VENTILATION OVERBOARD VALVE........ CHECK CONDITION - CAMERA....................................................................... CHECK CONDITION - OUTFLOW VALVE........................................................ CHECK CONDITION Normally wide open. If not, risk of pressurized A/C) - DRAIN MAST................................................................. CHECK CONDITION - COMPARTMENT AIR EXTRACTION OUTLET............ CHECK CONDITION (Option) - BILGE DRAIN HOLES.................................................. NO LEAK - BELLY FAIRINGS......................................................... CHECK CONDITION - PACK BAY VENTILATION AIR INTAKES.................... CLEAR - RAM AIR INLET FLAP.................................................. CHECK CONDITION - ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED / CHECK CONDITION - PACK AIR INTAKES..................................................... CLEAR - BEACON LIGHT………................................................ CHECK CONDITION - PACK BAY VENTILATION AIR OUTLETS................... CLEAR - PACK AIR OUTLETS.................................................... CLEAR - CONDITIONED SERVICE AIR SYSTEM OUTLETS…...................... CLEAR - MLG BAY VENTILATION AIR INLET (ON LEFT SIDE ONLY)…...... CLEAR - FUEL PUMPS DRAIN HOLES...................................... NO LEAK

6 17

15

16


RH CENTER WING :

- WING / PANELS............................................................ CHECK CONDITION - WING FUEL TANK WATER DRAIN VALVE.................. NO LEAK - IGGS OUTLET............................................................... CHECK CONDITION - LANDING LIGHT........................................................... CHECK CONDITION - SLAT 1………................................................................ CHECK CONDITION


Ch List


7

2

- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION - AERODYNAMIC STRAKE............................................ CHECK CONDITION - DRAIN MAST................................................................ CHECK CONDITION / NO LEAK - STARTER VALVE OVERRIDE ACCESS..................... CLOSED - ENGINE ANTI-ICE EXHAUST GRID............................ CHECK CONDITION - ENGINE INLET AND FAN BLADES............................ CHECK CONDITION

3

1

4 5

22

8 7

23 24

6 9 12

18 13

10

19

11

14

ENG 2 RH SIDE :

- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION - ENGINE OIL FILL ACCESS DOOR.............................. CLOSED - ENGINE VENTILATION EXHAUST GRID.................... CHECK CONDITION - LATCH ACCESS DOORS…………………………...….. CLOSED - TURBINE EXHAUST..................................................... CLEAR

8

21

20

ENG 2 LH SIDE :

9

RH WING LEADING EDGE :

- WING / PANELS........................................................... CHECK CONDITION - REFUEL COUPLING DOOR........................................ CLOSED - SLATS 2, 3, 4................................................................ CHECK CONDITION

10 RH WING TIP :

17

15

16

- WING / PANELS............................................................ CHECK CONDITION - SLATS 5, 6, 7................................................................ CHECK CONDITION - VENT / SURGE TANK FUEL WATER DRAIN VALVE.. NO LEAK - FUEL VENTILATION OVERPRESSURE DISC ........... INTACT - SURGE TANK AIR INLET............................................. CLEAR - NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION - WINGLET....................................................................... CHECK CONDITION - ANTENNAS ON TOP OF FUSELAGE.......................... CHECK CONDITION



Ch List


11 RH WING TRAILING EDGE : - WING / PANELS............................................................ CHECK CONDITION - STATIC DISCHARGERS............................................... CHECK CONDITION - CONTROL SURFACES................................................ CHECK CONDITION - JETTISON OUTLET ..................................................... NO LEAK (If installed) - FLAPS AND FAIRINGS................................................ CHECK CONDITION - CAMERA LIGHT .......................................................... CHECK CONDITION (If installed)

3

1

4 5

22

7

23 24

8

12 RH LANDING GEAR :

6

21

9 12

18 13

20

10

19

- WING / PANELS............................................................ CHECK CONDITION - CHOCKS....................................................................... IN PLACE - WHEELS AND TIRES................................................... CHECK CONDITION - BRAKES AND BRAKE WEAR INDICATORS.............. CHECK CONDITION - ELEC AND HYDRAULIC LINES / EQUIPMENT........... CHECK - LANDING GEAR / DOORS STRUCTURE.................... CHECK - DOWNLOCK SPRINGS................................................ CHECK CHECK CONDITION :

11

14

13 CENTER FUSELAGE :

17

15

16

NO DAMAGE, NO DENT, NO IMPACT MARK, NO DEFORMATION, NO CRACK, NO FOD PRESENCE, NO MISSING ELEMENT, NO LEAK.

- FUSELAGE / BELLY FAIRINGS................................... CHECK CONDITION - ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED - FUEL DRAIN MAST...................................................... CHECK CONDITION / NO LEAK - MLG DOORS................................................................. CHECK CONDITION


Ch List


14 RH AFT FUSELAGE : 2

3

1

4 5

22

7

23 24

8

6

21

9 12

18 13

20

10

- FUSELAGE / DOORS................................................... CHECK CONDITION - BELLY FAIRINGS......................................................... CHECK CONDITION - SUPPLEMENTAL COOLING AIR INTAKE(S) ..……… CLEAR - RAT DOORS................................................................. CLOSED / CONDITION - SUPPLEMENTAL COOLING AIR OUTLETS ……...... CLEAR / CONDITION - ANTENNAS................................................................... CHECK CONDITION - DRAIN MAST................................................................. CHECK CONDITION - OUTFLOW VALVE........................................................ CHECK CONDITION (Normally wide open. If not, risk of pressurized A/C) - COMPARTMENT AIR EXTRACTION OUTLET............ CHECK CONDITION - BILGE DRAIN HOLES.................................................. NO LEAK - CARGO DOOR ............................................................ CLOSED - ACCESS DOORS (IF NOT REQUIRED)...................... CLOSED - POTABLE WATER SERVICE PANEL.......................... NO LEAK - TOILET SERVICE PANEL............................................ NO LEAK - VACUUM GENERATOR OUTLETS............................. CHECK CONDITION - TAILSTRIKE INDICATORS.......................................... CHECK CONDITION

15 TAIL : 19

11

14

- FUSELAGE / DOORS / PANELS.................................. CHECK CONDITION - STABILIZER, ELEVATOR, FIN AND RUDDER............ CHECK CONDITION - STATIC DISCHARGERS (ELEVATOR AND RUDDER)..................... CHECK - ACCESS DOORS.......................................................... CLOSED


16 APU : 17

15

16

- FUSELAGE................................................................... CHECK CONDITION - APU AIR INTAKE.......................................................... CHECK CONDITION - APU EXHAUST............................................................. CLEAR - NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION - ACCESS DOORS......................................................... CLOSED - DRAIN MASTS............................................................. CHECK CONDITION / NO LEAK


Ch List


17 LH AFT FUSELAGE : - FUSELAGE / DOORS / PANELS.................................. CHECK CONDITION - STABILIZER, ELEVATOR, FIN AND RUDDER............. CHECK CONDITION - BULK DOOR.................................................................. CLOSED - SUPPLEMENTAL COOLING AIR OUTLETS…...…..... CLEAR - DRAIN HOLES............................................................... NO LEAK

3

1

4 5

22

18 LH LANDING GEAR AND FUSELAGE : 7

23 24

8

6

21

9 12

18 13

20

10

19

11

14

17

15

16

- WING / PANELS............................................................ CHECK CONDITION - CHOCKS........................................................................ IN PLACE - WHEELS AND TIRES.................................................... CHECK CONDITION - BRAKES AND BRAKE WEAR INDICATORS.............. CHECK CONDITION - ELEC AND HYDRAULIC LINES / EQUIPMENT........... CHECK - LANDING GEAR / DOORS STRUCTURE.................... CHECK - DOWNLOCK SPRINGS................................................ CHECK

19 LH WING TRAILING EDGE : - WING / PANELS............................................................ CHECK CONDITION - STATIC DISCHARGERS............................................... CHECK CONDITION - CONTROL SURFACES................................................. CHECK CONDITION - JETTISON OUTLET ..................................................... NO LEAK (If installed) - FLAPS AND FAIRINGS................................................. CHECK CONDITION - CAMERA LIGHT ........................................................... CHECK CONDITION (If installed)



Ch List


20 LH WING TIP : - WING / PANELS........................................................... CHECK CONDITION - SLATS 5, 6, 7................................................................ CHECK CONDITION - VENT / SURGE TANK FUEL WATER DRAIN VALVE.. NO LEAK - FUEL VENTILATION OVERPRESSURE DISC ........... INTACT - SURGE TANK AIR INLET............................................. CLEAR - NAVIGATION AND STROBE LIGHTS.......................... CHECK CONDITION - WINGLET...................................................................... CHECK CONDITION - ANTENNAS ON TOP OF FUSELAGE......................... CHECK CONDITION

3

1

4 5

22

7

23 24

8

21 LH WING LEADING EDGE :

6

21

9

- WING / PANELS........................................................... CHECK CONDITION - REFUEL COUPLING DOOR (OPTION)....................... CLOSED - SLATS 2, 3, 4................................................................ CHECK CONDITION

12

18 13

20

10

22 ENG 1 LH SIDE : 19

11

14

- REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION - DRAIN MAST................................................................ CHECK CONDITION / NO LEAK - STARTER VALVE OVERRIDE ACCESS..................... CLOSED - ENGINE ANTI-ICE EXHAUST GRID............................ CHECK CONDITION - ENGINE INLET AND FAN BLADES............................ CHECK CONDITION CHECK CONDITION :

17

15

16

NO DAMAGE, NO DENT, NO IMPACT MARK, NO DEFORMATION, NO CRACK, NO FOD PRESENCE, NO MISSING ELEMENT, NO LEAK.


Ch List


23 ENG 1 RH SIDE : - REVERSERS AND FAN COWLS................................. CLOSED / LATCHED / CHECK CONDITION - AERODYNAMIC STRAKE............................................ CHECK CONDITION - ENGINE OIL FILL ACCESS DOOR.............................. CLOSED - ENGINE VENTILATION EXHAUST GRID.................... CHECK CONDITION - LATCH ACCESS DOORS……………………………..... CLOSED - TURBINE EXHAUST..................................................... CLEAR

3

1

4 5

22

7

23 24

8

24 LH CENTER WING :

6

21

9 12

18 13

20

10

19

11

14

- WING / PANELS............................................................ CHECK CONDITION - IGGS OUTLET............................................................... CHECK CONDITION - SLAT 1………................................................................ CHECK CONDITION - LANDING LIGHT........................................................... CHECK CONDITION - WING FUEL TANK WATER DRAIN VALVE................. NO LEAK


17

15

16


Ch List

NOTE Training by Airbus


Ch List

Training by Airbus

CHECKLIST - COCKPIT OUTSIDE CHECK : - AIRCRAFT WALK AROUND......................................... PERFORM - ADAPTED WHEEL CHOCKS........................................IN PLACE - PAX / CARGO DOOR RED CAB PRESS......................NOT FLASHING

CENTER PEDESTRAL :

Ch List

Page 18

- PARK BRK LEVER....................................................... ON - LDG GEAR GRVTY EXTN SWITCHES........................ OFF / GUARDED - A/SKID SWITCH............................................................ ON - L/G LEVER.................................................................... DOWN - THRUST LEVERS......................................................... IDLE / REVERSE STOWED - ENG MASTER SWITCHES........................................... OFF - ENG START SELECTOR.............................................. NORMAL

- BAT P/B SWITCHES..................................................... ALL OFF / CHECK VOLT ABOVE 23 V - RESET SWITCHES....................................................... CHECK - CKPT EQPT POWER SUPPLY PANELS..................... CHECK - FIRE PUSHBUTTONS (ENG + APU)............................ IN / GUARDED - ALL PRIMS P/B SWITCHES......................................... NORMAL - ALL SECS P/B SWITCHES.......................................... NORMAL - FUEL PUMPS P/B SWITCHES..................................... OFF - CROSS-BLEED VALVE SELECTOR............................ AUTO - OXYGEN CREW SUPPLY P/B SWITCH...................... CHECK OFF - WIPER SELECTORS.................................................... OFF - DITCHING P/B SWITCH............................................... NOT SELECTED - EMER EXIT LT............................................................... OFF - EXT LT........................................................................... OFF - EMER BAT 2 P/B SWITCH........................................... ON - EMER BAT 1 P/B SWITCH........................................... ON - BAT 1 P/B SWITCH...................................................... ON - BAT 2 P/B SWITCH...................................................... ON - CDS (ALL EXCEPT OIS).............................................. ADJUST BRIGHTNESS - ECAM AC and DC ELEC PAGE................................... SELECT / CHECK - ON RMP 1...................................................................... ON / SET FREQ - EXT PWR 2 P/B SW (IF AVAIL ILLUMINATED) .......... ON - EXT PWR 1 P/B SW (IF AVAIL ILLUMINATED)........... ON - GEN P/B SW (ENG + APU)........................................... ON • SCAN ELEC PANEL AND CHECK NO AMBER AND WHITE LIGHTS (EXCEPT AMBER GEN FAULT LIGHT). ECAM AC and DC ELEC PAGE.................................... SELECT / CHECK - COCKPIT LIGHTS........................................................ AS REQUIRED - VENTILATION PANEL.................................................. CHECK NO LIGHTS ILLUMINATED - DISPLAY UNITs............................................................. ADJUST BRIGHTNESS AS REQD - COCKPIT LIGHTING.................................................... AS REQUIRED - ANN LT TEST................................................................. PERFORM - SCAN SEQUENCE........................................................ PERFORM NOTE : DURING THE SCAN SEQUENCE, IT IS A GENERAL RULE TO EXTINGUISH ALL WHITE LIGHTS ON THE OVERHEAD PANEL AND TO SET ALL THE ROTARY SELECTORS TO THE NORM/AUTO (12 O’CLOCK) POSITION - EXT LT SELECTORS.................................................... AS REQUIRED - EMER EXIT LT SELECTOR.......................................... AS REQUIRED - DITCHING P/B SWITCH................................................NOT SELECTED WARNING BE SURE THAT DITCHING PUSHBUTTON IS RELEASED OUT TO PREVENT RISK OF CABIN PRESSURIZATION.

- ECAM CONTROL PANEL............................................. SELECT PRESS • CHECK AVNCS OVBD AND OUTFLOW VALVES OPEN. - RMP 2.............................................................................ON / SET TO INT • CHECK TRANSMISSION AND RECEPTION WITH GROUND CREW.


Training by Airbus

CHECKLIST - COCKPIT

- ECAM CTL PNL (ROTARY KNOB /”ALL” KEY).......... SELECT C/B - FLAPS / SPEED BRAKE LEVER POSITION............... CHECK • IF LEVER DOES NOT AGREE WITH INDICATIONS ON PFD/ ECAM, SET LEVERS TO CORRESPONDING POSITION. - PARK BRK LEVER........................................................ ON • CHECK BRAKES PRESS INDICATIONS. • CHECK ACCUS PRESS INDICATIONS NORMAL (GREEN BAND). IF NOT, PRESS ACCUS REINFLATE P/B SWITCH.

LEAVING THE AIRCRAFT : - ADAPTED WHEEL CHOCK......................................... IN PLACE - EXT PWR....................................................................... ON - APU BLEED P/B SWITCH............................................ OFF - APU................................................................................ OFF - PARK BRK LEVER........................................................ CONFIRM ON • CHECK BRAKES PRESS INDICATIONS. • CHECK ACCUS PRESS INDICATIONS NORMAL (GREEN BAND). IF NOT, PRESS ACCUS REINFLATE P/B SWITCH. NOTE : WAIT 2 MIN FOR ACCUMULATOR RECHARGE CYCLE - TOWING ON BAT P/B SWITCH.................................... OFF - BAT VOLT SELECTOR................................................. OFF - ADIRS MODE ROTARY SELECTORS.......................... OFF - WIPER SELECTORS..................................................... OFF - CREW OXYGEN SUPPLY P/B SWITCH....................... OFF - EXT LT SELECTORS.................................................... OFF - SIGNS AND EMER EXIT LT SELECTOR..................... OFF - CABIN PRESS MODE P/B SWITCHES........................ CONFIRM BOTH IN AUTO - FUEL PUMPS P/B SWITCHES..................................... CONFIRM OFF - CROSSFEED P/B SWITCHES...................................... OFF - CROSS-BLEED VALVE SELECTOR............................ AUTO - DITCHING P/B SWITCH................................................ NOT SELECTED - CDS................................................................................ DIMMED IF NECESSARY - RECORDER GROUND CONTROL............................... NORMAL FLT (NOT ON) - RMP 1, 2 AND 3............................................................. OFF - L/G LEVER.................................................................... DOWN - THRUST LEVERS ......................................................... IDLE / REVERSE STOWED - ENG MASTER SWITCHES........................................... OFF - ENG START SELECTOR.............................................. NORMAL - LDG GEAR GRVTY EXTN SWITCHES........................ OFF / GUARDED - A/SKID SWITCH SWITCH............................................. ON - EXT PWR 1 P/B SWITCH.............................................. OFF (AVAIL) - EXT PWR 2 P/B SWITCH.............................................. OFF (AVAIL) - BAT 2 P/B SWITCH....................................................... OFF - BAT 1 P/B SWITCH....................................................... OFF - EMER BAT 1 P/B SWITCH............................................ OFF - EMER BAT 2 P/B SWITCH............................................ OFF - AIRCRAFT WALK AROUND......................................... PERFORM

Ch List

Page 19


1

2

3

4

5

6

OFF

B SCS

C FMC-A

D FMC-C

E

B

WHC 1

C

FCU

D

PRINTER

E

FQMS 1

OFF

OFF

SEC 3

RESET

OXYGEN

ENG

ON

SVCE INT OVRD

ON

ENG 1

ELEC REMOTE C/B CTL

ON

EMER 2

EMER 1

OFF

CKPT DOOR LOCKG SYS

ISOL

OVHT

SUPPLY

1

2

BAT

APU

1B

OFF

FAULT

APU GEN

COLD

ON

FAULT

ON

OFF

BUS TIE

COCKPIT

A U T O

ON

FAULT

A U T O

ON

FAULT

CKPT

LO

GND COOLG

POWER

ISOL

PAX SYS

265VU

NORM HI

255VM

GND CONNECTION

COM

CHARGE

ON

OFF

FAULT

PUMP

YELLOW

OVHT

SUPPLY

ON

2A

OFF

OFF

FAULT

DRIVE

DISC

TRGT

AUTO

OFF

OFF FF

EMER EXIT LT ON

F I R E

235 VM

H Y D

F U E L

225 VM

E L E C

A I R

ARM

ON

DITCHING

215 VM

ON

RAM AIR

ON

WINDSHIELD DEFOG

FAULT

GEN

AC 2A BUS

OFF

COMMERCIAL 1 2

OFF

STBY

R TK

FAULT

OFF

FAULT

MAIN

ISOL

GALLEY

OFF

FAULT

PACK 2

OFF

OFF

FAULT

ENG 2 BLEED

DN

UP

CABIN V/S

MAN

MODE A U T O

INT LT

BRT

OFF FF F

NO MOBILE ON

SIGNS

AUTO

245VM

HIGH MED LOW

TOWING ON BAT

ON

ENG 2

SQUIB

AGENT 2

ELM

OFF

FAULT

OFF

2B

AC 2B BUS

AVAIL

EXT 2

DRIVE

OFF

FAULT

GEN

DISC

OFF FF

NO PED ON

M DIM

ANN LT TEST

A U T O

CABIN PRESS

OFF

FAULT

ON

FAULT

CABIN

AUTO

HOT AIR 2

COLD HOT H HOT H XBLEED PURS SEL AUTO OPEN

ICE IND

MAN

MODE

CABIN ALT INC

OFF F FF

SEAT BELTS ON

OFF F FF

STBY COMPASS & EYE REF

TRGT

MASTER SW

APU

DEC

APU BLEED CLOSE

ON

PROBE & WINDOW HEAT

AUTO

ON

AVAIL

START

DISCH

SQUIB

FAULT

PUMP

OFF

R

OFF

FAULT

DISCH

AGENT 1

DISCH

SQUIB

ENG 2

AGENT

OFF

AVNCS

FUEL

ON

REFUEL

ISOL

OVHT

SUPPLY

GREEN

END

ON

A U T O

ON

OPEN

CROSSFEED B

APU

ECON MODE

OFF

ON

OPEN

MAN

FAULT

CTR TK FEED

CROSSFEED A

OFF

FAULT

PUMP

YELLOW

FIRE

OVRD

ENG 1

GND HF DATALINK

SQUIB

AGENT 2

DISCH

SQUIB

OFF

FAULT

PUMP

GREEN

OVHT

SUPPLY

ISOL

L

OFF

FAULT

DRIVE

OFF

FAULT

GEN

DISC

2

HI

FAULT

AIR FLOW NORM

ON

FAULT

SIDE 1 & 2 ISOL

FAULT

FAULT

OFF

FAULT

R TK XFR

BAT 2

FAULT

ON

FAULT

OFF

LO

MAN

AC 1B BUS

BAT EMER 1 BAT EMER 2

OFF

AVAIL

EXT 1

ON

FAULT

PACK 1

OFF

HOT AIR 1

OFF

FAULT

1

LOGO ON

OFF FF F

A U T O

L TK XFR

OFF

STBY

L TK

FAULT

1A

OFF

FAULT

DRIVE

DISC

ON

OFF

ON

NAV 1

OFF FF

2

FAULT

ENG

ANTI ICE

FAULT

WING ON

FF OFF

BEACON ON

OFF

FAULT

AUTO

EXT LT

AUTO MODE

CKPT HI VENT

ON

ENG 1 BLEED

FAULT

GEN

AC 1A BUS

OFF

FAULT

BAT 1

OFF

FAULT

MAIN

DISCH

AGENT 1

ON

FADEC GND PWR 1 2

ON

FAULT

F I R E

H Y D

F U E L

E L E C

A I R

WING FAULT

STROBE ON

OFF FF

26.8 88.8 8 8

OVERHEAD PANEL PRESENTATION

231VM

1

2

3

4

5

6

211VM

ATT

221 VM

CIDS 1

EIM 1

F

OFF

OCCPD

LAVATORY

IR2 FAULT

NAV

OFF

ADR2 FAULT

OFF

FAULT

OFF

OFF

IR3

ON BAT

ADIRS

OFF

FAULT

NAV

ADR3 FAULT

OFF

OFF

FAULT

ACTIVE

PRIM 3

ARM

OPEN

ON

RAT MAN ON

A U T O

PURS

CAPT &

RAIN RPLNT

AFT

CALL

EMER

CAPT APT

EVAC

FAST

SLOW

EXIT

CAB REST

HORN OFF

OFF

CREW SUPPLY

A U T O

EMER R ELEC PWR

ON

FUEL JETTISON

F/CTL

ATT

MOBILE COM

OFF

OFF

ATT

PAX INFO

PAX PERS LANDSCAPE CAMERA ELEC SPLY

CABIN

F

Training by Airbus

A VCS 1

RESET

PACK 1

FLAPS 1

ATC

AESU 1

SLATS 1

BSCS 1

SDS 1

LGCIS 1

EMER TR1

OFF

KBD 1

CKPT EQPT POWER SUPPLY

FWS 1

TR 1

AICS 1

CCD 1

A

IR1 FAULT

NAV

OFF

ADR1 FAULT

OFF

FAULT

SEC 1

OFF

FAULT

PRIM 1

ELT ON

RCDR

FAULT

GND CTL

ARMED

EVENT

DFDR

TEST/RESET

ACMS

PAX

OXYGEN

ON

TRIGGER

OFF

WIPER

MID

ALL

CALLS

ON

EVAC

COMMAND

SYS ON

MASK MAN O ON

A U T O

FLT REST

MECH CALL

PURS

FWD

INTMT FAST

INTMT MEDIUM INTMT SLOW

OFF FF

1

2

3

4

5

6

CKPT DOOR CTLR

PACK 2

R

EMER TR2

VCS 2

S

LGCIS 2

SDS 2

FLAPS 2

V

CIDS 2

FQMS 2

W

U

SLATS 2

AESU 2

FMC-B

BSCS 2

EIM 2

KBD 2

T

WHC 2

U

HUMID

V

EFB 3

W

DSCS

RESET

TR 2

FWS 2

T

AICS 2

CINS

S

CVR

ON

OFF

TURB DAMPG

OFF

FAULT

YELLOW ELEC PMP

ERASE

CKPT EQPT POWER SUPPLY

OIS OIS CAB AVNCS & MAINT

CCD 2

R

TEST

OFF

GATELINK

B O O M S E T

CAB DATA TO OIS

OIS

OIS DATA TO AVNCS

OFF

A U T O

GND HYD

OFF

OFF

F/CTL

FAULT

SEC 2

ON

GREEN ELEC PMP

OFF

FAULT

A U T O

OFF

FAULT

PRIM 2

CARGO AIR COND

5

25 25

TEMP REGUL 15

OFF

FAULT

BULK ISOL VALVES

25 25

OFF

FAULT

AFT ISOL VALVES

OFF

FAULT

FWD ISOL VALVES

OFF

TEMP REGUL 15

5

FAULT

HEATER

OFF

CAB FANS

FIRE

FIRE

232VM

1

2

3

4

5

6

222VM

212VM

MLG BAY

OFF

ACTIV

FWD CARGO PRESEL

DISCH

SMOKE

OFF

FAULT

COOLG

FAST

SLOW

OFF

SMOKE

IFEC

OFF

SMOKE

PAX BBAND

CAB SYS SMOKE

A U T O

AGENT TO AFT

CARGO SMOKE AGENT TO FWD

BTL1 BTL1 BTL2 BTL3 BTL2 SMOKE

DISCH

AVNCS EXTRACT

VENT AVNCS SMOKE

A U T O

INTMT SLOW

OFF

WIPER

OVRD

FAULT

ENG

SMOKE

INTMT FAST

ON

MAN START 1 2

ON

RAIN RPLNT

INTMT MEDIUM

Ch List


MAIN INSTRUMENT PANEL & GLARESHIELD PRESENTATION CAPT EFIS CONTROL PANEL

ATC MESSAGE-INDICATOR ATTENTION GETTERS

AUTOLAND LIGHTS

411 VU

TAXI

TAXI

QNH

CSTR

WPT

VORD

NDB

WX

TERR

TRAF

1016 MASTER WARN

LOUDSPEAKER

OFF

LOUDSPEAKER SOUND - LEVEL CONTROL OIS

HUD

NORM

PTT

ATC

AUTO

MSG

LAND

CHRONO

DECLUTTER

SIDESTICK PRIORITY

CAPT

MAX M

XWIND N ND

OFF

in Hg

SPD

MAG

---

HDG

HDG HDG V/SV/S

MASTER CAUT

40 ARC PLAN

LS

IXAT

ALT

TRK TRK FPAFPA

V/S

7000 1000 1000

100 100

CSTR

-----

AP2

20 DN

320

10

SIDE-STICK PRIORITY LIGHTS

A/THR

LOC

640

ZOOM

PERMANENT DATA

SD

ED

ALT

WD

VORD

NDB

WX

TERR

TRAF

ARPT

TAXI

1016 hPa

10 APPR

ZOOM

MASTER WARN

SIDESTICK PRIORITY

NAV

80

ARC

VOR

160

MASTER CAUT

PLAN

LS

320

VV

640

ATC MESSAGE-INDICATOR

ATTENTION GETTERS

412 VU

QNH

in Hg 40

AP1

160

WPT

UP

80

20

VV

METER

--FD

VOR

LS

ARPT

MAG

hPa NAV

BRT BR

TRUE TRUE

MACH SPD SPD

Training by Airbus

F/O EFIS CONTROL PANEL

AFS CONTROL PANEL

CHRONO

HUD

DECLUTTER

OFF

LOUDSPEAKER

NORM

F/O

LS

B BRT

AUTO

ATC

LAND

MSG OFF

IND ND D XWIND

SIDE-STICK PRIORITY LIGHTS

ATC MAIL BOX

PTT

M MAX

LOUDSPEAKER SOUND - LEVEL CONTROL OIS

311 VU 312 VM

LIMIT SPEED (IAS KT)

313 VU

VLO = VLE NORM & GRVTY 250 M 0.55 255 220 212 195 190 186

VFE 1 1+F 2 3 T/O 3 LDG FULL °

140 135

BRK FAN

FLEX

83. 9 % 53°C

5 10 0

EGT °C

692

PACKS

5

THR %

74. 0 78. 1

N1 %

10 0

692

T.O INHIBIT NO SMOKING SEAT BELTS GND SPLRs ARMED

OIS MAP LT

AVNCS

CONSOLE LT

CAPT ON BKUP

AUTO

OIS

A/BRK

MAP LT

L/G

AIR DATA VIEW OFFSIDE

314 VU

140 135

EGT °C

74. 0 78. 1

UP

VIEW OFFSIDE

F/O ON BKUP

INOP

CONSOLE LT

INOP

ON

ON

FMS PEDALS LT ON

BOTH ON 2

NORM

PEDALS LT ON

BOTH ON 1

OFF FF

OFF FF

DOWN

301 VM

SLAT/FLAP LIMITATION MEMO

MODE

ND PFD

MFD

VD

302 VM

LS/

MODE

+

LS/

ND

+

VD MENU

SET/SEL

+53°C

MENU

SET/SEL

DISPLAY CYCLE

CAPT OIS ON CENTER

F/O OIS ON CENTER

DISPLAY CYCLE

AVAIL

INOP

INOP

AVAIL

ON

ON

MFD

SLAT/FLAP LIMITATION MEMO

PFD


Ch List

HF

TEL

SQWK

VHF2

VHF1

123.125 VHF3

TEL1

CALL

2

9

6

3

C/L MENU

NOTE PAD

9

ENT

3

8 +/-

6 7 0

SPACE

KBD

ESC

.

NAV AID

NAV

RST

BRT . .OF OFF

LOAD

VOICE

KBD 1 CCD 1

ON

OFF

CLEAR

RET

1/2

FULL

0 0

ACCU

TEST

1

FIRE

FLX M C T

TO GA

CL

FLX M C T

TO GA

A

L

DN

2

FIRE FAULT

VIDEO

VD AZIM

GAIN

ELEVN

WXR

RCL ALL

EMER CANC

OFF

ON

0

A

IGN START

T H R

NORM

ABN

MORE

F/CTL

STS

PRESS

TA ONLY

SYS 2

SYS 2

UP U

+

R

115 VM

F / O

VIDEO

CL

ENG START

DEFRD

DISPCH

HYD

FUEL

COND

WHEEL

EL/DC

DOOR

BLEED

TCAS

G/S MODE OF FF OFF

WXR

XPDR TCAS

TA

APU

ABV

BLW

SYS 1

SYS 1

PITCH TRIM

LOCK

NORM

UNLOCK

CKPT DOOR

NOSE R

RUDDER TRIM NOSE L

OPEN FAULT

RESET

NOSE UP

NOSE DN

EL/AC

ENG

CRANK

T H R 0

RCL LAST

UP U

+

R

INTEG LT

3.5 PSI 3.5 x1000

VD AZIM

GAIN

ELEVN

WXR

ALL

SD

T.O CONFIG

FAULT

DN

L

YELLOW

1.6

GREEN

STATUS

CKPT LT

FLOOD LT

SLEW

C A P T

Q

/

KBD 2

SQWK

W .

Z

L SPACE

P

ND

VHF2

VHF1 123.450

121.900

7

4

1

8

5

2

9

6

3

RST

ADF 2 1

PA

CLR

ATT

0

CAB

.

INT

MECH

RAD NAV

.

BRT

NAV

.

OIS

NOTE PAD

121.700

DATA

MENU

123.125 VHF3

3

RST

LOAD

BRT . .OF OFF

VOICE

LS 1 R VOR 2 MKR

STBY

DATA SQUAWK: 2523

TEL1

CALL

6

LOAD

OFF OF

VOICE

2 MKR

NAV

ENT

ATC COM

TEL

C/L MENU

HF

ESC

VHF

CLR INFO

A

1 4 7

SPACE

.

KBD

MSG CLR

HF1

CALL

CALL

CALL

CALL

TEL2

VHF1

CALL

HF2

INT

0

D RAD

0

2

1

FLAPS

VHF2

CALL

VHF3

1

3

2

MENU

121.900

SQWK

FULL

3

2

L FULL

3

3

2

TEL

123.450

HF

VHF1

STBY

VHF2

2

DATA

5

9

1

8

ADF 1

PA

7

ATT

CLR

CAB

0

INT

RAD NAV

MECH

.

4

VHF3

121.700

TEL1

CALL

SQUAWK: 2523

DATA

HF1

CALL

CALL

CALL

TEL2

CALL

CALL

HF2

VHF1

VHF2

INT

RAD

1

123.125

VHF

135 VM

CCD 2

CLEAR

MSG CLR

ESC

CENTER PEDESTAL PRESENTATION

MENU

STBY

121.900 123.450

5

PA

ABORT

DOWN

OFF

RESET

ACCU REINFLATE

FULL

1/2

RET

GND SPLRS ARMED

LS 1 R VOR 2 MKR

DATA

1

8

ATT

CLR

4

CAB

0

INT

ADF 2 1

ON

SPEED BRAKE

RAD NAV

MECH

.

7

VHF 1 RECEPTION NOT SELECTED

DATA

121.700

VHF

Training by Airbus

MSG CLR

HF1

CALL

CALL

CALL

CALL

TEL2

VHF1

CALL

HF2

D RAD

INT

VHF2

CALL

VHF3

OFF

PARK BRK

PULL & TURN L/G GRVTY EXTN

0123456789

CALL

VHF3

Ch List


EXTERNAL PANELS

FORWARD, NOSE FUSELAGE & CENTER FUSELAGE Training by Airbus

NOTE CENTER FUSELAGE

132BR 132AR 122AR

FORWARD & NOSE FUSELAGE

141AZ

142AZ


Ext Pa

AFT BOTTOM & AFT RIGHT Training by Airbus 152BR 152AR

171AL

NOTE

AFT BOTTOM

164AR

FWD

AFT RIGHT

152BR

FWD

152BR


Ext Pa

BELLY FAIRING REAR 199

Training by Airbus

198VR

198RR

198UR

199BR

198CR

197MB

198AB

197RB 2L

197BB

197KB 197JB

197QB 197NB

197FB

197SB

198AR

198EB

198GB 199AB

198CR

198GR 198HB

198PB

FWD

NOTE

198YR

198QR 198PR 198NR 198SR 198MR 198LR

2R

197

198HR

198TR 199AR

198ER

198JR

198KR

198

197LB

197DB

197AB 197CB

197AL

197ML 197GL

199AL

197KL

197QL 197NL

197HL

197PL

197LL

197JL

197RL 197EL 197CL

197BL Page 25

FR69 FR65

FR61

FR54


Ext Pa

BELLY FAIRING FRONT Training by Airbus 191

194

192

NOTE

194MR

193JR

194KR

194KB 194JB

194HR

194DB

194FB 193QB

193XB 193LL 193ML 193NL

194CR

193TB

194BR

191AB

2R

193AB 193FB

191BB

193BB

193KB 193HB

193LB 193MB

193GL

193KL

2L 191BL

193AL

193CL 193EL

193EB

193GB

193JL 193FL

193DB

193DL

191AL

193BL

FWD

193PL FR54

192AR

193CB

194CB

193UB

193HL

192BR

194AB

193JB 193PB

194DR

194AR

194BB

193SB 193RB

193WB

194FR

194ER

194GB

194HB 193VB

194GR

194LR

194EB

194NR

193NB

194QR 194PR

193

FR49

FR42


Ext Pa

BELLY FAIRING LEFT - REAR & FRONT Training by Airbus FR54

FR61 195DT

195

FR65

197

NOTE

FR69 195ET

195FT

197BT

195GT 197ET

197CT

197DT

197AT

197DL

BELLY FAIRING LEFT - REAR

197SL 197CL

197FL

197LL

197PL

199AL

197JL

FWD

195 191 FR49

FR42

191BT AT 191

195AT

195BT

FR54 195CT

191CL

BELLY FAIRING LEFT - FRONT

FWD


Ext Pa

BELLY FAIRING DETAIL A Training by Airbus OPTION A : EXTRA SCS ON RH WITH CDM PLUS 1 OR 2 VCRU

NOTE

198XR

198ZR

198AS

198RR 198WR

198FR

FWD

OPTION B : EXTRA SCS ON RH WITH ONLY A CDM 198XR 198ZR Page 28 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

BELLY FAIRING RIGHT - BACK & FRONT Training by Airbus 198

196

FR65

FR61

FR69

198FT

198ET

198BT 198DT

BELLY FAIRING RIGHT - BACK

199AR

NOTE

198CT

198UR

198RR

198VR

198KR

196ET

196FT 198GT 196GT

198AT

199BR

FR54 196DT

198DR 198FR

198CR

198JR

FWD

FR54

192BT

FR49 196CT

196BT

196AT

196 FR42

19 2

192

AT

192CR

BELLY FAIRING RIGHT - FRONT

FWD


Ext Pa

VTP LH & VTP RH Training by Airbus 324AT

32

5F 32

L 2C

EL

32

5D

L 2B

32

5D

R

2B L

5E

L 3 25

32

32

L

R

2C

5F

32

32

32

R

322DL

326AT

NOTE

5G

L 3 25

326AT

32

GL

324AT

32

L 2A

5B

L

32

32

L 323DR

323ER 323CR

323BL 323CL

VTP LH

R

323EL

5B

325AR

2A

2 R3

325AL

32

5C

323AL

FWD

32

5C

L

R

323DL

321AL

FWD

321AL

323AR 323BR

VTP RH Page 30 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

HTP TOP & HTP BOTTOM 34

4E

33

T 34

4D

34 1E T

T

Logo light 34 4C T 34 344AT 4B T

34 1D T

F W D

Logo light

33 334AT BT 4 33

4C

343AT

34 1B T

333AT

33

T 1B

33

33

NOTE

T 1E

T 1D

HTP BOTTOM

T 1C

332AT

342AT 334EB

331AT

341AT

T

DT

T

33 34 1C T

4 33

4E

332AT

342AT

Training by Airbus

33 332AB

33

344EB

4D

B

1E T 33

HTP TOP

33

1D T

4C

B

33

33

1C T

4B

33

B3

34

AB

333AB

1B T

331AT

34

B 4A

34

4

BB

343AB

T 1B 34

34

4

CB

T 1C 34

34

4D

B

T 1E 342AB 34

T 1D 34

341AT

F W D Page 31 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

HTP LEFT & HTP RIGHT Training by Airbus

NOTE

HTP LEFT

HTP RIGHT FWD

FWD

333AT

343AT

333AB

343AB


Ext Pa

HTP RIGHT & LEFT ELEVATOR Training by Airbus

NOTE HTP RIGHT ELEVATOR

345CB

345AB

345BB

345DB

345EB 345FB

F W D

HTP LEFT ELEVATOR

F W D 335AB

335BB

335CB

335DB 335EB 335FB


Ext Pa

S19 Training by Airbus

S19 TOP

NOTE

S19 LEFT

311BL 317AB

317AB 315AL

317BB 311AL FWD

FWD

S19 RIGHT

S19 BOTTOM 316BR

317AB

317AB

312BR

311BB 316AR

314AR 316AR

315AL 312AR

311AB 314AR

FWD

FWD


Ext Pa

PYLON 1 OUTBOARD & INBOARD Training by Airbus

PYLON 1 OUTBOARD

455CL 455BL

4 52

AL

L 4 5 3B

PYLON 1 INBOARD

45

4 5 5DL 4 5 5EL 4 5 5A L 4 5 3FL 4 5 3EL 4 5 3GL 3 DL

45

5F

L

4 59A L

455

4 5 5 JL

55 4 5 5HL 4

4 5 5L KL

L

ML 455

PL

NOTE

L

455RL

455QL 455NL 459CL

459BL 4 5 5GL

455JR SL

455

S 455

455 PR

455DL 455ER

455CL

455M R

455QR 455NR

455LR 455FR 455 KR 455H R

4 5 5 BL

4 5 3 BR

4 5 3A R

4 5 2 BR

4 52 A L

459AR

Page 35

455GR © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

PYLON 2 OUTBOARD & INBOARD Training by Airbus

PR

4 6 5M

465QR

R 4 65LR

465JR

465K R

465NR

5F

465

R

PYLON 2 OUTBOARD SL

46

465

465CR 4 6 5DR 4 6 5ER 4 6 5 BR 4 6 3ER 4 6 3 F R 4 6 3 DR

4 6 3 BR

469AR

469CR 469BR

465HR

4 62 AL

463CR

465GR

465DR

PYLON 2 INBOARD

465BR

465EL

465CR

L 4 6 5M L 4 6 5 J L 4 6 5L L F 5 3 EL 4 6 3 F L 4 6 4 6 5K L 4 6 3 DL 4 6

465

4 6 5A L

4 62 A

L

NOTE

4 6 3B

L

PL

465

SL

465RL 465QL

465NL 469AL

465HL

465GL


Ext Pa

ENGINE 1 INBOARD & OUTBOARD Training by Airbus

ENGINE 1 INBOARD

ENGINE 1 OUTBOARD

NOTE

417FR

417FL

417DR

417DL

417AR

417GR

417CL

417AL 417GL

41 5A 41 7C

417ER 417QR

R

41 5A

415CL

L

417EL

R 5A 41 415CL

7C 41

R 5A 41

417RR

L

417QL

L

417RL 417BR

417BL 415BR


Ext Pa

ENGINE BOTTOM 417KL

417SL

Training by Airbus 417ML 417PL

ENGINE 1 BOTTOM

415AL

NOTE

417NL

411AL

417CL 417HL 417HR

415BL

417CR 415AR

417NR 417PR

417JL

417SR 417SR

417LL

427SR

427KL

427ML

427PR

ENGINE 2 BOTTOM

425AR

427NR

421AL

427CR 427HR 427HL

425BL

427CL 425AL

427NL 427PL

Page 38 427LL

427SL

427JL


Ext Pa

ENGINE 2 OUTBOARD & INBOARD Training by Airbus

ENGINE 2 INBOARD

ENGINE 2 OUTBOARD

427FR

NOTE

427FL

427DR

427DL

427AR

427AL

427CL

427GL

427GR 42

7C

42

R

42

427ER

5A

4 2 5 CL

5A

L

R 5A 42 4 2 5 CL

R

427QR 427RR

4 427BR

A 25

L

4

C 27

427EL

L

427QL 427RL

427BL 425BR


Ext Pa

LEFT WING TOP Training by Airbus

NOTE RIB1 522AT

F W D

RIB11

572CT

572BT

572AT

RIB23

534BB 534GB

534FB

5 81 AT

T

T

1C

534AT

571BT

57

534BT

57 1 581HT 581GT 581FT 581ET 581DT DT 5 81 CT 5 81 B

57 1 AT

534JB


Ext Pa

LEFT WING BOTTOM IN & OUT Training by Airbus 523FB

LEFT WING BOTTOM IN

LEFT WING BOTTOM OUT RIB18

52

521AB 521BB

F W D

511AB

3G

NOTE RIB20

B 52

3H

RIB22 F 5 RIB24 542MB 23J 542KB W B 521JB D 54 3 A 52 3 RIB26 51 572EB RIB4 B 1 KB 542NB BB 52 5 57 2 43 1D FB CB 5 2 3 511EB 542PB B 5 511C RIB28 L 5 RIB6 21 521KB 7 2G 5 EB B 51 54 B 5 4 511AZ B 3B 523NB 3 1D EB 2 3M B B 57 3 B RIB8 RIB30 5 A B 4 3D 54 B 523PB 3 521FB 5 GB 523QB 57 3 4 572HB 541AB 521GB BB 3 F B 534GB 591AB RIB11 1 522AB 534FB 541BB 591EB 550AB 52 57 3 572CT 523CB 3 C 541CB AB B RIB33 550BB 591CB 591DB 541DB 57 3 52 RIB14 591FB 550CB 534BB 3 DB 541EB BB 542CB 523EB B 591GB 542AB 571BB 52 RIB16 3D 542BB 591HB 591KB 542EB B 571EB 571MB 591LB 591MB 542DB 591JB 542FB 571FB 571AB 534HB 571GB 534JB 572AB 542GB 571CB 571JB RIB2

542JB

57 2

571LB

571DB 571HB

571KB

572BB

542LB

CB

57 2

DB

B

542HB Page 41 572EB


Ext Pa

LEFT WING BOTTOM INSIDE Training by Airbus RIB7

542BZ

542AZ

NOTE

541AZ 541CZ 541BZ

515AZ


Ext Pa

LEFT WING FAIRING IN & OUT Training by Airbus 531CR

531AR

531BR

531BB

NOTE

531AB 532AR

531DB

531AT

532BB

531CB

532AB

531EB 532AT

532CB

532DB

533AR

532CR

532EB

533BR 533AB

533AT 533EB

LEFT WING FAIRING IN

532BR

533BB

533DB 533CR

533CB

533AL

532BL 532AL

LEFT WING FAIRING OUT

533DL 533BL 533CL

533EB

533AB 532AB

533AT

533DB

533EL

532DB

532CL

532DL

532AT 532EB 532EL 531AT

531BL 531AL

531AB

531DB

531EB 531DL

531CL


Ext Pa

RIGHT WING TOP Training by Airbus

NOTE RIB1 622AT RIB11 RIB23

634GB 672AT

672BT

634BB

672CT

634JB

634FB AT 6 71

681FT 681DT DT 671 81CT 6 T BT 1C 681ET 681GT 6 81 67 T A 6 81

671BT

681HT

634AT

634BT


Ext Pa

RIGHT WING BOTTOM OUT & IN Training by Airbus RIB18 RIB20

RIGHT WING BOTTOM OUT

623FB GB

NOTE

3 62 642KB

B 642JB 3H 62 642LB 621BB 621AB RIB24 JB B 611AB 3 N 62 42 B 6 B RIB26 A RIB2 43 642MB 3K 672EB F 62 B 6 611BB FB W 3B B RIB4 PB RIB28 672 3L 6 4 6 42 D 62 B B G B 2 611DB B C 1D 67 621JB 1C EB 62 MB 643DB 643 RIB6 1 3 6 611AZ 621KB RIB30 62 21 AB 643EB 611EB 6 3 672HB 7 6 NB 643FB RIB8 641AB 23 B 6 B 691AB 3 B 643GB 634GB 7 621FB P 6 634FB 23 641BB 672CT 621GB B 6 650AB 3CB RIB11 691DB Q 623CB RIB1 7 3 650BB RIB33 6 B 2 691FB 641CB 6 622AB 691CB 3A 691EB 641DB 62 634BB 650CB 3DB 691GB RIB14 B 671MB 67 641EB 691HB 3B 634JB 62 691KB 691JB 642AB RIB16 RIB1 16 671BB B 642CB 691LB 634HB 3D 642BB 671DB 62 642E 2EB 642EB 691MB 623EB 642DB 671FB 671AB 671GB 672AB 671CB 642HB 642FB RIGHT WING BOTTOM IN 671JB

RIB22

642GB

F W D

67

2 DB

67 2

672KB

CB

671HB

671LB Page 45

672BB

671EB © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

RIGHT WING FAIRING IN & OUT Training by Airbus 631AL 631BL

631BB

631AB 632AL 632BB

631CB

631EB 632CL

632DB

633AL

63

632EB

633BL

3A

RIGHT WING FAIRING IN

632AT

632CB 633BB

NOTE 631AT

631DB

632BL

632AB

631CL

633CL

B

633AT 633DB

633CB 633EB 633DR 6 633BR

633AT 633EB

RIGHT WING FAIRING OUT

633CR 633ER

632AT 632EB 632ER 631EB

633DB

633AR

633AB

632DB 632AB 632DR 632CR 631BR 631DB

631AT 631DR 631CR

632BR 632AR

631AR

631AB Page 46 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

Ext Pa

RIGHT WING BOTTOM INSIDE Training by Airbus 642BZ

RIB7

642AZ

NOTE

641AZ

641CZ

641BZ

615AZ


Ext Pa

FORWARD, NOSE & AFT FUSELAGE Training by Airbus

NOTE

FORWARD & NOSE FUSELAGE

821BR

821AR

AFT FUSELAGE

Page 48 822BR 822AR


Ext Pa

COMPUTER & C/B LOCATIONS LOCATIONS OF C/B PANELS Training by Airbus

NOTE NORMAL ACCESS TO C/B MANAGEMENT

BACKUP ACCESS TO C/B MANAGEMENT

NOTE: FOR C/B STATUS SELECTION PAGE,SEE SHEET 2


CO & C/B

LOCATIONS OF C/B PANELS Training by Airbus

NOTE C/B STATUS SELECTION PAGE

NOTE: FOR LOCATION ON PANEL, SEE SHEET 2


CO & C/B


C/B STATUS SELECTION PAGE

NOTE

FACE Page 51 NOTE : FOR LOCATION ON PANEL, SEE SHEET 2

POWER CENTER

ZONE

MATRIX


CO & C/B


NOTE EPDC1 FACE 1

EPDC1 FACE 3

A B

E

A

D

D

01 03 05 02 04 06 A B C D E F G

C

B

FWD

C MATRIX

NOTE : MECHANICAL CIRCUIT BREAKERS ARE ON ZONES 1C, 1D, 1F, 1G, 1I AND 1J

FOR DETAIL E, MECHANICAL CIRCUIT BREAKERS ARE ZONES 3H, 3I AND 3K FWD

E


CO & C/B


NOTE EPDC2 FACE 2

EPDC2 FACE 4

F

G

J

F

H H

G

FWD

FOR DETAIL G, MECHANICAL CIRCUIT BREAKERS ARE ZONES 2C, 2D, 2F, 2I AND 2J

J

FWD

Page 53 NOTE: MECHANICAL CIRCUIT BREAKERS ARE ZONES 4H, 4I AND 4K © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

CO & C/B

COMPUTERS LOCATION BY VU - 1000 VU Training by Airbus

NOTE GCU 1B 2XU1

VOR 1 1RS1

SCI 1 1TL1

CIDS 1 100RH1

CIDS 2 100RH2

SCI 2 1TL2

1011VU

GCU VOR 2 2B 1RS2 2XU2

1000 VU

1012 VU FWD IMCC-OSFC 2TC

IMCC-ASFC 1TC

1021 VU

1051 VU

ADF 1 1RP1

ADF 2 1RP2

CRDC A08

1TS06 CRDC A06

1TS08 OPU 2B 102XU2

AESU 1 1SE1

1042 VU OPU 1B 102XU1

DME 1 1SD1

CRDC A09

CRDC A05

1041 VU

1TS09

FMC C 1CC3

1TS05

PRIM 3 1CE3

SW 9 1TH 09

1031 VU

1TS03 CRDC A03

SEC 3 2CE3

SW19 1 TH 19

AECM A 18GF1

1022 VU

1052VU Page 54 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

CO & C/B


RBCU 1 10GL1

SW FMC A 13 1CC1 1TH 13

SW CPIOM CPIOM CPIOM 15 GCU 1A H63 H61 J51 1TH 8TF63 8TF61 9TF51 15 1XU1

1100 VU

NOTE

1111VU SW CPIOM CPIOM CPIOM CPIOM 11 J23 H33 H41 J11 1TH 9TF11 9TF23 8TF33 8TF41 11

BOMU CPIOM QAR H31 1 SPARE 14HA1 8TF31

FWD

1121VU CDAU 2TU

CPIOM CPIOM J71 H43 8TF43 9TF71

SEC 1 2CE1

CMV 1 1TE1

1131VU SDU 5RV1

SW 5 1TH 05

SW 3 CPIOM 1TH J21 03 9TF21

SW 1 OPU 1A 1TH 101XU1 01

PRIM 1 1CE1

1141VU AMU 1 1RN1

RA 1 MVDR 1 1SA1 1RC1

MMR 1 40RT1

SFCC 1 2CV1

HFDR 1 1RE1


CO & C/B


CPIOM H44 8TF44

RBCU 2 10GL2


AECM B 18GF2

GCU EMER 2XE

OPU 2A 101XU2

NOTE

1212VU BOMU SW CPIOM 16 FMC B 2 1TH H 32 14HA2 16 8TF32 1CC2

1200 VU


GCU 2A 1XU2

FWD

1222VU SEC 2 2CE2

SW CPIOM 4 J72 1TH 9TF72 04

SW 2 1TH 02

CMV 2 1TE2

SW CPIOM 6 H42 1TH 8TF42 06

1232VU PRIM 2 1CE2

SW CPIOM 12 J22 1TH 9TF22 12

AESU 2 1SE2

SFCC 2 2CV2

1242VU HFDR 2 1RE2

CPIOM MMR 2 H64 40RT2 8TF64

DME 2 1SD2

CPIOM SW MVDR 2 14 J24 1TH 1RC2 9TF24 14

AMU 2 1RN2


CO & C/B

PHYSICAL C/B LOCATION BY ATA Training by Airbus

DEVICE FIN

PROTECTION DEVICE DESIGNATION

FROM EQUIPMENT

PHYSICAL LOCATION

215200

3101HH

C/B-ASCU1 NORM

EPDC1

1FD07

215200 227700

3102HH

C/B-ASCU2 NORM

EPDC2

2FC05

3201CC

C/B-FMC-A

CBP1

5AH03

227700 227700

3102CC

C/B-FMC-B

EPDC2

2KM04

3101CC

C/B-FMC-C

EPDC1

1KL02

228100

3201CB

C/B-FCU CHAN1

CBP1

5AC11

228100 231100

3102CB

C/B-FCU CHAN2

EPDC2

2KJ01

3101RE

C/B-XCVR HFDR1

EPDC1

1JA07

231100

3102RE

C/B-XCVR HFDR2

EPDC2

2JA02

231200

3102RC

C/B-XCVR MVDR2

EPDC2

2KP03

231200

3202RC

C/B-XCVR MVDR2 EMER

CBP2

6AB01

232800

3101RV

C/B-SATCOM1

EPDC1

1JA06

235000

3201RN

C/B-AMU1 & RMP1

CBP1

5AD07

235000

3105RN

C/B-AMU1 & RMP1 BKUP SPLY

EPDC1

1KN01

235000 235000

3102RN

C/B-AMU2

EPDC2

2KN03

3202RN

C/B-AMU2 & RMP2

CBP2

6AF01

235300

3101WC

C/B-MECH CALL HORN

EPDC1

3AF02

237100

3203RK

C/B-CVR CTL

CBP1

5AD03

237100

3202RK

C/B-CVR SPLY

CBP2

6AE13

237500

3101RM

C/B-TAC BELLY

EPDC1

1FC01

TO ATA

PHYSICAL LOCATION

TO ATA

DEVICE FIN


FROM EQUIPMENT

237500 242200 242200

3104RM

C/B-TAC VERT STAB

EPDC2

2FC08

3201XU

C/B-GCU1A

CBP1

5AC09

3201XU

C/B-GCU1A

CBP1

5AH11

C/B-GCU1B

CBP1

5AC10

242200

3203XU 3203XU

C/B-GCU1B

CBP1

5AJ15

242200 242200

3202XU 3204XU

C/B-GCU2A

CBP2

6AB08

C/B-GCU2B

CBP2

6AE05

242200 242200

3204XU 3209XU

C/B-GCU2B

CBP2

6AJ06

C/B-OPU1A BKUP

CBP1

5AJ06

242200 242200 242200

3105XU 3211XU 3107XU

C/B-OPU1A POR

EPDC1

1GA01

C/B-OPU1B BKUP C/B-OPU1B POR

CBP1 EPDC1

5AJ07 1DA03

242200

3210XU

C/B-OPU2A BKUP

CBP2

6AK09

242200 242200

3106XU 3212XU

C/B-OPU2A POR

EPDC2

2GA02

242200 242200

3108XU 3205XU

242200

3205XU 3101XU

C/B-VFG1A DISC

CBP1

5AH07

242200

C/B-VFG1A POR

EPDC1

1GA02

242200

3207XU

C/B-VFG1B DISC

CBP1

5AC15

242200

C/B-OPU2B BKUP

CBP2

6AJ14

C/B-OPU2B POR

EPDC2

2DA01

C/B-VFG1A DISC

CBP1

5AC14


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

242200

3207XU

C/B-VFG1B DISC

CBP1

5AJ11

242200 242200

3103XU

C/B-VFG1B POR

EPDC1

1DA02

3206XU

C/B-VFG2A DISC

CBP2

6AB04

242200

3102XU

C/B-VFG2A POR

EPDC2

2GA01

242200

3208XU

C/B-VFG2B DISC

CBP2

6AE04

242200 242200 242400

3208XU

C/B-VFG2B DISC

CBP2

6AK06

3104XU

C/B-VFG2B POR

EPDC2

2DA02

3202XE

C/B-RAT POR

EPDC2

4GB03

242400

3208XE

C/B-RAT POR 1

EPDC2

4GA01

242400

3210XE

C/B-RAT POR 2

EPDC2

4GA02

242400 242400

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

243400 243400

3203PE

C/B-EMER TR1 POM

EPDC1

3HZ15

3200PE

C/B-EMER TR2 BKUP

EPDC2

4HJ05

243400 243600 243600

3202PE

C/B-EMER TR2 POM

EPDC2

4HZ14

1001PM 1002PM

C/B-701PM C/B-702PM

EPDC1 EPDC2

1KZ02 2KZ02

243600 243600

3103PM

C/B-BAT1 VOLTAGE IND

EPDC1

3AE01

3102PM

C/B-BAT2 VOLTAGE IND

EPDC2

4AF04

243600 243600

3105PM

C/B-BMU1

EPDC1

3AG05

3104PM

C/B-BMU2

EPDC2

4AG07

2003PB

C/B-703PB

EPDC1

3HZ08

3212XE

C/B-RAT POR 3

EPDC2

4GA03

3201XE

C/B-RAT SOL AUTO

EPDC1

3HH01

243800 243800

2004PB

C/B-704PB

EPDC2

4HZ08

3203PB

C/B-EMER BAT1 VOLTAGE IND

EPDC1

3HK02

242400 242800 242800

3200XE

C/B-RAT SOL AUTO MANUAL

EPDC2

4HK05

243800

2001XB

C/B-STATIC INVERTER 1

EPDC1

3HZ09

243800

3202PB

C/B-EMER BAT2 VOLTAGE IND

EPDC2

4HH02

2002XB

C/B-STATIC INVERTER 2

EPDC2

4HZ09

3205PB

C/B-EMER BMU1

EPDC1

3HJ04

243200 243200

3101PU

C/B-TR1 BKUP

EPDC1

3AG02

243800 243800

3204PB

C/B-EMER BMU2

EPDC2

4HK04

3103PU

C/B-TR1 POM

EPDC1

1KZ01

3101XG

C/B-EXT PWR1 AVAIL

EPDC1

1KJ03

243200 243200

3100PU

C/B-TR2 BKUP

EPDC2

4AE04

244100 244100

3103XG

C/B-EXT PWR1 NOT IN USE

EPDC1

1KJ04

3102PU

C/B-TR2 POM

EPDC2

2KZ01

244100

3102XG

C/B-EXT PWR2 AVAIL

EPDC2

2KH04

243400

3201PE

C/B-EMER TR1 BKUP

EPDC1

3HK04

244100

3104XG

C/B-EXT PWR2 NOT IN USE

EPDC2

2KH03


CO & C/B

Training by Airbus

FROM EQUIPMENT

PHYSICAL LOCATION

C/B-ATUC1A

EPDC1

C/B-ATUC1B

EPDC1

C/B-ATUC2A

EPDC2

TO ATA

DEVICE FIN


245100

3101XN

245100 245100 245100

3103XN 3102XN 3104XN

C/B-ATUC2B

EPDC2

4AE02

245100 245100

3105XN

C/B-ATULC1A

EPDC1

3AE06

3107XN

C/B-ATULC1B

EPDC1

3AG06

245100 245100

3106XN

C/B-ATULC2A

EPDC2

4AG02

3108XN

C/B-ATULC2B

EPDC2

4AG01

245200

1001XP

C/B-101XP

EPDC1

1JZ02

245200 245200

3AG07

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

3AE07

245500

3292XD

C/B-492XD

EPDC2

2CZ01

4AE01

245700 246100

3102XF

C/B-CFFC

EPDC2

2FD07

1001PN

C/B-101PN

EPDC1

1KZ03

246100 246100

1003PN

C/B-103PN

EPDC1

1KZ04

1011PN

C/B-111PN

EPDC1

1KZ13

246100 246100 246100

1013PN

C/B-113PN

EPDC1

1KZ14

1071PN

C/B-171PN

EPDC1

1KZ15

1002PN

C/B-202PN

EPDC2

2KZ03

1004PN

C/B-204PN

EPDC2

2KZ04

1003XP

C/B-103XP

EPDC1

1JZ03

1005XP

C/B-105XP

EPDC1

1FZ01

246100 246100

1012PN

C/B-212PN

EPDC2

2KZ12

1014PN

C/B-214PN

EPDC2

2KZ13

245200

1007XP

C/B-107XP

EPDC1

1FZ04

246100

245200 245200

1051XP

C/B-151XP

EPDC1

1JZ01

246100

1072PN

C/B-272PN

EPDC2

2KZ14

1002XP

C/B-202XP

EPDC2

2JZ02

246100

1111PN

C/B-311PH NORM

EPDC1

1KZ05

245200 245200

1004XP

C/B-204XP

EPDC2

2JZ03

246100

1112PN

C/B-412PH NORM

EPDC2

2KZ05

1006XP

C/B-206XP

EPDC2

2FZ01

2001PH

C/B-301PH

EPDC1

3HZ12

245200

1008XP

C/B-208XP

EPDC2

2FZ04

246400 246400

2003PH

C/B-303PH

EPDC1

3HZ13

245200

C/B-252XP C/B-301XD

EPDC2 EPDC1

2JZ01 1CZ02

246400 246400

2005PH

C/B-305PH

EPDC1

3HZ14

245500

1052XP 2001XD

245500

3291XD

C/B-391XD

EPDC1

1CZ01

245500

2002XD

C/B-402XD

EPDC2

2CZ02

246400 246400

2011PH 2071PH 2073PH

C/B-311PH EMER C/B-371PH C/B-373PH

EPDC1 EPDC1 EPDC1

3HZ05 3HD01 3HZ07


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

245500

2002PH

C/B-402PH

EPDC2

4HZ13

245500 245500

2004PH

C/B-404PH

EPDC2

4HZ11

2006PH

C/B-406PH

EPDC2

4HZ12

245500

2012PH

C/B-412PH EMER

EPDC2

4HZ05

245500 245500

2072PH

C/B-472PH

EPDC2

2074PH

C/B-474PH

247100

3205XZ

C/B-EPU1A

247100 247100

3207XZ 3206XZ

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

247100 247100

3103XZ

C/B-SRPU 2A&2B AC1B SPLY

EPDC1

1KJ01

3202XZ

C/B-SRPU 2A&2B EMER2 SPLY

EPDC2

4HZ01

1016XZ

C/B-SRPU 2A&2B NORM2 SPLY

EPDC2

2KZ06

4HD05

247100 247100

3102XZ

C/B-SRPU1A DC2 SPLY

EPDC2

2KZ10

EPDC2

4HZ07

247100

3101XZ

C/B-SRPU2B DC1 SPLY

EPDC1

1KZ11

EPDC1

3HZ03

247100

3111XZ

C/B-TR1 INPUT NORM1

EPDC1

1HB08

C/B-EPU1B

EPDC1

3HZ04

247100

3112XZ

C/B-TR1 INPUT NORM2

EPDC2

2HB08

C/B-EPU2A

EPDC2

4HZ03

1017XZ

C/B-TR1 OUTPUT A NORM1

EPDC1

1HB01

247100

3208XZ

C/B-EPU2B

EPDC2

4HZ04

247100 247100

1018XZ

C/B-TR1 OUTPUT A NORM2

EPDC2

2HB01

247100

3107XZ

C/B-RCCB 115V NORM1 SPLY

EPDC1

1KZ07

247100

3113XZ

C/B-TR1 OUTPUT B NORM1

EPDC1

1HB02

247100

3108XZ


EPDC2

2KZ07

247100

3114XZ

C/B-TR1 OUTPUT B NORM2

EPDC2

2HB02

3115XZ

C/B-TR1 OUTPUT C NORM1

EPDC1

1HB03

247100

3203XZ

C/B-RCCB 230V EMER1 SPLY

EPDC1

3HZ02

247100

247100

3204XZ

C/B-RCCB 230V EMER2 SPLY

EPDC2

4HZ02

247100

3116XZ

C/B-TR1 OUTPUT C NORM2

EPDC2

2HB03

247100

3105XZ


EPDC1

1KZ08

3117XZ

C/B-TR1 OUTPUT D NORM1

EPDC1

1HB04

3118XZ

C/B-TR1 OUTPUT D NORM2

EPDC2

2HB04

247100

3106XZ


EPDC2

2KZ09

247100 247100

247100 247100 247100

3109XZ


EPDC1

1KZ09

247100

3119XZ

C/B-TR1 OUTPUT E NORM1

EPDC1

1HB05

3110XZ 3104XZ

C/B-RCCB 28V NORM2 SPLY C/B-SRPU 1A&1B AC2B SPLY

EPDC2 EPDC2

2KZ08 2KH06

247100 247100

3120XZ

C/B-TR1 OUTPUT E NORM2

EPDC2

2HB05

3121XZ

C/B-TR1 OUTPUT F NORM1

EPDC1

1HB06

247100

3201XZ

C/B-SRPU 1A&1B EMER1 SPLY

EPDC1

3HZ01

247100

3122XZ

C/B-TR1 OUTPUT F NORM2

EPDC2

2HB06

247100

1015XZ

C/B-SRPU 1A&1B NORM1 SPLY

EPDC1

1KZ06

247100

3123XZ

C/B-TR1 OUTPUT G NORM1

EPDC1

1HB07


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

247100

3124XZ

C/B-TR1 OUTPUT G NORM2

EPDC2

247100

3209XZ

C/B-TR2 INPUT EMER1

EPDC1

247100

3218XZ

C/B-TR2 INPUT EMER2

247100

3211XZ

247100 247100

3220XZ 3213XZ

C/B-TR2 OUTPUT B EMER1

EPDC1

247100

3222XZ

C/B-TR2 OUTPUT B EMER2

EPDC2

PHYSICAL LOCATION

2HB07

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

3HM04

256200

3103MJ

C/B-ASPSU GPU1

EPDC1

1JB07

EPDC2

4HM04

C/B-TR2 OUTPUT A EMER1

EPDC1

3HM01

256200 261100

3104MJ 3201WP

C/B-ASPSU GPU2 C/B-CM/A MLG BAY

EPDC2 CBP1

2JB01 5AA04

C/B-TR2 OUTPUT A EMER2

EPDC2

4HM01

3202WP

C/B-CM/B MLG BAY

CBP2

6AA15

3HM02

261100 261200

3211WD

C/B-CM/A ENG1

CBP1

5AA05

4HM02

261200

3121WD

C/B-CM/A ENG2

EPDC1

1KC01

3112WD

C/B-CM/B ENG1

EPDC2

2KQ05 6AA14

247100

3215XZ

C/B-TR2 OUTPUT C EMER1

EPDC1

3HM03

261200

247100

3224XZ

C/B-TR2 OUTPUT C EMER2

EPDC2

4HM03

3222WD

C/B-CM/B ENG2

CBP2

247100 247100

3210XZ

C/B-TR2 RAT INPUT

EPDC2

4HN04

261200 262100

3211WE

C/B-FIRE BTL1/A ENG1

EPDC1

3HJ02

3212XZ

C/B-TR2 RAT OUTPUT A

EPDC2

4HN01

3121WE


EPDC1

3AE05

247100 247100

3214XZ

C/B-TR2 RAT OUTPUT B

EPDC2

4HN02

262100 262100

3112WE

C/B-FIRE BTL1/B ENG1

EPDC2

4AF05

3216XZ

C/B-TR2 RAT OUTPUT C

EPDC2

4HN03

3222WE

C/B-FIRE BTL1/B ENG2

EPDC2

4HH03

247100 247100

3125XZ

C/B-TR3 INPUT NORM1

EPDC1

1HC02

262100 262100

3213WE


EPDC1

3HH02

3126XZ

C/B-TR3 INPUT NORM2

EPDC2

2HC02

262100

3123WE


EPDC1

3AF01

247100

3127XZ

C/B-TR3 OUTPUT NORM1

EPDC1

1HC01

262100 262100 262200

3114WE 3224WE

C/B-FIRE BTL2/B ENG1 C/B-FIRE BTL2/B ENG2

EPDC2 EPDC2

4AE05 4HH04

247100

3128XZ

C/B-TR3 OUTPUT NORM2

EPDC2

2HC01

251100 251100

3103MS

C/B-SEAT CAPT

EPDC1

1KF06

3104MS

C/B-SEAT F/O

EPDC2

2KD04

256200

3102MJ

C/B-ASPSU

EPDC2

2JB03

3203WF

C/B-EMER STOP RLY 1 APU

CBP1

5AH01

262200 262200

3204WF

C/B-EMER STOP RLY 2 APU

CBP2

6AK03

3201WF

C/B-FIRE BTL/1 APU

EPDC1

3HH05

262200

3202WF

C/B-FIRE BTL/2 APU

EPDC2

4HJ02


CO & C/B

Training by Airbus


FROM EQUIPMENT

PHYSICAL LOCATION

3101CV

C/B-SFCC1 FLAP

EPDC1

1KK03

3103CV

C/B-SFCC1 FLAP WTB

EPDC1

1KS01

TO ATA

DEVICE FIN

275100 275100 278100

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

279100 279100 279100

3115CE

C/B-ACCLRM LAF VERT3 R

EPDC1

1KQ04

2001CE

C/B-PRIM 1

EPDC1

3HZ11

2002CE

C/B-PRIM 2

EPDC2

4HZ10

1005CE

C/B-PRIM 3

EPDC1

1KZ10

3225CE

C/B-RGAU1

EPDC1

3HB01

3201CW

C/B-SFCC1 SLAT

CBP1

5AH13

278100 278100

3102CW

C/B-SFCC2 SLAT

EPDC2

2KD06

3104CW

C/B-SFCC2 SLAT WTB

EPDC2

2KL06

279100 279100

3223CE

C/B-ACCLRM DAMP LAT1 AFT

CBP1

5AD15

279100 279100

3218CE


CBP2

6AD02

279100

3231CE

C/B-RGAU2

EPDC1

3HB02

279100

3218CE


CBP2

6AG04

279100

3230CE

C/B-RGAU3

EPDC2

4HA01

279100

3121CE

EPDC1

1KQ05

279100

3221CE

CBP1

5AD13

279100 279100

3226CE 3131CE

C/B-RGAU4 C/B-RGAU5

EPDC2 EPDC1

4HA02 1KA06

C/B-SEC 1

EPDC1

3HB05

3221CE

CBP1

5AK12

279100 279100

2003CE

279100

2004CE

C/B-SEC 2

EPDC2

4HB01

CBP2

6AD04

279100 282200

1007CE

C/B-SEC 3

EPDC1

1KZ12

3200QC

C/B-APU FUEL LP V

CBP2

6AF06

CBP2

6AG05

282200

3206QC

C/B-APU FUEL V RLY

CBP2

6AJ10

EPDC1

1KA04

282200 282300 282300

3202QC

C/B-APU ISOL V

CBP2

6AK14

3201QE

C/B-CROSSFEED V A

CBP1

5AA07

3200QE

C/B-CROSSFEED V B

CBP2

6AE12

282400 282400

3201QG

C/B-LP V MOT1 ENG1

CBP1

5AE01

3200QG

C/B-LP V MOT1 ENG2

CBP2

6AA10

282400

3100QG

C/B-LP V MOT2 ENG1

EPDC2

2KE04

279100

3217CE

C/B-ACCLRM DAMP LAT3 AFT C/B-ACCLRM DAMP VERT1 FWD C/B-ACCLRM DAMP VERT1 FWD C/B-ACCLRM DAMP VERT2 FWD C/B-ACCLRM DAMP VERT2 FWD C/B-ACCLRM DAMP VERT3 FWD C/B-ACCLRM LAF VERT1 R

279100 279100

3210CE

C/B-ACCLRM LAF VERT2 L

3212CE

279100

3113CE

279100

3216CE

279100

3216CE

279100

3119CE

CBP1

5AG12

CBP2

6AD03

C/B-ACCLRM LAF VERT2 R

CBP2

6AD01

C/B-ACCLRM LAF VERT3 L

EPDC1

1KA03


CO & C/B

Training by Airbus

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

282400

3101QG

C/B-LP V MOT2 ENG2

EPDC1

1KC03

285100 285100

3201QM 3200QM

C/B-TWDC1 A EMER C/B-TWDC1 B EMER

CBP1 CBP2

285100 285100

3203QM

C/B-TWDC2 A EMER

3202QM

C/B-TWDC2 B EMER

285100 285100

3205QM 3204QM

291100

3205JG

C/B-G ENG1 FSOV CL/OP

CBP1

5AB01

291100 291100 291100

3209JG

C/B-G ENG1 FSOV CLOSE

CBP1

5AB02

TO ATA

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

5AA08 6AE11

291300

3205JY

C/B-Y ENG1 PUMP XDCR SET2

CBP1

5AB04

291300

3208JY

C/B-Y ENG2 FSOV CL/OP

CBP2

6AB15

CBP1

5AE02

291300

3212JY

C/B-Y ENG2 FSOV CLOSE

CBP2

6AB14

CBP2

6AE10

291300

3203JY

C/B-Y ENG2 PUMP DEPRESS

CBP1

5AE03

C/B-TWDC3 A EMER

CBP1

5AA09

291300

3108JY


EPDC2

2KE03

C/B-TWDC3 B EMER

CBP2

6AA09

291300 293100

3207JY


CBP1

5AE07

3101JS

C/B-G SYS PRESS XDCR 1

EPDC1

1KL05

3202JS

C/B-G SYS PRESS XDCR 2

CBP2

6AB13

3201JS

C/B-Y SYS PRESS XDCR 1

CBP1

5AB06

3102JS

C/B-Y SYS PRESS XDCR 2

EPDC2

4AD04 1KC05

3202JG

C/B-G ENG1 PUMP DEPRESS

CBP2

6AA05

3105JG

C/B-G ENG1 PUMP XDCR SET1

EPDC1

1KC04

293100 293100 293100

291100 291100

3206JG


CBP2

6AE08

293200

3101JR

C/B-G RSVR PRESS XDCR

EPDC1

3207JG

C/B-G ENG2 FSOV CL/OP

CBP1

5AE04

293200

3102JR

C/B-Y RSVR PRESS XDCR

EPDC2

4AA03

291100 291100

3211JG

C/B-G ENG2 FSOV CLOSE

CBP1

5AE05

293300

3101JX

C/B-G FLTR CLOG MONIT LH

EPDC1

1KC06

3204JG

C/B-G ENG2 PUMP DEPRESS

CBP2

6AE06

C/B-Y FLTR CLOG MONIT RH

EPDC2

2KE02

3107JG


EPDC1

1KL04

293300 304200

3104JX

291100 291100

3201DG

C/B-WHC1 PWR SPLY

CBP1

5AH06

3208JG


CBP2

6AA07

291300

3206JY

C/B-Y ENG1 FSOV CL/OP

CBP2

6AF15

291300

3210JY

C/B-Y ENG1 FSOV CLOSE

CBP2

6AF14

291300

3201JY

C/B-Y ENG1 PUMP DEPRESS

CBP1

5AH12

291300

3106JY


EPDC2

2KQ03

304200 304200

3100DG

C/B-WHC2 PWR SPLY

EPDC2

2KF05

3103DG

C/B-WINDOW AFT L PWR SPLY

EPDC1

1FD04

304200 304200

3104DG

C/B-WINDOW AFT R PWR SPLY

EPDC2

2FE06

3101DG

C/B-WINDOW FWD L PWR SPLY

EPDC1

1FB02


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

EPDC2

2FB02

EPDC1

1CD05

311900 311900 311900


FROM EQUIPMENT

PHYSICAL LOCATION

TO ATA

DEVICE FIN

311900

3218VM

C/B-ICP MID L 2

CBP2

6AF09

311900

3219VM 3220VM

C/B-ICP MID R 1 C/B-ICP MID R 2

CBP1 CBP2

5AD02 6AA04

3101VM

C/B-ICP NORM1

EPDC1

1KD03

3102VM

C/B-ICP NORM2

EPDC2

2KQ01

3205TU

C/B-CDAU

CBP1

5AF05

3207TU

C/B-FDRS ACCLRM

CBP1

5AF03

304200

3102DG

304500 304500

3201DB

C/B-WINDOW FWD R PWR SPLY C/B-WIPER CAPT 115VAC

3100DB

C/B-WIPER F/O 115VAC

EPDC2

2FA04

308100 308100

3101DD

C/B-ICE DET1 115VAC

EPDC1

1FE05

3100DD

C/B-ICE DET2 115VAC

EPDC2

2FD10

311900

3202VM

C/B-ICP AIR & ELEC 2

CBP2

6AF13

311900

3203VM

C/B-ICP ENG START & ECP 1

CBP1

5AB08

311900 311900

3114VM

C/B-ICP ENG START & ECP 2

EPDC2

2KK04

C/B-SSFDR

EPDC1

1CC03

C/B-ICP FIRE 1

CBP1

5AE10

313300 316100

3201TU

3205VM

3107WK

C/B-DU INNER CAPT

EPDC1

1KB01

311900

3206VM

C/B-ICP FIRE 2

CBP2

6AF12

316100

3207WK

C/B-DU INNER CAPT STBY

CBP1

5AD09

311900

3207VM

C/B-ICP FUEL & HYD 1

CBP1

5AB09

3108WK

C/B-DU INNER F/O

EPDC2

2KG06

311900 311900

3209VM

C/B-ICP LOWER CTR 1

CBP1

5AE11

316100 316100

3106WK

C/B-DU LOWER CENTER

EPDC2

2KF06

3210VM

C/B-ICP LOWER CTR 2

CBP2

6AF11

316100

3206WK

C/B-DU LOWER CENTER STBY

CBP2

6AH09

311900 311900

3211VM 3212VM

C/B-ICP LOWER L 1 C/B-ICP LOWER L 2

CBP1 CBP2

5AB10 6AB10

316100 316100

3109WK

C/B-DU OUTER CAPT

EPDC1

1KB03

3110WK

C/B-DU OUTER F/O

EPDC2

2KP04

311900 311900

3213VM

C/B-ICP LOWER R 1

CBP1

5AF01

3105WK

C/B-DU UPPER CENTER

EPDC1

1KP01

3214VM

C/B-ICP LOWER R 2

CBP2

6AF10

316100 316100

3205WK

C/B-DU UPPER CENTER STBY

CBP1

5AH09

311900 311900

3215VM

C/B-ICP MAINTENANCE 1

EPDC1

3HC03

316200

3101WT

C/B-KCCU CAPT

EPDC1

1KM01

3216VM

C/B-ICP MAINTENANCE 2

CBP2

6AB09

316200

3201WT

C/B-KCCU CAPT STBY

CBP1

5AF04

311900

3217VM

C/B-ICP MID L 1

CBP1

5AF02

316200

3102WT

C/B-KCCU F/O

EPDC2

2KF04

313300 313300


CO & C/B

Training by Airbus

FROM EQUIPMENT

PHYSICAL LOCATION

TO ATA

DEVICE FIN


316200

3202WT

C/B-KCCU F/O STBY

CBP2

6AF08

316600

3101TE

C/B-CMV1

EPDC1

1KS04

FROM EQUIPMENT

PHYSICAL LOCATION

TO ATA

DEVICE FIN


3201GL

C/B-RBCU1 CHAN-B

CBP1

5AH08

3203GL

C/B-RBCU1 CHAN-E

EPDC1

3HH03

316600

3202TE

C/B-CMV2

CBP2

6AK08

328100 328100

323100

3103GA

C/B-L/G CTL LEVER SYS1

EPDC1

1KM02

328100

3100GL

C/B-RBCU2 CHAN-A

EPDC2

2KD05

2KJ06 5AH15

328100 328100

3200GL

C/B-RBCU2 CHAN-B

CBP2

6AH08

3202GL

C/B-RBCU2 CHAN-E

EPDC2

4HJ03

6AC01 1KM03

328100

3107GL

C/B-WRDC NLG

EPDC1

1KM06

328100

3109GL

C/B-WRDC1 L MLG

EPDC1

1KD06

2KJ05

3111GL

C/B-WRDC1 R MLG

EPDC1

1KE01

3110GL

C/B-WRDC2 L MLG

EPDC2

2KG05

323100 323300 323300 324200 324200 324200 324200 324300 324300

3102GA 3201GF 3200GF 3101GG

C/B-L/G CTL LEVER SYS2 C/B-AECM-A SPLY1 C/B-AECM-B SPLY1 C/B-L NBSELV RELAY S1

EPDC2 CBP1 CBP2 EPDC1

3103GG

C/B-R NBSELV RELAY S1

EPDC1

1KD04

328100 328100

3102GG

C/B-R NBSELV RELAY S2

EPDC2

2KF03

328100

3112GL

C/B-WRDC2 R MLG

EPDC2

2KB04

3101LE

C/B-CKPT LT CAPT

EPDC1

1KR04

3100GG

C/B-L NBSELV RELAY S2

EPDC2

3101GY

C/B-ABSELV RELAY S1

EPDC1

1KM05

331200

3100GY

C/B-ABSELV RELAY S2

EPDC2

2KJ04

331200

3201LE

C/B-CKPT LT EMER

EPDC1

3HD05

331200 331200

3100LE

C/B-CKPT LT F/O

EPDC2

2KM02

3107LE

C/B-OUTLET 115V/400HZ

EPDC1

1JB06

331200

3105LE

C/B-OUTLET 28VDC

EPDC1

3AD04

331300 331400

3101LF

C/B-DIM CTL UNIT&INTEG LT

EPDC1

1KN02

3101LP

C/B-ANN LTG RELAY DC 1

EPDC1

1KE02

3102LP

C/B-ANN LTG RELAY DC 2

EPDC2

2KB03

3202LP 3215FP

C/B-ANN LTG RLY DC 2 EMER C/B-ADIRU 1& 3 SWTG DC

CBP2 CBP1

6AA01 5AE15

324300

3200GY

C/B-G BRK ACCU PRESS XDCR

EPDC2

4HJ04

324300

3201GY

C/B-Y BRK ACCU PRESS XDCR

EPDC1

3HH04

324400 324400 324400 325100 325100 328100

3201GZ 3200GZ

C/B-PARK BRK CTL S1 C/B-PARK BRK CTL S2

EPDC1 EPDC2

3HJ03 4HK03

3100GZ

C/B-PARK BRK RELAY S2

EPDC2

2KB02

3101GC

C/B-N/WS XMTR UNIT CAPT

EPDC1

1KD05

3100GC 3101GL

C/B-N/WS XMTR UNIT F/O C/B-RBCU1 CHAN-A

EPDC2 EPDC1

2KF01 1KK04

331400 331400 341100


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

341100

3203FP

C/B-ADIRU1

CBP1

341100

3201FP

C/B-ADIRU1 BKUP

EPDC1

PHYSICAL LOCATION

FROM EQUIPMENT

PHYSICAL LOCATION

3131FC

C/B-STBY STAT L ANTI ICE

EPDC1

1FD01

3133FC

C/B-STBY STAT R ANTI ICE

EPDC1

1FE04

3101RT

C/B-MMR1

EPDC1

1JA03

3102RT

C/B-MMR2

EPDC2

2JA05

5AF06

DEVICE FIN

3HK03

342200

3102FP

C/B-ADIRU2 PROBE PWR SPLY

EPDC2

2KD03

342200 343600 343600

3206FP

C/B-ADIRU3

CBP2

6AB07

343600

3102RT

C/B-MMR2

EPDC2

2JA06

3201SA

C/B-RA 1

EPDC1

1CE05

3102SA

C/B-RA 2

EPDC2

2FA06

3101SA

C/B-RA 3

EPDC1

1FC03 1FC04

341100

3100FP

C/B-ADIRU2

EPDC2

2KL05

341100

3114FP

C/B-ADIRU2 BKUP

EPDC2

4AF07

341100 341100


TO ATA

341100

3103FP

C/B-AOA PROBE PWR SPLY

EPDC1

1KB05

344200 344200 344200

341100 341100

3221FP

C/B-ISP1 ANTI ICE

EPDC1

1CB05

345100

3101SD

C/B-DME 1

EPDC1

3112FP

C/B-ISP2 ANTI ICE

EPDC2

2JA04

3102SD

C/B-DME 2

EPDC2

2FE07

3101RS 3102RS

C/B-VOR1 C/B-VOR2

EPDC1 EPDC2

1FC07 2FE10

EPDC1

1JA03

341100

3204FP

C/B-ADIRU3 BKUP

EPDC2

4HJ01

341100

3101FP

C/B-AOA PROBE ANTI ICE

EPDC1

1FD07

341100 341100

3220FP

C/B-ISP3 ANTI ICE

EPDC2

2CE01

3219FP

C/B-MFP1 ANTI ICE

EPDC1

1CC06

345100 345500 345500

341100

3104FP

C/B-MFP2 ANTI ICE

EPDC2

2JA07

347100

3103SE

C/B-AESU1 (WXR + TAWS)

341100

3216FP

C/B-MFP3 ANTI ICE

EPDC2

2CB06

347100

3101SE

C/B-AESU1 (XPDR + TCAS)

EPDC1

1JA05

3104SE

C/B-AESU2 (WXR + TAWS)

EPDC2

2JA06

341100 341100

3217FP

C/B-SSA1 ANTI ICE

EPDC1

1CE06

347100

3108FP

C/B-SSA2 ANTI ICE

EPDC2

2JA03

347100 421100

3102SE

C/B-AESU2 (XPDR + TCAS)

EPDC2

2JA02

3205TF

C/B-CPIOM H31

CBP1

5AF10

421100 421100

3108TF

C/B-CPIOM H42

EPDC2

4AC07

3103TF

C/B-CPIOM H43

EPDC1

1KR05

421100

3110TF

C/B-CPIOM H44

EPDC2

2KL02

341100

3218FP

C/B-SSA3 ANTI ICE

EPDC2

2CD02

342200

3201FC

C/B-ISIS IND1 28VDC EMER

EPDC1

3HA04

342200 342200

3202FC 3221FC

C/B-ISIS IND2 28VDC EMER C/B-STBY PITOT ANTI ICE

CBP2 EPDC1

6AD15 1CB04


CO & C/B

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

421100

3107TF

C/B-CPIOM H61

EPDC1

1KR06

TO ATA

DEVICE FIN


421100 421100

3114TF

C/B-CPIOM H62

EPDC2

2KL03

424100

3134TS

C/B-CRDC B02 DSO GP1

EPDC2

2KJ03

3109TF

C/B-CPIOM H63

EPDC1

1KH05


EPDC2

2KC01

3116TF

C/B-CPIOM H64

EPDC2

2KL01

424100 424100

3136TS 3138TS


EPDC2

2KJ02

3116TS

C/B-CRDC B04

EPDC2

4AA04


EPDC1

1KF05

421100 423100

FROM EQUIPMENT

PHYSICAL LOCATION

3211TH

C/B-AFDX SW 11

EPDC1

3HC02

424100

423100 423100

3212TH

C/B-AFDX SW 12

EPDC2

4HC03

424100

3145TS

3213TH

C/B-AFDX SW 13

EPDC1

3HD02


CBP1

5AF08

3214TH

C/B-AFDX SW 14

EPDC2

4HC04

424100 441100

3227TS

423100

3122RH

C/B-DEU-A CTR FWD ESS

EPDC2

4AD07

423100

3215TH

C/B-AFDX SW 15

EPDC1

3HC01

441100

3124RH

C/B-DEU-A CTR MID ESS

EPDC2

4AC06

423100

3216TH

C/B-AFDX SW 16

EPDC2

4HC05

441100

3226RH

C/B-DEU-A CTR1 AFT EMER

EPDC2

4HG03

423100

3219TH

C/B-AFDX SW 19

EPDC1

3HD03

441100

3126RH

C/B-DEU-A CTR1 AFT ESS

EPDC2

4AC05

424100 424100

3201TS

C/B-CRDC A01

CBP1

5AB15

441100

3222RH

C/B-DEU-A CTR1 FWD EMER

EPDC2

4HF04

3101TS

C/B-CRDC A03

EPDC1

1KR01

441100

3228RH

C/B-DEU-A CTR2 AFT EMER

EPDC2

4HG04

424100

3103TS

C/B-CRDC A05

EPDC1

1KA02

C/B-DEU-A CTR2 AFT ESS

EPDC2

4AB02

3106TS

C/B-CRDC A06

EPDC2

2KC05

3224RH

C/B-DEU-A CTR2 FWD EMER

EPDC2

4HE03

424100

3105TS

C/B-CRDC A07 BKUP

EPDC1

1KP02

441100 441100 441100

3128RH

424100

3111RH

C/B-DEU-A L FWD ESS

EPDC1

3AB04

424100

3107TS

C/B-CRDC A09

EPDC1

3AD01

3113RH

C/B-DEU-A L MID ESS

EPDC1

3AC03

424100

3110TS

C/B-CRDC A10 BKUP

EPDC2

2KG04

424100

3109TS 3113TS

C/B-CRDC A11 C/B-CRDC A15

EPDC1 EPDC1

1KA01 1KN06

441100 441100 441100 441100

3215RH 3115RH

C/B-DEU-A L1 AFT EMER C/B-DEU-A L1 AFT ESS

EPDC1 EPDC1

3HF05 3AB03

3211RH

C/B-DEU-A L1 FWD EMER

EPDC1

3HE05

3114TS

C/B-CRDC B02

EPDC2

2KG02

441100

3217RH

C/B-DEU-A L2 AFT EMER

EPDC1

3HG01

424100 424100


CO & C/B

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

441100 441100

3117RH 3213RH

C/B-DEU-A L2 AFT ESS C/B-DEU-A L2 FWD EMER

EPDC1 EPDC1

3AC02 3HE04

441100 441100

3112RH 3114RH

C/B-DEU-A R FWD ESS C/B-DEU-A R MID ESS

EPDC2 EPDC2

4AC03 4AC04

441100 441100 441100 441100 441100 441100 441100 441100 441100 441100 441100 441100 441100 441100 441100

3216RH 3116RH

C/B-DEU-A R1 AFT EMER C/B-DEU-A R1 AFT ESS

EPDC2 EPDC2

4HE02 4AB04

3212RH 3218RH

C/B-DEU-A R1 FWD EMER C/B-DEU-A R2 AFT EMER

EPDC2 EPDC2

4HG01 4HG02

3118RH 3214RH

C/B-DEU-A R2 AFT ESS C/B-DEU-A R2 FWD EMER

EPDC2 EPDC2

4AA07 4HE01

3243RH 3143RH

C/B-DEU-B L AFT EMER C/B-DEU-B L AFT ESS

EPDC1 EPDC1

3HE03 3AA01

3241RH 3141RH

C/B-DEU-B L FWD EMER C/B-DEU-B L FWD ESS

EPDC1 EPDC1

3HF04 3AC06

3247RH 3147RH

C/B-DEU-B L2 AFT EMER C/B-DEU-B L2 AFT ESS

EPDC1 EPDC1

3245RH 3145RH 3244RH

C/B-DEU-B L2 FWD EMER C/B-DEU-B L2 FWD ESS C/B-DEU-B R AFT EMER

441100

3144RH

C/B-DEU-B R AFT ESS

EPDC1 EPDC1 EPDC2 EPDC2

3HG02 3AB02 3HE02 3AA02 4HF01 4AB05

441100 441100 441100

3242RH 3142RH 3201RH

C/B-DEU-B R FWD EMER C/B-DEU-B R FWD ESS C/B-DIR1 EMER

EPDC2 EPDC2 EPDC1

4HE04 4AB07 3HF01

Training by Airbus

TO ATA

DEVICE FIN


FROM EQUIPMENT

PHYSICAL LOCATION

441100

3101RH

C/B-DIR1 ESS

EPDC1

3AB05

441100 441100 441100

3202RH 3102RH

C/B-DIR2 EMER C/B-DIR2 ESS

EPDC2 EPDC2

4HE05 4AD06

3251RH

C/B-FAP DR1 EMER

EPDC1

3HE01

441100 441100

3151RH

C/B-FAP DR1 ESS

EPDC1

3AB06

3253RH

C/B-FAP DR2 EMER

EPDC1

3HG03

441100 454500 461100 461100 461100 494100 494100 525100 715100

3153RH

C/B-FAP DR2 ESS

EPDC1

3AC05

3202TC 3201TL

C/B-OSFC EMER C/B-SCI-1

EPDC2 EPDC1

2CA04 1CA04

3102TL 3102TL 3101KA 3200KA 3101MQ 3107KS

C/B-SCI-2 C/B-SCI-2 C/B-POR APU C/B-SGCU BKUP SPLY C/B-CDLCU C/B-A/C PERMISSION DSCRT1

EPDC2 EPDC2 EPDC1 CBP2 EPDC1 EPDC1

2FD05 2FD08 1DA01 6AD06 1KB02 1KQ03

715100

3108KS

EPDC2

2KN05

715100 715100 732100 732100 741100 741100

3201KS 3202KS 3201KC

C/B-A/C PERMISSION DSCRT2 C/B-EEC1 CHAN-A C/B-EEC2 CHAN-A C/B-HP FUEL SOV ENG1

EPDC1 EPDC2 CBP1

1CA03 2CE01 5AG06

3202KC 3201EH 3202EH

C/B-HP FUEL SOV ENG2 C/B-IGN SYS A ENG1 C/B-IGN SYS A ENG2

CBP2 EPDC1 EPDC2

6AH04 1CE06 2CA02


CO & C/B

Training by Airbus

AIRFRAME

ELECTRO-MECHANICAL SYSTEMS

ATA 29 - HYDRAULIC POWER

P. 289

ATA 32 - LANDING GEARS

P. 305

ATA 51 - STANDARD PRACTICES AND STRUCTURES

P. 349

ATA 52 - DOORS

P. 356

ATA 25/50 - EQUIPMENT & FURNISHING AND CARGO & ACCESSORY COMP.

P. 371

ATA 27 - FLIGHTS CONTROLS

P. 384

ATA 35 - OXYGEN

P. 409

ATA 38 - WATER AND WASTE

P. 416 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

ATA 29 HYDRAULIC POWER

HYDRAULIC SYTEM USERS BRAKES WHEELS 5, 6, 7, 8

Pr

MLG EXTENSION/RETRACTION

BRAKES WHEELS 1, 2, 3, 4

RAM AIR TURBINE RETRACTION

NLG EXTENSION/RETRACTION

RUDDER (LOWER ACTUATOR: EHA REFILLING) RUDDER (MIDDLE ACTUATOR)

ELEVATOR ACTUATOR & EHA REFILLING (RIGHT)

INBOARD AILERON EHA (RIGHT) (REFILLING)

ISOLATION VALVE

RUDDER (UPPER ACTUATOR) SPOILERS 2, 5, 7 (LEFT & RIGHT)

SPOILERS 3, 4, 6 (LEFT & RIGHT) HYDRAULIC FUSE

NOTE

NOSE WHEEL STEERING

ELEVATOR ACTUATOR & EHA REFILLING (LEFT)

ISOLATION VALVE

Training by Airbus

CARGO DOORS

SPOILERS 1 (RIGHT)

HYDRAULIC FUSE

SPOILERS 1 (LEFT)

HYDRAULIC FUSE

INBOARD AILERON EHA (LEFT) (REFILLING) INBOARD AILERON (LEFT & RIGHT) OUTBOARD AILERON (RIGHT)

OUTBOARD AILERON (RIGHT) OUTBOARD AILERON (LEFT) HYDRAULIC FUSE

OUTBOARD AILERON (LEFT) MLG PITCH TRIMMER LEFT & RIGHT FLAP POWER CONTROL UNIT

BACKUP POWER SUPPLY SLAT & FLAP PCU

Page 289 GREEN HYD SYSTEM

YELLOW HYD SYSTEM


29

HYDRAULIC SYSTEM (CONTROLS & INDICATING) Training by Airbus

ELEC EMP AUTO P/B SW GND HYD

A U T O

FAULT

ON

OFF

YELLOW ELEC EMP P/B SW

YELLOW ELEC PMP

GREEN ELEC PMP A U T O

NOTE

FAULT

OFF

ON

ENG 2

SYSTEM PRESSURE AND LABEL

FIRE FIR RE E PUSH

ELEC PUMPS INDICATION

AGENT 1

AGENT 2

SQUIB

SQUIB

DISH

DISH

F I R E

FSOV OPEN

ENGINE IDENTIFICATION EDP

GREEN

FSOV

SUPPLY

RESERVOIR FLUID LEVEL RSVR PRESS LO

GREEN

H Y D

SUPPLY

PUMP

ENG 1

YELLOW SUPPLY

PUMP

GREEN SUPPLY

FAULT FAU F AULT L

ISOL

OFF O F

FSOV ISOLATION

OVHT

PUMP

ENG 2

YELLOW SUPPLY

PUMP

OVHT

FAULT F FAU L LT

OVHT

FAULT F FAU L LT

OVHT

FAULT F FAU L LT

OVHT

FAULT F FAU L LT

ISOL

OFF

ISOL

OFF

ISOL

OFF FF

ISOL

OFF

PUMP

OVHT VH

EDP CTL

235 VM

H Y D

Page 290 GREEN ENG 1 EDP P/B SW

GREEN ENG 2 SUPPLY P/B SW


29

HYDRAULIC SYSTEM (ARCHITECTURE) PRIMARY F/CTL

NOSE LANDING GEAR EXTENSION/RETRACTION

HIGH LIFT SYSTEM

NOSE WHEEL STEERING

BRAKES

BRAKE ACCU REFILL S

Training by Airbus CARGO DOORS

NOTE

ARV

SAMPLING VALVE ISOLATION VALVE S

PRESSURE MAINTAINING VALVE HP MANIFOLD

BYPASS VALVE HHX

CASE DRAIN MANIFOLD

BYPASS VALVE

Th

HHX ACCUMULATOR TO LP RETURN MANIFOLD

TO LP RETURN MANIFOLD

SYSTEM MANIFOLD

CASE DRAIN MANIFOLD

EDP C

LP RETURN MANIFOLD

ENG 1 M


HP MANIFOLD

Th

C EDP

PRESSURE RELIEF VALVE

P

EMP HYDRAULIC AUXILIARY PUMP

ENG 2 M

XDCR

FSOV


GROUND CONNECTOR DELIVERY

FROM USERS

FSOV

GROUND CONNECTOR SUCTION

Page 291

RESERVOIR


29

HYDRAULIC SYSTEM (ARCHITECTURE) PRIMARY F/CTL

HIGH LIFT SYSTEM

NOSE LANDING GEAR EXTENSION/RETRACTION

NOSE WHEEL STEERING

BRAKES

BRAKE ACCU REFILL S

HP MANIFOLD

HP MANIFOLD

Training by Airbus

CARGO DOORS

NOTE

ARV

SAMPLING VALVE

PRESSURE MAINTAINING VALVE

PRESSURE RELIEF VALVE

ISOLATION VALVE S

TO LP RETURN MANIFOLD Th

BYPASS VALVE HHX

CASE DRAIN MANIFOLD

C EDP

BYPASS VALVE HHX ACCUMULATOR



SYSTEM MANIFOLD

CASE DRAIN MANIFOLD

EDP C

LP RETURN MANIFOLD

ENG 1 M

Th

RESERVOIR

P

EMP HYDRAULIC AUXILIARY PUMP

ENG 2 M

XDCR

FSOV



FROM USERS

GROUND CONNECTOR SUCTION FSOV

EMP STARTED FROM COCKPIT


29

GREEN HYDRAULIC SERVICING PANEL Training by Airbus

NOTE

D

RESERVOIR FILLING HOSE (INSIDE)

RESERVOIR FILLING HAND PUMP PORT RESERVOIR-FILLING HAND-PUMP HANDLE

RESERVOIR FILLING SELECTOR-VALVE RESERVOIR FILLING HAND-PUMP

C

C RESERVOIR LEVEL GAGE RESERVOIR-FILLING QUICK-DISCONNECT COUPLING RESERVOIR-FILLING FILTER + POP-OUT

D


29

YELLOW HYDRAULIC RESERVOIR SUCTION TO PUMP

Training by Airbus

SYSTEM DISPLAY

HP FROM ACCU/PUMP CPIOM

NOTE

LGERS TEMP SENSOR

S

XDCR

L/G EXTENDED/RETRACTED AND DOORS POSITION CPIOM HMCA-Y

FLUID LEVEL SW

RESERVOIR LP FROM RETURN

GREEN GROUND SERVICE PANEL


29

YELLOW HYDRAULIC RESERVOIR Training by Airbus

BLEED VALVE BLEED VALVE

NOTE SUCTION TO PUMP

ROTARY KNOB

HP FROM ACCU/PUMP

BLEED VALVE

LVE & HP RELIEF VALVE RESS VALVE MANUAL DEPRESS

DRAIN VALVE

S

ELECTRICAL DEPRESSURIZATION VALVE

XDCR

SW

RESERVOIR DRAIN VALVE

YELLOW GROUND SERVICE PANEL

LP FROM RETURN


29

RESERVOIR MONITORING ITEMS Training by Airbus RESERVOIR LEVEL TRANSDUCER (LVDT)

TEMPERATURE SENSOR X2

LOW LEVEL SWITCH

CRDC HMCRF

GREEN HYD SYSTEM SHOWN AS EXAMPLE (YELLOW SYSTEM SIMILAR)

PRESSURE TRANSDUCER

NOTE

RESERVOIR PRESSURE AND LEVEL

AFDX NETWORK

CPIOM HMCA-G

CDS HYD GREEN

FLIGHT WARNING SYSTEM

5000 PSI

ELEC PUMPS

YELLOW 5000 PSI

1

2

GREEN RSVR


YELLOW RSVR

HYDRAULIC PAGE


29

SOURCES FOR YELLOW HYRDAULIC SYSTEM PRESSURISATION Training by Airbus

GROUND SERVICE CART

NOTE

GND HYD YELLOW ELEC PMP

GREEN ELEC PMP A U T O

FAULT

ON

OFF

A U T O

FAULT

ON

OFF

TO CARGO DOOR & BRAKE/BRAKE ACCU

TO ALL USERS

CPIOM HMCA-Y GROUND SERVICE CART CONNECTOR

A F D X N E T W O R K

SAMPLING VALVE PRESSURE RELIEF VALVE

SSPC ISOLATION VALVE +28VDC

S


TO RSVR BOOTSTRAP

MANIFOLD SYSTEM SWITCH (DEDICATED TO ISOLATION VALVE ENERGIZATION) SYSTEM MANIFOLD



FROM EMP

FROM HYDRAULIC AUXILIARY PUMP


29

EMP CONTROL Training by Airbus

ICP GROUND HYDRAULIC PANEL

HMCA

HYD YELLOW ELEC PMP A U T O

OFF

OR +28VDC

SSPC

EMP START CMD

FOR GREEN AND YELLOW SYSTEMS (Accu Reinflate)

BCS

DSCS

FAULT

ON

EMP AUTO START

FOR YELLOW SYSTEM ONLY (Cargo Door Actuation)

ENGINE NOT RUNNING MLG COMPRESSED INFO GIVEN BY LGERS (WEIGHT ON WHEELS)

AND

NOTE

PCS

LGERS OR ADIRS

RCCB COMMAND NO FAULTS DETECTED BY MCPU OR CRDC

CRDC

EMP START CMD

RCCB AND

MCPU

EMP

Page 298

230 VAC


29

FSOV / EDP CONTROL Training by Airbus

HYDRAULIC PANEL SUPPLY

28 VDC

PUMP

OVHT

FAULT

ISOL

OFF

NOTE TO USERS

ENGINE START

FQMS

UERF DETECTION LOGIC

EDP AUTO DEPRESS

LOW LEVEL IN WING FUEL TANK(S)

CPIOM HMCA-Y

OR

S

ENG 1

EDP DEPRESSURIZATION

AUTO CLOSURE FSOV 28 VDC

ENG 1 F I R E

FIRE

FSOV

RELAY LOGIC

M

PUSH

28 VDC

Page 299 FROM RESERVOIR


29

EDP CLUTCH / DECLUTCH DESCRIPTION SPLINE NE SHAFT

Training by Airbus

OUTLET TO CASE-DRAIN LINE

NOTE

ELECTRICAL CONNECTOR DEPRESSURIZATION VALVE

INLET FROM SUCTION LINE VISUAL INDICATION

OUTLET TO PRESSURE LINE

A

HEX SOCKET

COVER RELEASE CABLE

TO DISENGAGE: ROTATE HEX CCW TO OFF POSITION

TO RE-ENGAGE: 1 - REMOVE COVER 2 - PULL RELEASE CABLE 3 - REINSTALL COVER

Page 300

A


29

HYDRAULIC SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE

Z190

GREEN RESERVOIR

YELLOW RESERVOIR


29

HYDRAULIC SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE Z190

C Z310

A

B

D

B

FR98

A

E

RUDDER ISOLATION VALVE

B LH SHOWN, RH SYMMETRICAL


D


Page 302

C


29

HHX BYPASS VALVE (MANUAL OVERRIDE) Training by Airbus

For maintenance, manual override of the Heat Exchanger Bypass Valve is possible with GSE tool, independent from fluid temperature. This tool consists of :

HHX BYPASS VALVE

NOTE

GSE TOOL NUT (IT CAN BE MOVED INSIDE THE NUT THANKS TO A THREAD)

LATCH

WASHER

HHX BYPASS VALVE AND GSE TOOL

RING FOR A WARNING STREAMER


29

HHX BYPASS VALVE (MANUAL OVERRIDE) Training by Airbus

USE OF GSE TOOL FOR HHX BYPASS VALVE

NOTE

THREADS FLANGE ON NUT

Use of the tool: The latch of the GSE Tool is slide onto HHX Bypass Valve grabbing HHX Bypass Valve pin. The flange of the HHX Bypass Valve and the nut of GSE Tool are in contact, but the nut is still free to be rotated.

YELLOW VISUAL INDICATOR

When rotating the nut by a standard tool the latch is pulled away from the HHX Bypass Valve pulling out the pin of the HHX Bypass Valve. If the indicator (yellow visual indicator) is fully visible the HHX Bypass Valve is fully open.

PIN IN DEFAULT STATE (HHX BYPASS VALVE CLOSED)

Page 304

PIN PULLED PUT OUT (HHX BYPASS VALVE OPEN)


29

ATA 32 LANDING GEARS

L/G AND BRAKING SYSTEMS (CONTROLS) Training by Airbus

PARKING BRAKE CONTROL PANEL PARK BRK

ACCUS REINFLATE

OFF

NOTE

YELLOW 0

4

BRK FAN

PSI

ACCU

x1000

0

4

ANTI SKID ON O

HOT GREEN

PULL & TURN

ON

ON

OFF F BRAKING BRA ACTION ACTI TI

NOSE WHEEL STEERING HAND WHEEL LANDING GEAR GRAVITY EXTENSION A/BRK

BRAKE PANEL L/G

UP

D DOWN

L/G LEVER

BRAKE PEDALS


32

L/G AND BRAKING SYSTEMS (INDICATING) Training by Airbus

WHEEL

NOTE

WHEEL

X 1000 PSI BRAKES 3.5


L/G GRVTY EXTN IN PROGRESS

1

1

Y

Y 0

G

NORM ALTN EMER

G

Y

123 °C 2

120 3

G

Y ACCU

PSI

G

120 6

0

G SYS BRK

120 7

120 8

G

GEAR NOT DOWNLOCKED GEAR GEAR IN DOWNLOCKED TRANSITION

1.6 0

1.6

120 123 °C 120 120 Y Y 1 Y ACCU 2 3 4 Y ACCU PSI A-SKID A-SKID

NORM ALTN EMER

120 5

NORM ALTN EMER

G

3.5

120 4

Y

Y SYS BRK

Y

1.6 0

120 1

0

Y SYS BRK

Y

Y ACCU

3.5

G SYS BRK NORM ALTN EMER

G ACCU

3.5

120 5

G

120 6

120 7

G

120 8

1.6 0

G ACCU

3.5

DOOR DOOR DOOR FULLY FULLY OPEN UPLOCKED OPEN FAULTY

GEAR STATUS GEAR NOT GEAR UPLOCKED UPLOCKED NOT VALID OR GEAR RETRACTION FAULT

DOOR IN TRANSIT

DOOR IN TRANSIT FAULTY

INVALID DOOR POSITION


32

NLG DESCRIPTION Training by Airbus

NOTE NITROGEN CHARGING VALVE NITROGEN CHAMBER (HP)

MAIN FITTING

SLIDING TUBE

NO BAND = PRIMARY SEAL ACTIVE RED BAND = SPARE SEAL ACTIVATED

CHANGEOVER VALVE OIL CHARGING VALVE

NITROGEN

Page 307

FLUID


32

MLG DESCRIPTION AND SERVICING Training by Airbus

NOTE

NITROGEN CHARGING VALVE NITROGEN CHAMBER (HP) MAIN FITTING N2

GREEN BAND = PRIMARY SEAL ACTIVE RED BAND = SPARE SEAL ACTIVATED SLIDING TUBE

SEAL

NITROGEN

CHANGEOVER VALVE

CHANGEOVER VALVE

OIL CHARGING VALVE OIL PUMP

Page 308

FLUID


32

NORMAL EXTENSION / RETRACTION SYSTEM L/G

LGCIS 1 CPIOM LGERS

UP

Training by Airbus

LGCIS 2

CPIOM LGERS

CPIOM LGERS

CPIOM LGERS

NOTE

D DOWN

GEARS/ DOORS POSITION SYSTEM 1

CRDC

AFDX NETWORK AIRCRAFT SPEED

28 VDC SSPC

28 VDC SSPC

CRDC

ADIRS

GEARS/ DOORS POSITION SYSTEM 2

28 VDC

28 VDC GROUND

ISOLATION VALVES SELECTOR VALVES

GROUND MLG ONLY SHOWN. SAME PRINCIPLE FOR NLG WITH YELLOW SYSTEM.

HYDRAULIC SUPPLY UPLOCK OCK VAL VALVES

MLG DOOR ACTUATOR ACT

MLG ACTUATORS S

NLG

MLG

ACTUATORS

NLG

+ DOORS ACTUATORS

+ DOORS ACTUATORS

ISOLATION VALVE

GEAR UPLOCK

DOOR UPLOCK

INTEGRATED MANIFOLD NLG MLG


32

NORMAL EXTENSION / RETRACTION SYSTEM Training by Airbus 2

1

1

LGCIS 1

2

LGCIS 2

1

2

OR OR ISOLATION GEAR SEQUENCE VALVE VALVE OFF

DOWN

OPEN P R

1

2

2

1

OR DOOR SEQUENCE VALVE

OR DOOR UPLOCK VALVE

2

1

OR GEAR UPLOCK VALVE

NOTE

S

R S

S

EXTEND

S

S

RETRACT OPEN

S

CLOSE

RELEASE A

A

A

A

S INTEGRATED RELEASE MANIFOLD

A

A

A

CPIOM LGERS L/G

TO RH MLG

CRDCs GROUND

UP

VALVES ENERGIZED

CPIOM LGERS

SSPC

28 VDC SYSTEM 1 OR 2

LH MLG SHOWN ONLY.


32


1

1

LGCIS 1

2

LGCIS 2

1

OR ISOLATION VALVE

2

2

1



UP

NOTE

OPEN P R

DOWN

S

R S

S

S

S

S

RELEASE

OPEN A A

A

S

A

INTEGRATED MANIFOLD

A

A

A

TO RH MLG


32


1

1

2

1

2

OR OR OR ISOLATION GEAR SEQUENCE DOOR SEQUENCE VALVE VALVE VALVE OFF

1

LGCIS 1

2

LGCIS 2

DOWN

2

1


L/G

NOTE

OPEN P R

UP

DOWN

R

S

S

S

S

S

S

RETRACT OPEN

RELEASE A

A

A

S

A

INTEGRATED MANIFOLD

A

A

A

TO RH MLG


32


1

LGCIS 1

2

LGCIS 2

2

2

OR OR ISOLATION GEAR SEQUENCE VALVE VALVE

1

2


2

1


L/G

NOTE

OPEN P R

UP

DOWN

R

S

S

S

S

S

S

RETRACT OPEN

RELEASE A

A

A

S

A

INTEGRATED MANIFOLD

A

A

A

TO RH MLG


32

NORMAL EXTENSION / RETRACTION SYSTEM Training by Airbus

1 1

LGCIS 1

2

LGCIS 2

OR

2

1

ISOLATION VALVE

OR

2 UP

NOTE

DOOR SEQUENCE VALVE

OPEN P R

DOWN

S

R S

S

S

S

S

S

CLOSE A A

A

A

INTEGRATED MANIFOLD

A

A

A

TO RH MLG


32

NORMAL EXTENSION / RETRACTION SYSTEM Training by Airbus

1 1

LGCIS 1

2

LGCIS 2

OR

2

1

ISOLATION VALVE

OR

2 UP

NOTE

DOOR SEQUENCE VALVE

OPEN P R

DOWN

S

R S

S

S

S

S

S

CLOSE A A

A

A

INTEGRATED MANIFOLD

A

A

A

TO RH MLG


32

NORMAL EXTENSION / RETRACTION SYSTEM Training by Airbus UP

NOTE

CLOSED P R

S DOWN

R S

S

EXTEND

RETRACT

S

S

OPEN

CLOSE

A

S

RELEASE A

A

INTEGRATED RELEASE MANIFOLD

S

A

A

A

A

TO RH MLG


32

GROUND DOOR OPENING SYSTEM Training by Airbus A

TO OTHER DOOR

MLG MANIFOLD ASSEMBLY DOOR SELECTOR VALVE

BAULK MECHANISM

NOTE

P S

BYPASS VALVE

OPEN

S

CLOSE

BYPASS VALVE

A

GDO HANDLE NOT USED

GDO HANDLE

GEAR DOOR


32

GROUND DOOR OPENING SYSTEM Training by Airbus A

TO OTHER DOOR

MLG MANIFOLD ASSEMBLY DOOR SELECTOR VALVE

NOTE

P S

BYPASS VALVE

OPEN

S

CLOSE

A

HANDLE LOCKED BY BAULK

HANDLE RELEASED BY HYDRAULIC

GDO HANDLE

GEAR DOOR


32

ALTERNATE EXTENSION SYSTEM A

ALTERNATE EXTENSION CIRCUIT TO R/H MLG

B

TO R/H MLG

Training by Airbus

A L/G GRVTY EXTN RESET

NOTE

AECM

OFF

A

DOWN

B

MLG ALTERNATE POWER PACK

S

HP SUPPLY S

RETURN

S

S

S

S

B B

B

B

S

REDUCED PRESS

B

B

D

S

D

R

VENT VALVE C

C

LH MLG GDO HANDLE SCENARIO : LGERS ALL CPIOMs APPLICATION FAILED


32



B

TO R/H MLG

TO NLG ALTERNATE POWER PACK

L/G GRVTY EXTN RESET

NOTE

AECM

OFF

A

DOWN

Training by Airbus

A

B


S

HP SUPPLY S

RETURN

S

S

S

S

B B

B

B

S

REDUCED PRESS

B

B

S

D

D

R

VENT VALVE C

C



32



B

TO R/H MLG

Training by Airbus A L/G GRVTY EXTN

NOTE

AECM A

B


S

S

RETURN

S

S

S

S

B B

B

B

S

B

B S

D

D

R

VENT VALVE C

C

LH MLG A/C ON GROUND

GDO HANDLE SCENARIO : LGERS ALL CPIOMs APPLICATION FAILED

WARNING: BEFORE STARTING THE RESET PROCEDURE , ENSURE THAT ALL THE GROUND DOOR OPENING HANDLES ARE IN THE DOWN (DOOR OPEN) POSITION.


32



B

TO R/H MLG

Training by Airbus A L/G GRVTY EXTN

NOTE

RESET

AECM

OFF

A

DOWN

B


S

HP SUPPLY S

RETURN

S

S

S

S

B B

B

B

S

B

B

REDUCED HP PRESS S

D

D

R VENT VALVE C

C



32



B

TO R/H MLG

TO NLG L/G GRVTY EXTN

NOTE

RESET

AECM

OFF

E

TO VENT VALVE

A

DOWN

E B


S

S

RETURN

Training by Airbus

A

S

S

S

S

B B

B

B

S

B

B

E

D

S

D

R

C

C



32

L/G AND DOORS POSITION MONITORING Training by Airbus

IND SYSTEM NOSE, LEFT AND RIGHT LANDING GEAR SENSORS

NOSE, LEFT AND RIGHT LANDING GEAR AND DOORS SENSORS

NOSE, LEFT AND RIGHT LANDING GEAR AND DOORS SENSORS

GEAR DOWN LOCKED

GEAR GEAR DOOR GEAR BOGIE DOOR DOWN UP UP EXTENDED DIPPED OPENED LOCKED LOCKED LOCKED

GEAR GEAR DOOR GEAR BOGIE DOOR DOWN UP UP EXTENDED DIPPED OPENED LOCKED LOCKED LOCKED

POSITIONS PROVIDED BY LGCIS 1

POSITIONS PROVIDED BY LGCIS 2

CRDC

CRDC NOSE LEFT RIGHT

CRDC NOSE LEFT RIGHT

NOSE LEFT RIGHT

CPIOM

NOTE

LGERS

AFDX NETWORK

PFD

SD WHEEL X 1000 PSI Y MAX

CDS FWS

1

Y G

200

200

0

G

Y SYS BRK NORM ALTN EMER

120 1

Y

120 °C 2

120 3

G

120 6

120 7

PSI

Y

120 4

G

120 8

0

Y ACCU

3.5

G SYS BRK 120 5

NORM ALTN EMER

0

SLAT-FLAP LIMITATION MEMO

G ACCU

WHEELS PAGE

3.5

OTHER SYSTEMS


32

L/G BRAKING SYSTEM (INDICATING) Training by Airbus

NOTE

WHEEL


L/H & R/H BRAKING PRESSURE

1

Y 0

Y SYS BRK

Y G

G

1.6 0

FWD WHEELS GROUP

120 1

Y

123 °C 2

120 3

Y

FWD WHEELS GROUP MODE

NORM ALTN EMER

Y ACCU

3.5

120 4

PSI

G SYS BRK

AFT WHEELS GROUP MODE

NORM ALTN EMER AFT WHEELS GROUP

120 120 G 5 G ACCU 6 A-SKID

ACCU PRESSURE

120 120 G 7 8 G ACCU A-SKID

1.6 0

G ACCU

3.5

ACCU PRESSURE


32

NORMAL BRAKING MODE OPERATION CAPT PEDAL

Training by Airbus

F/O AUTO RETRACTION PEDAL BRAKE BRAKING L/G

BRAKE FAN

YELLOW HP SUPPLY

UP

ANTI SKID ON O

HOT ON OFF BRAKING ACTION

RWY COND

R

PRESSURE LIMITING VALVE

A/BRK

2X SELECTOR VALVE

CPIOM BCS

R

R

R S

NBSELV

NSV SV

SV

1

R S

S

NBSELV 2X PRESSURE TRANSDUCER 4X NSV R SERVO R VALVE

RBCU

PRV

S

ARV

ADIRS

NOTE

R X D C R

ASV

S

ABSELV

R

NSV

PBSELV

SV

SV

ASV

NSV

R

SV

SV

2

4X PRESSURE TRANSDUCER 4X WHEEL SPEED

T

WHEEL 1

T

WHEEL 5

F

F

F

T

WHEEL 2

T

WHEEL 6

T

F

T

WHEEL 3

T

WHEEL 4

T

WHEEL 7

WHEEL 8


32

ALTERNATE BRAKING MODE OPERATION CAPT PEDAL

Training by Airbus

F/O AUTO PEDAL BRAKE YELLOW HP SUPPLY

BRAKE FAN

ANTI SKID ON O

CDS

HOT ON OFF BRAKING ACTION

RWY COND

TO RBCUs R


A/BRK

1X SELECTOR VALVE

CPIOM BCS

R

A

1X PRESSURE TRANSDUCER 2X SERVO R VALVE

RBCU 1

R

R

S

S

NBSELV

NSV

NSV

R

ASV SV

R S

NBSELV

SV

PRV

S

ARV

ADIRS

NOTE

R X D C R

S

ABSELV

A

R

NSV

PBSELV

NSV

R

SV

SV

ASV

SV

SV

2

4X PRESSURE TRANSDUCER 4X WHEEL SPEED

T

WHEEL 1

T

WHEEL 5

F

F

F

T

WHEEL 2

T

WHEEL 6

T

F

T

WHEEL 3

T

WHEEL 4

T

WHEEL 7

WHEEL 8


32

PARKING BRAKE / ULTIMATE BRAKING MODE OPERATION PARK BRK

A

ACCUS REINFLATE

4 PSI

ACCU

x 1000

0

4

EMER BATT 2 (HOT BUS)

GREEN

YELLOW HP SUPPLY

TO RBCUs


R

CDS

R

R

R

NSV

R S

NBSELV

NSV

R

ASV

R

B

S

ABSELV

PBSELV

NSV R

SV SV

SV

1

B

R

NBSELV

RBCU

PRV

S

S

NOTE

S

ARV

CPIOM BCS

A

R X D C R

Training by Airbus

EMER BATT 1 (HOT BUS)

YELLOW 0

NSV

SV

ASV

SV SV

2

4X PRESSURE TRANSDUCER T

WHEEL 1

T

WHEEL 5

F

F

F

T

WHEEL 2

T

WHEEL 6

F

T

T

WHEEL 3

WHEEL 4

T

T

WHEEL 7

WHEEL 8


32

ACCUMULATOR AND CIRCUIT PRESSURIZATION / DEPRESSURIZATION Training by Airbus

ON

FIRE

PARK BRK

1

OFF

TO RBCUs YELLOW HP SUPPLY PRESSURE LIMITING VALVE R

FAULT OFF FF

28 VDC L/G

UP

OR

28 VDC

SSPC

ARV

R

CPIOM BCS

R

NSV

RBCU

PULL & TURN

R X D C R

PSI x1000

4

ON

NOTE

GREEN

PRV

R

NSV

R

4

0

R S

NBSELV

ASV

R

LEVER

S

ABSELV

PBSELV

NSV R

SV SV

SV

1

0

ACCU

S

NBSELV

YELLOW

S

R S

ACCU REINFLATE

NSV

SV

ASV

SV SV

2

F

T

WHEEL 1 DURING ACCUMULATOR REMOVAL, IF DAMAGED, RELEASE THE GAS PRESSURE: - REMOVE THE SCREW - TURN THE LOCK NUT IN THE CLOCKWISE DIRECTION

T

WHEEL 5

F

F

T

WHEEL 2

T

WHEEL 6

T

F

T

WHEEL 3

WHEEL 4

T

T

WHEEL 7

WHEEL 8


32

NORMAL BRAKING SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE

Z190

A FR54

FR60

B

C Page 330

A


32


NOTE

YELLOW NBSELV MANIFOLD

B YELLOW PLV

GREEN NBSELV MANIFOLD

C

GREEN PLV Page 331 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

32


NOTE B A BRAKES 1, 2 (3 , 4) SV MANIFOLD

A Page 332 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

32


C

NOTE

B

BRAKES 5, 6 (7, 8) SV MANIFOLD GEARBEAM

Page 333

C


32

ALTERNATE BRAKING SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE Z190

FR54

FR60


32

ALTERNATE BRAKING SYSTEM (COMPONENTS LOCATION) Training by Airbus

YELLOW BRAKE ACCUMULATOR

NOTE

GREEN BRAKE ACCUMULATOR

GREEN ABSELV MANIFOLD

YELLOW ABSELV MANIFOLD


32

PARKING BRAKE SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE Z190 Z190

FR54

FR60


32

PARKING BRAKE SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE

GREEN PBSELV

YELLOW PBSELV


32

NWS DESCRIPTION Training by Airbus PEDAL

PRIM/ SEC

XDCR UNIT

NOTE

LGERS

ADIRS AFDX NETWORK

HANDWHEEL CPIOM MON WSCS CRDC

A

CPIOM COM WSCS

CPIOM MON WSCS

CRDC

CRDC

A

SIDE 1

CPIOM COM WSCS

SIDE 1 SHOWN IN CONTROL, SIDE 2 SAME PRINCIPLE.

CRDC SIDE 2

GROUND

ROTATING VALVE (CHANGEOVER VALVE)

28VDC SERVO VALVE NWS SHUTOFF VALVE P R

S

NWS ISOLATION VALVE

RETURN CHECK VALVE

PRVs

RVDTs

ACTUATOR

BLEED VALVE FILL VALVE ACCUMULATOR

Page 338 HYDRAULIC BLOCK


32

OVERSTEERING DETECTION

NWS LOGIC AND CONDITIONS Training by Airbus

NOTE

STEERING WARNING

NWS AVAILABLE

TOWING LEVER NOT IN “TOWING” POSITION

A

STRESS LINE

OVERSTEER BRACKET

AND

AT LEAST ONE ENGINE MASTER LEVER AT “ON” POSITION

NWS DISCONNECT FAULT

72° 50°

10° 6° 30 50

100

150

Rudder NWS Demand Limit (°)

B

STEERING FAULT LIGHT (FLASHING)

YELLOW HYDRAULIC SYSTEM PRESSURIZED

PARK BRAKE ON

Steering Handwheel Maximum NWS Angle (°)

A

STEERING DISCONNECT PANEL

NLG AND MLG COMPRESSED (PROVIDED BY LGERS)

Aircraft Ground Speed (kt)

7 6 5 4 3 2 1 0

0 20 40 60 80 100 120 140 160 180 200

Aircraft Ground Speed (kt)

B

Take Off

Landing


32

NWS (INDICATING) Training by Airbus

NOTE

WHEEL STEER CTL :

YELLOW HYDRAULIC SYSTEM INDICATOR

1 2

NWS DISCONNECT Light

X 1000 PSI BRAKES 3.5 1

Y 0

NOSE WHEEL STEERING INDICATOR

Y SYS BRK

Y G

NORM ALTN EMER

G

1.6 0

120 1

Y

123 °C 2

120 3

Y

Y ACCU

3.5

NWS DISCONNECT sw

120 4

PSI

G SYS BRK NORM ALTN EMER

120 5

G

120 6

120 7

G

120 8

1.6 0

G ACCU

3.5

ENG A ICE

MAX SPEED 200KT

S

3

INDICATION Y N/W STEER

CONDITION THE SYSTEM IS NORMAL THE SYSTEM IS FAILED

F

PARKING BRAKE INDICATION The parking brake is set to ON and the pressure is effective on brakes.

NOTE: NOT ALL WARNING WILL BE SHOWN AT THE SAME TIME


32

STEERING SYSTEM (COMPONENTS LOCATION) Training by Airbus

MECHANICAL SHUT-OFF VALVE

NOTE ISOLATION VALVE

SERVO VALVE

S

P R

NWS SHUTOFF VALVE RETURN CHECK VALVE

BLEED VALVE NWS FILL ISOLATION VALVE VALVE ACCUMULATOR

PRVs



32

STEERING SYSTEM (COMPONENTS LOCATION) Training by Airbus NITROGEN FILLING PORT

NOTE

HYDRAULIC BLOCK

SERVO VALVE BLEED PORT

ROTATING VALVE

NLG

S

P R

NWS SHUTOFF VALVE

SERVO VALVE

RETURN CHECK VALVE

BLEED VALVE NWS FILL ISOLATION VALVE VALVE ACCUMULATOR

PRVs

ACTUATOR

RVDTs



32


NOTE

ROTATING SELECTOR VALVE ACTUATOR


32


A

NOTE

RVDT

ADJUSTMENT SCREW

Page 344

A


32

LGMS - BTMS Training by Airbus

AFDX NETWORK CPIOM

CPIOM

LGMS

LGMS

RBCU1

WRDC L1

CDS

NOTE

RBCU2

WRDC R1

WRDC L2

WRDC R2

BRAKE TEMPERATURE SENSOR

BTCM1

BTCM2

1

2

3

4

5

6

7

8

Page 345

BRAKE UNIT


32

LGMS - TPIS Training by Airbus

WHEEL ASSY PRESSURE SENSOR

WIRELESS SIGNAL (RADIO FREQUENCY)

NOTE

ROTATING INTERFACE UNIT (HUBCAP)

STATIC INTERFACE UNIT

WIRELESS SIGNAL (RADIO FREQUENCY)

Page 346 STATIC INTERFACE UNIT


32

LGMS - TPIS Training by Airbus AFDX NETWORK CPIOM

CPIOM

LGMS

LGMS

RBCU1

WRDC L1

2

5

6

CDS

RBCU2

WRDC R1

1

NOTE

WRDC NLG

LEFT

RIGHT

WRDC L2

WRDC R2

3

4

7

8


32

LGMS - BCF Training by Airbus LGERS

PCS

NOTE

AFDX NETWORK

HOT ON

115V SSPC MODULE

BRAKE FAN SWITCH

FAN MOTOR

CPIOM LGMS

ONE FAN PER MAIN WHEEL

Page 348

OPTIONAL SYSTEM


32

ATA 51 STANDARD PRACTICES AND STRUCTURES

MATERIALS - PRESENTATION FUNCTION / DESCRIPTION & LOCATION

Training by Airbus

NOTE GFRP CFRP MONOLITHIC CFRP SANDWICH TITANIUM ALLOY ALUMINUM ALLOY QFRP


51

FUSELAGE LAYOUT - PRESENTATION - FUNCTION / DESCRIPTION Training by Airbus

REAR FUSELAGE GE

4 LONG G SECTIONS

CENTER FUSELAGE

FOUR PANEL CONCEPT

NOTE

FRAME E CONCEPT PT

CFRP C FORWARD FUSELAGE NOSE FORWARD FUSELAGE

ALUMINUM TITANIUM

ALUMINUM

ALUMINUM Ω - SHAPED STRINGER

Page 350

RIGHT-HAND REAR LATERAL-PANEL


51

FUSELAGE LAYOUT - PRESENTATION - FUNCTION / DESCRIPTION Training by Airbus ALUMINUM

NOTE

CFRP PRESSURIZED SECTIONS

SKIN CFRP

Ω - SHAPED STRINGER

FRAME CFRP CABIN CROSSBEAM CARGO CROSSBEAM FRAME TITANIUM OR CFRP


51

ELECTRICAL STRUCTURE NETWORK (ESN) AND METALLIC BONDING NETWORK (MBN) Training by Airbus ESN

MBN

X X

X

X

FUNCTION

NOTE

ENSURES THE FUNCTIONAL CURRENT RETURN (GROUNDING) PROVIDE A CURRENT PATH FOR FAULT CURRENT AND ELECTROSTATIC CURRENT (BONDING) DISTRIBUTES A COMMON VOLTAGE REFERENCE

X

X

ENSURE LIGHTNING STRIKE PROTECTION

X

X

PROVIDE A CONNECTION TO THE EARTH WHEN THE A/C IS ON GROUND

X

X

PREVENT THE ACCUMULATION AND EVACUATE THE STATIC ELECTRICITY

METALLIC BONDING NETWORK AREA ELECTRICAL STRUCTURE NETWORK AREA


51

ESN Training by Airbus

ESN

+

ESN

ESN

NOTE USER

USER PVR

AC

DC

-

+

DC

+

AC

GENERATOR

BATTERY

ESN

-

COMPOSITE STRUCTURE

PVR

ESN DC

+

M

PVR

AC

ESN

GROUNDING CURRENT FLOW BONDING


51

ESN Training by Airbus EQUIPMENT RAIL

NOTE ESN NETWORK

FRAME

+

RACE WAY

SKIN

+

ESN CABLE/STRIP CABIN FLOOR BEAM SEAT TRACK

EX: LIGHT BONDING BRAID STRUT

PVR BAR ROLLER TRACK

FRAME

ALL THESE ELEMENTS ARE PART OF THE ESN

Page 354

CARGO FLOOR BEAM


51

MAINTENANCE - TOOLS Training by Airbus

DELAMINATION AND DISBOND DETECTION

NOTE FOR SANDWICH STRUCTURES

FOR MONOLITHIC STRUCTURES SINGLE TRANSDUCER (TRADITIONAL)

ARRAY TRANSDUCER

MANUAL TAP TEST OR AUTOMATIC TAP TEST ULTRASONIC INSPECTION

LINE TOOL

CAUTION

REFER TO THE NON-DESTRUCTIVE TESTING MANUAL FOR INSPECTION PROCEDURE AND LIMITATIONS


51

ATA 52 DOORS

COCKPIT DOOR LOCKING SYSTEM Training by Airbus AFDX NETWORK

NOTE

BUZZER CKPT DOOR LOCKG SYS

OFF OF FF

CDSS

FWS

CMS

CKPT DOOR CTLR

PRESSURE SENSOR

LATCHES STRIKES WITH MECHANICAL CATCHES DOOR HANDLE

1

2

3

4

5

6

7

8

9

0

CKPT DOOR UNLOCK OPEN FAULT

2

#

LOCK CONTROL AND STATUS DOOR POSITION

NORM LOCK

Page 356

KEYPAD EYPA


52

DOORS (INDICATING) Training by Airbus

DOOR / OXYGEN ECAM SD PAGE

DOOR

DOORS / SLIDES FAP PAGE

NOTE

OXYGEN

AVIONICS _ _ _ _ _ SLIDE 1

CAPT 1 2 0 0 PSI

X

1 SLIDE F/O

SLIDE 2

2 SLIDE

SLIDE 3

3 SLIDE

_ _ _ _ _ AFT CARGO

SLIDE 4

4 SLIDE

1 5 0 0 PSI

CAB V / S 0 FT / MIN

RAIN RPLNT LEVEL NORM

THE DOOR IS CLOSED AND LOCKED THE DOOR IS NOT LOCKED

THE INFORMATION IS NOT VALID

DOOR : LOCKED SLIDE : ARMED AND READY ATTENTION DOOR : UNLOCKED


52

PAX DOOR MECHANISM Training by Airbus

GEAR BOX

NOTE INNER HANDLE

CATCH OUTER HANDLE

DRIVE SHAFT ESCAPE SLIDE ARMING LEVER

INNER HANDLE LATCH LEVER

OUTER HANDLE

LATCH LEVER

FLAP ANTI LOWERING LEVER

DRIVE SHAFT TORQUE SHAFT

OUTER HANDLE Page 358

GIRT BAR


52

PAX DOOR MECHANISM Training by Airbus

NOTE

ESCAPE SLIDE ARMING LEVER

MECHANICAL INDICATORS INNER HANDLE

LATCH BRACKET DOOR FRAME LATCH LEVER

LATCH SHAFT LATCH LEVER

OUTER HANDLE

DRIVE SHAFT

LATCH LEVER

ANTI LOWERING LEVER TORQUE SHAFT

LOCK STOP DRIVE SHAFT GIRT BAR

LOCKING CAM


52

PAX DOOR MECHANISM Training by Airbus ESCAPE SLIDE ARMING LEVER

NOTE UPPER LINK LEVER

INNER HANDLE LATCH LEVER

OUTER HANDLE

DOOR FRAME INNER VIEW

LATCH LEVER

ANTI LOWERING LEVER

DRIVE SHAFT TORQUE SHAFT

GIRT BAR

LOWER LINK LEVER DRIVE SHAFT TORQUE SHAFT (WEIGHT COMPENSATION) ANTI LOWERING LEVER

WEIGHT COMPENSATION ADJUSTMENT MECHANISM


52

SLIDE ARMING SYSTEM Training by Airbus

NOTE

GIRT BAR CONTROL SHAFT

LOCKING FITTING

SLIDE DISARMED

SLIDE ARMED

SLIDE ARMED AND DOOR OPENED IN EMERGENCY


52

SLIDE ARMING SYSTEM Training by Airbus

NOTE

PRESSURE GAUGE

SLIDE SELECTOR LEVER

PRESSURIZED GAS BOTTLE ACTUATION LEVER

ACTUATION LEVER

ACTUATOR

ARMED MODE

DISARMED MODE

DOOR DAMPER AND EMERGENCY-OPENING ACTUATOR


52

SLIDE ARMING SYSTEM Training by Airbus SAFETY EXHAUST PLUG

NOTE SAFETY PIN

DOOR EMERGENCY OPERATION ACTUATOR IN ACTIVE MODE

DOOR EMERGENCY OPERATION ACTUATOR DEACTIVATED


52

CARGO DOOR MECHANISM Training by Airbus

LOCK HANDLE

NOTE FLAP

LATCH HANDLE

DOOR LATCHED AND LOCKED

DOOR UNLATCHED AND UNLOCKED

SPRING SYSTEM

CATCH SYSTEM

SEQUENCE MECHANISM


52

CARGO DOOR MECHANISM Training by Airbus FLAG

NOTE

LOCKING SHAFT LATCHING SHAFT

INDICATOR WINDOW

LATCHING SHAFT

STOP LEVER INTERLOCK LEVER

INTERLOCK TERLOCK GUIDE DE FITTING ON FUSELAGE

LATCHING SHAFT END

LOCKING SHAFT INTERLOCK ROD

ADJUST FITTING

FLAG

FLAG

LEVER

INTERLOCK MECHANISM (DOOR CLOSED)

LOCKING CAM DOOR OUTER SKIN

DOOR LOCKED AND LATCHED

DOOR UNLOCKED AND LATCHED

DOOR UNLOCKED AND UNLATCHED


52

CARGO DOOR - NORMAL OPERATION & MANUAL OPERATION Training by Airbus

CPIOM PCS

HMCA-Y

LGERS

ENG NOT RUNNING AFDX NETWORK

LATCHING HANDLE DOWN

EMP-Y

WOW

CPIOM

CRDC

P

NOTE

DSCS ELEC POWER SUPPLY A/C ON GROUND NO ENGINE RUNNING DOOR SILL LATCHES UP LATCHING HANDLE DOWN

CARGO DOOR OPERATION POSSIBLE

CARGO DOOR OPERATION PANEL UP POSITION

DOOR SILL LATCH

CDCV LOWER DECK CARGO DOOR ACTUATOR

UNLATCH PROX SENSOR


52

CARGO DOOR - NORMAL OPERATION Training by Airbus

CPIOM HMCA-Y

NOTE EMP-Y ACTIVATION

AFDX NETWORK CPIOM CRDC

DSCS

RESERVOIR YELLOW SYSTEM FWD LOWER DECK CARGO DOOR ACTUATOR EMP-Y P

SYSTEM MANIFOLD

AUX PUMP VALVE OPEN SV

FWD CDCV CLOSE SV

FWD CARGO DOOR OPERATION PANEL

Page 367 TO AFT CARGO DOOR


52

CARGO DOOR - MANUAL OPERATION Training by Airbus

IN CASE OF: -NO HYDRAULIC POWER SOURCE (EMP; GROUND CART) -DSCS, AFDX NETWORK, CRDCS UNAVAILABLE.

RESERVOIR YELLOW SYSTEM

HYDRAULIC AUXILIARY PUMP

NOTE

FWD LOWER DECK CARGO DOOR ACTUATOR EMP-Y PINOP

MANUAL LEVER

GEAR BOX SYSTEM MANIFOLD

AUX PUMP VALVE OPEN SV

FWD CDCV CLOSE SV

DR DRILLING MACHINE MA TO AFT CARGO DOOR

FWD CARGO DOOR OPERATION PANEL


52

DSCS (ARCHITECTURE) CDS OXYGEN X

_ _ _ COCKPIT EMER CKPT 1 8 5 0 PSI

X

SLIDE

X 1L

X 1R

SLIDE

X 2L

X 2R

SLIDE

X 3L

X 3R

X

Screen Caution Context Help Off

Doors/Slides

Aircraft-Wide Adjustment

___ AVIONICS _ _ _ _ _

Training by Airbus

CIDS

DOOR

Legend Door: Locked Slide: Armed and Ready

SLIDE

CPIOM

Attention

_ _ _ _ _ FWD CARGO

Door: Unlocked

X BULK CARGO _ _ _ _

SLIDE

X X 4L

X 4R

SLIDE

CAB V / S

SLIDE

SLIDE

FT / MIN

RAIN RPLNT LEVEL NORM

DOORS PAGE

NOTE

CPCS

66 33 55 00

_ _ _ _ _ AFT CARGO

CIDS

Cabin Status

Music

Pre Ann

Lights

Doors/ Slides

Temp

Water/ Waste

Smoke Seat Detect Setting

Cabin Status

Pax Call

Lights

FAP AFDX NETWORK

CRDC

CARGO DOOR ACTUATION SYSTEM

CPIOM DSCS

DSCS

PROXIMITY SENSORS

ESCAPE HATCH

AVIONIC ACCESS

FWD AND AFT AVIONICS INTERNAL ACCESS DOOR

PAX DOOR

CARGO DOOR

BULK CARGO DOOR


52

DSCS - RESIDUAL PRESSURE WARNING Training by Airbus COMMAND

CIDS

EVAC

CAPT &

HORN OFF

PURS

EVAC

NOTE

ON CAPT CA APT A PT

AFDX NETWORK WOW CPIOM DSCS

LGERS BUZZER

DIP ESCAPE SLIDE ARMING LEVER

ASPSU DIP

OUTER HANDLE D O H S

DRIVE SHAFT

TORSION BAR S L S

DOOR HANDLE POSITION

DIFFERENTIAL P E PRESSURE SWITCHES S S

CARGO DOOR

STATIC LINE FROM STATIC PORT

FROM STATIC PORT

SLIDE DISARMED

ASPSU SUPPLY: -GROUND SERVICE POWER MODE -DIRECTLY BY GROUND POWER UNIT

GIRT BAR


52

ATA 25 / 50 EQUIPMENT & FURNISHING AND CARGO & ACCESSORY COMP.

CABIN PANELS Training by Airbus

NOTE

UPPER ATTACH POINT (HOLDER) PANELS PIN LEVER

SLIDE CASE

ATTACHING DEVICE

SLIDE CASE

PIN

LEVER

ATTACHING DEVICE INSULATION BLANKET ATTACH

LOWER ATTACH POINT (FASTENER)


25 / 50

CABIN PANELS Training by Airbus MATCH BOX BRACKET

NOTE FASTENER

LEVER

SLIDE CASE PINS

CEILING MODULE OHSC/PSC MODULE LATERAL

SIDEWALL MODULE

OHSC/PSC MODULE CENTER

CEILING MODULE OHSC/PSC MODULE LATERAL

SIDEWALL MODULE

SLIDE CASES

ATTACHING DEVICE TOP VIEW Page 372 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

25 / 50

CABIN PANELS Training by Airbus

NOTE

PASSENGER SERVICE CHANNEL OVERHEAD STOWAGE COMPARTMENT

FIXED BRACKETS

ALLEN KEY

PASSENGER SERVICE CHANNEL EQUIPMENTS BRACKET

SLIDE CASE

LIGHT COVER PANEL


25 / 50

GAIN POWER SUPPLY MANAGEMENT Training by Airbus ELMF

DEU - B

NOTE

GNC (RH)

AFDX NETWORK

GAIN

RCCB

EPDS

GAIN

GAIN

DOOR ZONE 3

DOOR ZONE 4

GAIN

GAIN

GALLEY FEEDERS

DOOR ZONE 1

GAIN CIDS DIRECTOR

GAIN

DOOR ZONE 2

GAIN

CAM

1 2

GNC (LH)

DEU - B


25 / 50

GAIN ELECTRICAL SUPPLY Training by Airbus

NOTE GAIN GALLEY FEEDER

CTB

GALLEY CONTROL PANEL

RCCB

EPDS

DOOR ZONE 1

GAIN


25 / 50

ESCAPE SLIDES PACK ASSEMBLY DESCRIPTION Training by Airbus UPPER PACKBOARD LATCH ASSEMBLY

PACKBOARD ASSEMBLY (WITH ESCAPE SLIDE/RAFT AND INFLATION SYSTEM)

NOTE

A LATCH LOCK LATCH LEVER

UPPER DOOR MOUNTING BRACKET

A

B

LOWER MOUNTING HOOK (INSTALLED ON THE DOOR FRAME)

PACKBOARD ASSEMBLY (WITH ESCAPE SLIDE/RAFT AND INFLATION SYSTEM)

DECORATIVE COVER

LOWER MOUNTING BRACKET

B


25 / 50

ESCAPE SLIDES DEPLOYMENT Training by Airbus 04 ESCAPE SLIDE/RAFT DEPLOYED AND INFLATED

NOTE FUSELAGE

GIRT

GIRT RELEASE CABLE GIRT BAR GIRT GROMMET WEBBINGS

GIRT CORD LOOPS

PARACHUTE PINS

PARACHUTE PIN

GIRT CORD GIRT RELEASE CABLE HANDLE


25 / 50

ESCAPE SLIDES INFLATION Training by Airbus PULLEY ACTUATION MECHANISM

PRESSURE GAUGE INFLATION VALVE/ REGULATOR

NOTE

GAS RESERVOIR

SAFETY PIN

ACTUATION MECHANISM SAFETY PIN HOLE

ACTIVATING CABLE

A SAFETY PIN

UPPER PACKBOARD LATCH ASSEMBLY

A LOWER MOUNTING BRACKET

PACKBOARD TRAY

RELEASE MECHANISM

LOWER MOUNTING BRACKET

SAFETY PIN

GIRT BAR


25 / 50

CARGO LOADING SYSTEM (ARCHITECTURE) Training by Airbus

NOTE

FW D

AF T

MONITORED SILL LATCH (2)

PDU SPRING LOADED

PROXIMITY SWITCH FOR LOCKABLE CENTER LATCH

FWD/AFT JOYSTICK COMMAND

PROXIMITY SWITCH FOR XZ LATCH

INSIDE CONTROL PANEL

PDU SELF ERECTING

SYSTEM READY

CMS

SYSTEM POWER ON/OFF CARGO ARG CONTROL BOX

JOYSTICK COMMAND

OUTSIDE CONTROL PANEL


25 / 50

CARGO LOADING SYSTEM (CLS) DESCRIPTION Training by Airbus

ROLLER

OPTICAL SENSOR

FWD CARGO COMPARTMENT

NOTE AFT CARGO COMPARTMENT

SPRING LOADED PDU (TRACKS) ROLLER

OPTICAL SENSOR

SELF ERECTING PDU (BALL MAT)

CENTER LATCH

BALL TRANSFER UNIT

TRANSPORT ROLLER

ENTRANCE GUIDE SELF ERECTING PDU SPRING LOADED PDU

ROLLER TRACK

SPLITTER GUIDE (BALL MAT)

LATERAL GUIDE (BALL MAT)


25 / 50

CLS LATCHES DESCRIPTION Training by Airbus

NOTE FWD CARGO COMPARTMENT

DOOR SILL LATCH (5)

Z

X

YZ LATCH

Y

FWD CARGO SHOWN AS EXAMPLE AFT CARGO IS SIMILAR

LATCHES POSITION SHOWN AS EXAMPLE

XZ LATCH

Page 381

CENTER LATCH


25 / 50

CLS SILL LATCHES DESCRIPTION Training by Airbus ANTI ROLL OUT DEVICE


PROXIMITY SWITCH ANTI ROLL OUT DEVICE

DOOR SILL ROLLER

LATCH PAWL

NOTE

DOOR SILL ROLLER

DOOR-SILL LATCH UNIT TOP VIEW

LATCH PAWL

DOOR-SILL LATCH UNIT DOWN VIEW

AFT CARGO COMPARTMENT Page 382 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

25 / 50

CLS (CONTROLS) Training by Airbus

NOTE

FW D

AF T


SYSTEM READY LAMP

TOGGLE SWITCH

LAMP TEST

INSIDE CONTROL PANEL

SWITCH ON/OFF

CARGO CONTROL BOX

PRIORITY ALWAYS GIVEN TO OUTSIDE CONTROL PANEL

JOYSTICK COMMAND

FWD CARGO SHOWN AS EXAMPLE AFT CARGO IS SIMILAR

OUTSIDE CONTROL PANEL


25 / 50

ATA 27 FLIGHTS CONTROLS

PRIMARY FLIGHT CONTROL SYSTEM (PFCS) ACTUATION Training by Airbus

NOTE

E1

E1

P3 P2

P2

P1

P2 P3 S2

S1

S3 S2

P1 S1

P3 S3

P2 P3

P1

S2 S3

S1

E1

SPOILERS

S2 S3

P1

P3

S1

S3

E1

INBOARD AILERON OUTBOARD AILERON

E1 E3

E1: EMER 1 BUS E2: EMER 2 BUS E3: AC 1 BUS

M

M

THS ACTUATOR

P3

CONVENTIONAL SERVO-CONTROL

P1

EHA

E2

E2

E2

P2

S1 S2

RUDDER

ELEVATORS

EBHA

RECONFIGURATION ARROW

S3

P1

P2

P2

P3

S1

S2

S2

S3


27

F/CTL CONTROLS Training by Airbus F/CTL

F/CTL

211VM

PRIM 1

SEC 1

PRIM 3

SEC 3

FAULT

FAULT

FAULT

FAULT

OFF

OFF

OFF

OFF

PRIM 2

SEC 2

FAULT

FAULT

OFF

OFF

F/CTL PANEL

212VM

NOTE

F/CTL PANEL

SIDE STICK UNIT

SIDE STICK UNIT

115VM

PITCH TRIM NOSE DN

RUDDER PEDALS

RUDDER PEDALS NOSE UP N GND SPLRS LRS ARMED

RET

SPEED BRAKE

RET

RUDDER TRIM NOSE SE L

1/2

FULL

1/2

NOSE NO R

0

0

1

1

2

2

3

3

RESET FLAPS

FULL

FULL

SPEED BRAKE LEVER

FULL

Page 385

FLAPS LEVER

PITCH TRIM & RUDDER TRIM


27

F/CTL (INDICATING) Training by Airbus

SD FLIGHT CONTROL PAGE 14 1 2

F / CTL

13 RUDDER TRIM R10.0 °

PRIM 1 2 3

SLATS 1

2

12

FLAPS 1 2

SEC 1 23

3 4

11

PITCH TRIM

10

0.8 °UP

1 : F/CTL COMPUTERS 2 : ELEVATOR POSITION 3 : PITCH TRIM MOTORS 4 : ELEVATOR ACTUATORS 5 : SPOILER POSITION 6 : SLATS / FLAPS MOTORS 7 : AILERON ACTUATORS

8 FLAPS INNER OUTER

7

COMPUTER

POWER SOURCE AVAILABLE

COMPUTER

POWER SOURCE UNAVAILABLE COMPUTER DATA NOT VALID

6

OUTBOARD FLAP INBOARD FLAP SLAT

T . O THS FOR 35.0 %

S 2

F

8 : AILERON POSITION 9 : PITCH TRIM POSITION 10 : PITCH TRIM INDICATION 11 : RUDDER POSITION 12 : SLATS / FLAPS COMPUTERS 13 : RUDDER TRIM POSITION 14 : RUDDER ACTUATORS

POWER SOURCE AVAILABLE POWER SOURCE UNAVAILABLE ACTUATOR FAILURE

9

SLATS

5

NOTE

NOTE

35.0 %

THS POSITION Page 386

FLAP LEVER POSITION


27

PFCS ELECTRICAL BACKUP SYSTEM Training by Airbus

NOTE TO LEFT INBOARD AILERON SERVOCONTROL

BCM

BPS


27

PFCS ELECTRICAL BACK UP (COMPONENTS LOCATION) Training by Airbus

RUDDER SERVOCONTROL (FOR EXAMPLE)

NOTE

BCM CONNECTOR R

BPS

BCM


27

LATERAL FUNCTION : ROLL DESCRIPTION Training by Airbus SERVO-LOOP PRINCIPLE AFS SPD

SPD

---

TRUE

MAG

MAG

HDG

ADIRU

METER

TRK

ALT

FPA

---

A/THR

ALT

NOTE

VALVEs XDCRs

A/C ATTITUDE

AP2 DN

LOC

RGAU

V/S

FCRM/EM

-----

7000 FD

AP1

TO AND FROM COMPUTERS

APPR

CTL PANEL

ACTUATOR

FMC 1 2

3

PRIM1

SEC1

ROLL

PRIM2

SEC2

PRIM3

SEC3

S

AILERON & SPOILER ACTUATORS TO BCM

SFCC 2

CR

CR

P2 P3 S2 S3

5

6

7

XD

1

4

Y

XD

2

3

1

P2

P1

S2

S1

P3

ROLL SPOILERS P2 P1 P3 P2

S3

OUTBOARD INBOARD AILERON AILERON

S2

S1

S3

S2

EHA EBHA


27

LATERAL FUNCTION : YAW DESCRIPTION Training by Airbus

AFS TRUE

SPD

MAG

---

V/S

MAG

HDG

RUDDER SERVO-LOOP PRINCIPLE

TRK

METER

ALT

FPA

---

AP1

TO AND FROM COMPUTERS

V/S

-----

7000 FD

UP

AP2 DN

LOC

A/THR

ALT

APPR

CTL PANEL

ADIRU

FCRM/EM

ACTUATOR

A/C ATTITUDE

1 2

3

PRIM1

SEC1

ROLL

S

XDCR

XDCR

RUDDER TRIM

PRIM2

SEC2

PRIM3

SEC3

NOSE L

NOSE R

RESET

RUDDER ACTUATORS

YAW TO BCM

P2/S2 P3/S3 E

TRIM SENSOR XDCRs

PFTU TRIM SENSOR

M EM M EM

TRIM

S2 S3

TO BCM

XDCR

YAW

PDFU

S

NOTE

XDCRs

RGAU

FMC

VALVEs

P3

S3

P1

S1

P2

S2

XDCR

P INO

E

P3

S3

P1

S1

P2

S2

XDCR

XDCR

NORMAL CONFIGURATION: - SERVO-CONTROL ACTUATORS: ACTIVE MODE - EHA: DAMPING MODE

FAILURE CONFIGURATION: - SERVO-CONTROL ACTUATORS: DAMPING MODE - EHA: ACTIVE MODE


27

FLT CTL (COMPONENTS LOCATION) Training by Airbus

NOTE

PEDAL

INTERCONNECTION ROD

PFTU

PEDAL TRANSDUCERS

PDFU Page 391 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

27

VERTICAL FUNCTION : PITCH DESCRIPTION Training by Airbus SERVO-LOOP PRINCIPLE TO AND FROM COMPUTERS ADIRUs

NOTE

VALVEs

FCRM/EM

XDCRs

RGAUs

ACTUATOR A/C ATTITUDE

AFS MACH

SPD

SPD

---

TRUE

MAG

MAG

HDG

HDG

V/S

TRK

METER

ALT

FPA

---

V/S

-----

7000 FD

AP1

LOC

EMCU1

AP2

A/THR

ALT

APPR

CTL PANEL FMC

PRIM1

1 2

EMCU3 M

SEC1

ELEVATOR AND THS ACTUATOR

3

M

P1

P3

S1

S3

WHEN EMCU3 IS ACTIVE, RECONFIGURATION IS P3 TO P1 TO S3 TO S1

TO BCM

TO BCM PITCH

PRIM2

SEC2 E

S PITCH TRIM NOSE DN

NOSE UP

MANUAL TRIM ORDER

XDCR

XDCR

E

XDCR

XDCR

PRIM3

SEC3

P1

P2

P2

P3

S1

S2

S2

S3


27

SPEED BRAKES AND GROUND SPOILERS DESCRIPTION Training by Airbus RA TRANSCEIVER 1

ADIRU RGAU

LGERS 2

NOTE

3

A/C ATTITUDE AFDX NETWORK PRIM1

SEC1 AILERON & SPOILER ACTUATORS

GND SPLRS LRS ARMED

RET

RET

SPEED BRAKE

1/2

1/2

PRIM2

SPEED BRAKES AND GROUND SPOILER

SEC2

FULL

FULL

USED AS GROUND SPOILERS SFCC

PRIM3 1

3

1

5 7

SEC3

2

4 6

2

DROOP PANEL

SPOILERS

FLAPS

XDCR

CONTROLLED GAP Page 393

ADHF


27

BACKUP SYSTEM COMPUTER DESCRIPTION Training by Airbus SIDE STICK UNIT

ELECTRICAL BACKUP SYSTEM BCM

C O M P U T A T I O N

RUDDER PEDALS PITCH GYROMETER YAW GYROMETER

XDCRs

PFTU

E X E C U T I O N

NOTE SERVO-LOOP ACTUATORS AND SENSORS

POWER SUPPLY

M EM

BPS

M EM

VALID P2 VALID S2 AND Y

CPIOM PRIM 1

ON

FCDC 2

1

3

2

PITCH TRIM NOSE DN

NOSE UP

PITCH TRIM SWITCHES

VALID P1 VALID P3 VALID S1 VALID S3 BPS ACTIVE

AND

P

R

ACTIVATION INHIBITION SIGNALS

SEC 1

2

3

TEST COMMAND

BCM

BCM ACTIVATED

AND

POWER INHIBITION SIGNALS

BACKUP SYSTEM ACTIVE

BPS


27

ACTUATOR MODES PRINCIPLE

S

EHSV

ACTIVE/ DAMPING SOLENOID FCRM

Training by Airbus

R

P

MANUAL RELIEF VALVE

S HARD/SOFT DAMPING SOLENOID

NOTE

VISUAL INDICATOR

ACCUMULATOR

MODE SELECTOR VALVE

ACTIVE MODE MODE SELECTOR VALVE

MODE SELECTOR VALVE

Page 395

HARD DAMPING MODE

SOFT DAMPING MODE


27

SERVO CONTROL DESCRIPTION Training by Airbus RUDDER SERVOCONTROL

COM / MON CONNECTORS FCRM

INBOARD AILERON SERVOCONTROL

MODE SELECTOR VALVE BCM CONNECTOR MODE SELECTOR VALVE TRANSDUCER

NOTE

COM / MON CONNECTORS

RAM PRESSURE TRANSDUCER SOFT / HARD DAMPING SOLENOID VALVE ACTIVE / DAMPING SOLENOID VALVE

ACCUMULATOR

VISUAL INDICATOR SERVOVALVE TRANSDUCER ACTIVE / DAMPING SOLENOID VALVE

FCRM

MANUAL DISCHARGE

EHSV

EHSV HP HYDRAULIC PORT

GREASE NIPPLE


27

EHA DESCRIPTION Training by Airbus RUDDER EHA

AILERON EHA

NOTE COM / MON CONNECTORS

ELECTRONIC MODULE FILLING SOLENOID VALVE

POWER CONNECTOR

DIRECT DRIVE SOLENOID VALVE

MOTOR - PUMP ASSY

ACCUMULATOR FILLING SOLENOID VALVE

ACCUMULATOR

VISUAL INDICATOR ELECTRONIC MODULE

DIRECT DRIVE SOLENOID VALVE


27

THS ACTUATOR DESCRIPTION Training by Airbus

UPPER LOAD SENSING PIN EMCU3 EMCU1 FILL PLUG

NOTE

PSU1

DRAIN PLUG

MECHANICAL STOP

PRIMARY LOWER LOAD-PATH ATTACHMENT

FILL PLUG

LOWER LOAD SENSING PIN

NUT ASSEMBLY PSU3

SECONDARY LOWER LOAD-PATH ATTACHMENT

SCREW JACK

DRAIN PLUG

SERVICE WITH TURBINE OIL MIL-PRF-7808 ONLY

LOWER STOP

Page 398

NO BACK BRAKE OIL INDICATOR


27

SLAT SYSTEM DESCRIPTION 0

0

1

1

2

2

3

FULL

Training by Airbus

SLAT/FLAP CONTROL LEVER FLAPS

DROOP NOSE

3

NOTE

SLAT PCU

FULL

FPPU

SENSORS

TSU

TSU

DIFFERENTIAL HYDRAULIC GEARBOX MOTOR

M

SFCC SLAT CHANNEL

POB

SLAT 2

1

MCE

POB

VALVE BLOCK

2

230VAC EMER 1

SLAT 4

YELLOW HYDRAULIC SUPPLY

SLAT 6

WTB APPU

GEARED ROTARY ACTUATOR : DRIVE STATION BEVEL GEARBOX

Page 399

SENSOR © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

27

SLAT SYSTEM (COMPONENTS LOCATION) Training by Airbus

MCE

NOTE

SLAT PCU EHSV

HYDRAULIC MOTOR

TSU

FPPU

HYDRAULIC MANIFOLD

SOLENOID VALVES

ELECTRICAL MOTOR HYDRAULIC PRESSURE-OFF BRAKE DIFFRENTIAL GEARBOX

ELECTRICAL POWER-OFF BRAKE


27


DROOP NOSE KINEMATICS RETRACTED POSITION

NOTE ACTUATOR LEVER DRIVE LINK HINGE ARM

DEFLECTED POSITION

DROOP NOSE TRANSMISSION

BEVEL GEARBOX

HINGE ARM 5

HINGE ARM 4

HINGE ARM 3 HINGE ARM 2

HINGE ARM 1 BEVEL GEARBOX

ARY GEARED ROTARY TOR ACTUATOR

Page 401 TORQUE LIMITER INDICATOR TO


27


NOTE TORQUE LIMITER INDICATOR SLAT LAT EXTENSION

SLAT TRACK

GEARED ROTARY ACTUATOR

GEAR RACK

7 AT SL

6 AT SL

PINION

MAINTENANCE MANUAL RELE RELEASE DEVICE

Page 402

WING TIP BRAKE KE


27

FLAP SYSTEM DESCRIPTION GEARED ROTARY ACTUATOR: DRIVE STATION

0

0

1

1

2

3

BEVEL GEARBOX

FULL

2

FLAPS

FLAPS CONTROL LEVER

3

FULL

Training by Airbus

NOTE

SENSOR

SFCC FLAP CHANNEL

ADGB DFPPU

ELEC MOTOR POB

M C E

1

2

230VAC EMER BUS SENSORS

WTB FPPU

STL

OTSSU

SPPU SPPU

LSDS

SPPU

INBOARD FLAP

HYDRAULIC MOTOR

LSDS

DIFFERENTIAL GEARBOX HYDRAULIC MOTOR

SPPU POB

OUTBOARD FLAP

VALVEMCE BLOCK

POB

VALVE BLOCK

FLAP PCU YELLOW HYDRAULIC SUPPLY

GREEN HYDRAULIC SUPPLY Page 403 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

27

FLAP SYSTEM (COMPONENTS LOCATION) Training by Airbus

FLAP KINEMATICS PRINCIPLE GEARED ROTARY ACTUATOR

NOTE

FLAP (SECTION)

FIXED SUPPORT FLAP RETRACTED GEARED ROTARY ACTUATOR LEVER DRIVE STRUT

FLAP LEVER PIVOT POINT

DROOP PANEL PRINCIPLE

DROOP PANEL HINGE

LINE

FIXED FIXE SUPPORTS SUPPO

INBOARD FLAP

Page 404 DRIVE STRUT

LEVER


27


FLAP PCU

NOTE HYDRAULIC MOTOR MANIFOLDS SOLENOID VALVES

HYDRAULIC MOTOR HYDRAULIC MOTOR

PRESSURE-OFF BRAKE DIFFERENTIAL GEARBOX

PRESSURE-OFF BRAKE


27


TOP VIEW (LH WING)

NOTE

F W D

MCE POWER-OFF BRAKE

N2 TIO ) A T P LA ES RIV RD F D TO NBOA (I

BOTTOM VIEW (LH WING) ELECTRICAL MOTOR

UPPER ATTACHMENTS POWER-OFF BRAKE

N3 TIO P) A T S LA IVE D F DR OAR O T TB (OU ELECTRICAL MOTOR

DIFFERENTIAL GEARBOX

DFPPU DIFFERENTIAL GEARBOX

DFPPU

LOWER ATTACHMENTS

RIGGING WINDOW


27


DRIVE STATION 1

NOTE DRIVE STATION 2 OUTPUT

DRIVE STATION 3

INB

GEARED RED ROTARY ACTUATORS 3&4

R OA

DF

LAP

GEARED ROTARY ACTUATOR ACTUATO 1 INPUT

OUTPUT

P

DRIVE STATION 4

D

AR

BO

A FL

GEARED ROTARY ACTUATOR 2

UT

INPUT

O

NON DRIVING TION 5 STATION OUTPUT TORQUE LIMITER L INDICATOR


27

FLAP SYSTEM (COMPONENTS LOCATION) SOLENOID CONNECTORS

Training by Airbus

DRIVE STATION 1

NOTE DRIVE STATION 2

DRIVE STATION 3

WING TIP BRAKE

INB

O

D AR

FLA

P

SYSTEM TORQUE LIMITER

MANUAL RELEASE DEVICE

A

P

T-BEVEL GEARBOX

DRIVE STATION 4

O U

TB

O

A

R

D

FL

TORQUE LIMITER INDICATOR

MOVING DAMPER

DOWN DRIVE GEARBOX

FUSE TENSION FUS

LVDT

ACCUMULATOR

TORQUE LIMITER INDICATOR


27

ATA 35 OXYGEN

CREW OXYGEN STORAGE AND DISTRIBUTION SYSTEM DESCRIPTION PAX A U T O

Training by Airbus

TO MASK DISTRIBUTION LINE

OXYGEN OXYGE CREW SUPPLY

LOW PRESSURE SWITCH

SYS ON OFF

RH OXYGEN COMPARTMENT PRESSURE MANIFOLD RELIEF VALVE

M

CREW SHUT-OFF VALVE

A/C SKIN

MASK MAN ON

NOTE

ON-OFF

RH ODI LP

TEMPERATURE TRANSDUCER

HP TRANSDUCER

TEST PORT

CPIOM CRDC

VENTURI VENT HOLE

HP

CYLINDER SWITCH OPEN

AIR FLOW

FROM FILL PANEL HP PORT

OSCM

CRDC AFDX NETWORK

CPIOM

CDS

OXYGEN

CAPT

OSCM

NOTE: RIGHT SIDE SYSTEM SHOWN LEFT SIDE SYSTEM SYMMETRICAL

CAPT 1850 REGUL PR F/O 850 REGUL PR

F/O

DOOR/OXY PAGE

PSI LO PSI LO


35

OXYGEN SYSTEM (CONTROLS & INDICATING) Training by Airbus

NOTE

OVERBOARD DISCHARGE INDICATOR MASK MAN ON O

OXYGEN PAX

A U T O

CREW SUPPLY

OXYGEN RESET FAULT

SYS ON

OFF

ON


35

FLIGHT CREW OXYGEN SYSTEM INDICATIONS Training by Airbus OXYGEN CYLINDER PRESSURE VALUE :

DOOR / OXY SD NORMAL PAGE

DOOR

OXYGEN

DOOR / OXY SD INDICATIONS

CAPT 1 8 5 0 PSI SLIDE 1

1 SLIDE F/O

NOTE

1 8 5 0 P S I GREEN - P >P2

1 8 5 0 PSI

50 PSI

OXYGEN

AMBER - If P < P2 with associated :

OXY CAPT(F/O) BOTTLE PRESS LO (WD) REGUL PR LO AMBER - Invalid value or

SLIDE 2

SLIDE 3

2 SLIDE

3 SLIDE

CAPT 1 8 5 0 PSI REGUL PR LO CAB V / S 0

SLIDE 4

4 SLIDE

P

8 5 0 PSI F/O REGUL PR LO

FT / MIN

loss of indication (failure, cylinder closed...).

XX PSI

P1 P2

= Mean cylinder presure (temperature compensated) = Dispatch pressure threshold = Low pressure threshold

RAIN RPLNT

HALF FRAME CONDITION : P2 < P < P1

LEVEL NORM

850 PSI

CAPT & F/O LEGEND :

CAPT &

F/O

WHITE - Normal indication

CAPT &

F/O

AMBER - If

P < P2 - or On ground only when

AMBER - On ground

- In flight if oxygen cylinder 8 5 0 P S I GREEN pressure REGUL PR LO LABEL :

REGUL PR LO AMBER - If

REGUL PR LO

LPS detects low pressure warning (< 47 psig) - or LP crew shut off valve is closed

comes up


35

FLIGHT CREW OXYGEN DISPENSING PURGE VALVE

Training by Airbus

FLOW BLINKER INDICATOR TEST/RESET P/BSW

T-SHAPE BUMP

FLAPS

NOTE AUDIO MANAGEMENT UNIT 2

REGULATOR INFLATABLE HARNESS INFLATION TABS

OXYGEN SUPPLY HOSE

3RD OCCUPANT MASK STOWAGE BOX

MICRO MICROPHONE CABLE CA

F/O MASK STOWAGE BOX

LP VALVES

REGULATOR SELECTOR KNOB 100%

R

NORM

RH CREW OXYGEN STOWAGE COMPARTMENT

LP SUPPLY VALVE EQUIPPED WITH PRESSURE SWITCH

NOTE: RIGHT SIDE SYSTEM SHOWN LEFT SIDE SYSTEM SYMMETRICAL

100%

RM NO

EME

EMER


35

FLIGHT CREW OXYGEN COMPARTMENT DESCRIPTION Training by Airbus

INTEGRATED CYLINDER ASSEMBLY

CREW SHUT-OFF VALVE

HP FILL PORT CAP STORAGE TEMPERATURE TRANSDUCER

NOTE

ON/OFF LEVER SAFETY PIN HP SAFETY DISCHARGE

LP OUTLET

RELIEF SYSTEM PORT HP TRANSDUCER

OXYGEN FILL SYSTEM PORT OXYGEN SUPPLY SYSTEM PORT VENTILATION PORT

DUAL MANIFOLD (OPTIONAL) LP RELIEF VALVE

DIRECT READING HP GAUGE

TEST PORT

OXYGEN COMPARTMENT

CYLINDER SWITCH OPEN 1


CYLINDER SWITCH OPEN 2

FILL PANEL (OPTIONAL) F/O OXYGEN SUBSYSTEM

FILL PORT

CAPT OXYGEN SUBSYSTEM

PRESSURE INDICATOR


35

FLIGHT CREW OXYGEN SYSTEM MAINTENANCE Training by Airbus

NOTE

BLOWOUT DISC (NO OXYGEN DISCHARGED)

INDICATOR (OXYGEN DISCHARGED)

OVERBOARD DISCHARGE INDICATOR

DIRECT READING PRESSURE GAUGE

OPTIONAL FILL PANEL

OXYGEN CYLINDER


35

PASSENGER OXYGEN SYSTEM Training by Airbus

CDS FMS

CPCS

NOTE DOOR/OXY PAGE

AFDX NETWORK ATMOSPHERIC PRESSURE TRANSDUCER

FWD CRDC MASK MAN ON

OXYGEN PAX P

EMER 115VAC

A U T O

POWER RELAY

OXYGEN CREW SUPPLY

SYS ON

RESET FAULT

OFF

ON

POWER RELAY CPIOM 1

1

...

...

X

X

OSCM

POWER SUPPLY BRIDGING POWER RETURN RELAY POWER SUPPLY MONITORING

AFT CRDC

PARTIAL L/H LATERAL SIDE ONLY SHOWN. SAME PRINCIPLE FOR ENTIRE PASSENGER SYSTEM.

POWER SUPPLY MONITORING


35

ATA 38 WATER AND WASTE

POTABLE WATER SYSTEM DESCRIPTION Training by Airbus

CABIN CONSUMERS

NOTE

CABIN FLOOR MAIN SUPPLY LINE

M

SUPPORT DEPRESS VALVE

AIR MANIFOLD

RECIRCULATION LINE NO STEP

NO STEP

NO STEP

HUMIDIFIER SHUT-OFF VALVES 1 TO 6

NO STEP

NO STEP

NO STEP

NO STEP

NO STEP

M

NO STEP

M

NO STEP

ATA 21

FWD DRAIN VALVE

WATER PUMP

NO STEP

WATER OUTLET PORT

NO STEP

NO STEP

FWD DRAIN LINE

RECIRCULATION PORT M

NO STEP

NO STEP

RECIRCULATION PORT

BYPASS DRAIN VALVE

WATER OUTLET PORT

MAIN DEPRESS VALVE

POTABLE WATER TREATMENT MODULE

M

FILL/DRAIN VALVE

A/C SKIN FWD DRAIN NIPPLE

NO STEP

OPTIONAL

DOOR SWITCH

M


38

WATER / WASTE FAP PAGE Training by Airbus

AUTO FLUSH FUNCTION ACTIVE

NOTE


38

POTABLE WATER INIDCATION PANEL (PWIP) Training by Airbus

NOTE

PWIP SERVICING, VALVE CLOSED PRE-SELECTION ENABLE AT PWIP

PWIP SERVICING, END OF FILLING

PWIP SERVICING, FILLING

PWIP DESINFECTION START PAGE


38

POTABLE WATER SYSTEM OPERATION CIDS

Training by Airbus

POTABLE WATER SYSTEM

NOTE

PWQT

PWQT

NO STEP

NO STEP

NO STEP

NO STEP

NO STEP

NO STEP

NO STEP

NO STEP

CAM NO STEP

NO STEP

NO STEP

CIDS DIRECTOR

NO STEP

NO STEP

FAP

LH WATER TANK

NO STEP

NO STEP

NO STEP

RH WATER TANK

PWS 1

PWSP

2

UV-WATER TREATMENT MODULE

PWIP

AFDX NETWORK

CMS

LGERS

POTABLE WATER PUMP FILL/DRAIN VALVE

WOW

FWD DRAIN VALVE BYPASS/DRAIN VALVE MAIN DEPRESS VALVE

DOOR SWITCH

SUPPORT DEPRESS VALVE OPEN/CLOSED

HUMIDIFICATION VALVES 1 TO 6


38

POTABLE WATER SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE FR93 VALVE-BYPASS / DRAIN 80MB

FR82

5020MB RESTRICTOR-POTABLE WATER

120MB PUMP-POTABLE WATER

100MB MODULE-TREATMENT, POTABLE WATER


38

POTABLE WATER SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE

FILL / DRAIN VALVE

FR93

01

QUANTITY TRANSMITTER

PWSP POTABLE WATER TANK

FR82

PWIP

DIP STICK

01

PWSP SHOWN WITHOUT DOOR


38

WASTE SYSTEM (ARCHITECTURE) Training by Airbus

LH TOILET CABIN SIDE FLUSH VALVE FLUSH CONTROL MODULE

WATER/WASTE FAP PAGE

FLUSH SWITCH

CMS FWS CPCS LGERS

A F D X

RINSE VALVE

VACUUM GENERATOR

CIDS DIRECTOR

N E T W O R K

NOTE

TOILET ASSEMBLY

WASTE CTL UNIT FLD CLM

1 ...

GALLEY ASSEMBLY

X

GWDU VCVA

VTS CAN BUS

VTS

FLUSH SWITCH

RINSE VALVE

GWDU CONTROLLER SKIN FULL SENSOR

VCVA

FLUSH VALVE

1 ...

WOW

1 2

OPEN/CLOSED DOOR STATUS DOOR SWITCH

WASTE SERVICE PANEL

VACUUM GENERATOR

FLUSH SWITCH

X

RINSE VALVE

FLUSH CONTROL MODULE

FLD CLM WASTE CTL UNIT

FLUSH VALVE

TOILET ASSEMBLY1

...

X

RH TOILET CABIN SIDE


38

WASTE TANK ASSEMBLY AND ASSOCIATED EQUIPMENT

Training by Airbus

WASTE INLET WAS

VACUUM CONTROL L VALVE ASSY

NOTE

FROM TOILET ASSY OR GWDU

WASTE CONTROL UNIT

OVERBOARD CHECK VALVE

WASTE SEPARATOR FILTER

RINSE NOZZLE

INTERNAL SKIN QUANTITY SENSOR MESHES

VACUUM GENERATOR

A/C SKIN

ACTUATION UNIT

RE M OV E

DEBRIS UNDER INNER FLAPPER

R E MO VE

DEBRIS UNDER INNER FLAPPER

F T OPEN THIS HANDLE FIRST

DOOR SWITCH S PATE N0 G.098.0 G 098 027 7 U.S. U .S. PAT PATENT ATENT N0. G.098.027

RINSE LINE NIPPLE WITH CAP ACTUATION UNIT

N0 G.245.131 2 55.131 131 U S PATENT N0. U.S. G.245.1 G .245 .131

OVERBOARD VENT PORTS (BLOWER OUT)

WASTE DRAIN VALVE

WASTE SERVICE VALVE WITH CAP RINSE LINE NIPPLE WITH CAP

WASTE SERVICE PANEL


38

TOILET ASSEMBLY - GWDU - DRAIN VALVES Training by Airbus LAVATORY

GALLEY

FLUSH SWITCH FLUSH CONTROL MODULE

S

CONTROLLER

RINSE VALVE

RINSE VALVE

THERMOSTAT

M

GWDU

M

DRAIN VALVE

NOTE SENSOR SINK

S

FLUSH VALVE

SHUT-OFF VALVE

SHUT-OFF VALVE

MANUAL SHUT-OFF VALVE MANUAL VACUUM DRAIN SHUT-OFF VALVE VALVE

VCVA

FLUSH VALVE FLUSH SWITCH

FROM OTHER LAVATORIES OR GALLEYS

POTABLE WATER DRAIN VALVE (DIAPHRAGM TYPE)

VACUUM GENERATOR

MANUAL CONTROL A/C SKIN Page 424 DRAIN MAST


38

WASTE SYSTEM (COMPONENTS LOCATION) Training by Airbus

5300MG TANK-MODULE WASTE

A

NOTE

FR93

FR82

341MG (440MG)

VALVE-WASTE DRAIN TANK-MODULE WASTE 5135MG 5301MG (5136MG)

VALVE-VACUUM CONTROL ASSY

CHECK VALVEOVERBOARD 5305MG CTL UNIT-VACUUM (5306MG) GENERATOR 351MG (450MG)

A Page 425 © Airbus SAS 2014. All rights reserved. Confidential and proprietary document.

38

WASTE SYSTEM (COMPONENTS LOCATION) Training by Airbus

NOTE WASTE TANK ASSEMBLY

WASTE CONTROL UNIT WASTE INLET

WASTE TANK MODULE WASTE INLET (FROM VACUUM WASTE LINE)

RINSE NOZZLE

90°-ELBOW

WASTE TANK

AIR OUTLET (TO OVERBOARD VENT LINE (BLOWER IN) )

WASTE TANK RINSE LINE

RINSE NOZZLE

ATTACHMENTS

WASTE SEPARATOR WASTE OUTLET (TO WASTE DRAIN LINE)

WASTE TANK ASSEMBLY


38

A350 Avionics

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