A350 Airframe

(1)

Training by Airbus

POWERPLANT

ATA 28 - FUEL

ATA 26 - FIRE PROTECTION SYSTEMS

ATA 49

-

AIRBORNE AUXILIARY POWER

ATA 70 - STANDARD PRACTICES - ENGINES

ATA 36 - PNEUMATIC

ATA 21 - AIR CONDITIONING

ATA 47 - INERT GAS SYSTEMS

ATA 30 - ICE & RAIN PROTECTION

P. 428

P. 449

P. 473

P. 487

P. 520

P. 530

P. 590

P. 593

(2)

NOTE

FUEL SYSTEM LAYOUT

M = Main Engine Feed Pump S = Stand - by Engine Feed Pump

CTR TK X-FEED VALVES JETTISON VALVE

ENG 2 REFUEL COUPLINGS REFUEL ISOLATION VALVE V E N T / S U R G E WING TANK INLET VALVE R WING TANK DEFUEL/JETTIS ON VALVE CENTRE TANK INLET VALVE APU LP VALVE APU APU ISOLATION VALVE FUEL SCAVENGE VALVE JETTISON VALVE V E N T / S U R G E L WING TANK WING TANK INLET VALVE LP VALVE ENG 1

ATA 28

FUEL Page 428

(3)

NOTE

F

U

E

L

F

U

E

L

CTR TK L CROSSFEED A STBY MAIN L TK STBY MAIN R TK R TK XFR L TK XFR FEED CROSSFEED B R A U T O ON FAULT N O FAULT ON FAULT ON FAULT MAN FAULT MAN FAULT OFF FAULT OFF FAU F F LTLL OFF FAULT OFF FAU F F LTLL OFF FAULT OFF FAULT OFF FAULT OFF FAULT OFF FAULT OFF FAU F F LTLL OFF FAULT OFF FAU F F LTLL ON OPEN ON OPEN ON OPEN ON OPEN

FUEL SYSTEM (CONTROLS)

FUEL JETTISON

ACTIVE ARM ON OPEN N O OPEN ON ON JETTISON

FUEL PUMPS - CROSSFEED VALVES - TRANSFERS

RESET PANEL RESET 232VM 1 2 W V U FMC-B SLATS 2 FQMS 2 FLAPS 2 RESET 231VM 1 2 F E D FMC-A FMC-C SLATS 1 FLAPS1 FQMS1 Page 429

(4)

NOTE

FUEL SYSTEM (INDICATING)

ECAM MEMO FUEL SD PAGE CROSSFEED OPEN CROSSFEED OPEN DEFUEL IN PROGRESS GND XFR IN PROGRESS JETTISON IN PROGRESS JETTISON IN PROGRESS REFUEL IN PROGRESS REFUEL PNL DOOR OPEN

REFUEL PNL DOOR OPEN

At least one crossfeed valve is open

Manual transfer from the left (right) wing tank to the center tank is in progress

The door of the refuel panel is open and an engine is running

The door of the refuel panel is open Refueling is in progress

Fuel jettison is in progress during the climb and the approach phases

Fuel jettison is in progress Ground transfer is in progress Defueling is in progress

At least one crossfeed valve is open during the takeoff phase

L(R) TK XFR IN PROGRESS

FUEL

ALL ENG FF FU FU FU 1 2 KG KG/MIN 160 14 14ºC ºC 9360 9360 2460 4350 8750 4350 ALL ENG APU CDS PERMANENT DATA

40300

33.5 GWCG

222200

32

00 ET

:

5:45:04 GPS

+5

°C

ISA

+5

KG KG

FOB

%

GW

°C

SAT

°C

TAT

32

00 ET

:

5:45:04 GPS

+5

°C

ISA

+5

°C

SAT

°C

TAT

Page 430

(5)

NOTE

FUEL SYSTEM (INDICATING)

OVERFLOW INDICATION

Appears when an overflow in the left or right wing surge tank is detected. The indication disappears, when the overflow is no longer detected

Appears when a low level in the left and/or right wing tank is detected LO LVL INDICATION

Engine 1(2) is running Engine 1(2) is not running ENGINE NUMBER INDICATION

The total fuel quantity on board the aircraft The value accuracy is degraded

Some fuel in at least one tank is not usable FUEL ON BOARD INDICATION

Appears when a fuel leak is detected LEAK INDICATION

CENTER TANK - FUEL QUANTITY INDICATION

The fuel quantity in the center tank is within a normal range The value accuracy is degraded

The fuel in the center tank is not usable

WING TANK - FUEL TEMPERATURE INDICATION When at least one of the temperature sensors of the wing

tank is immersed, the fuel temperature is displayed on the FUEL SD page.

When the temperature sensors of the wing tank are not immersed, the fuel

temperature is not displayed.

The fuel temperature is within a normal page The fuel temperature is above 53°C, or below - 40°C

ALL ENGINE FUEL FLOW (ALL ENG FF) INDICATION Indicates the fuel flow of all engines

The ALL ENG FF accuracy is degraded, because the fuel flow accurary of at least one engine is degraded

APU INDICATION

Fuel is not fed to the APU

Fuel is fed to the APU Fuel is abnormally fed to the APU Fuel is abnormally not fed to the APU

JETTISON INDICATION

Jettison is active. The jettison valves are open Jettison is actived, but the jettison failed

Either jettison valve is abnormally open (TBC)

WING TANK - FUEL QUANTITY INDICATION

The fuel quantity in the wing tank is within a normal range The value accuracy is degraded

The fuel quantity in the left wing tank is not balanced with the fuel quantity in the right wing tank

Some of the fuel in the wing tank is not usable The fuel in the wing tank is not usable

WING TANK TO CENTER TANK TRANSFER INDICATION

Fuel gravity transfer from the wing tank to the center tank. The ECAM displays the L(R) TK XFR IN PROGRESS memo.

Abnormal fuel gravity transfer from the wing tank to the center

(6)

NOTE

REFUEL / DEFUEL / TRANSFER SYSTEM (CONTROL / INDICATING)

INTEGRATED REFUEL PANEL

HI LVL

REFUEL/ DEFUEL VALVES

INCREASE DECREASE PRESELECT 88888888 PRESELECT (PFQ) FAULT OVERFLOW NORMAL BATTERY POWER SUPPLY 88888888 ACTUAL (FOB) 8888888888888888 STATUS 8888888888888888 MAN REFUEL XFR DEFUEL AUTO REFUEL OFF MODE SELECT 88888 88888 88888 R. WING OPEN SHUT R.WING CTR CTR L. WING L.WING 100 000 Kg NO BA 65 000 Kg FOB > PRESELECT AUTO REFUEL END 15000 35000 15000 SHUTOFF TEST TEST NORMAL TE NO SHUTDOWN NORMAL APU EMERGENCY SHUTDOWN SH NO S ALTN GAUGING ALTN NORMAL AL NO 1 2 ₃ ₄ 5 6 7 8 9 10 REFUEL/DEFUEL VALVE:

- OPEN: WHEN THE MODE SELECT SWITCH IS SET TO MANUAL REFUEL, DEFUEL OR TRANSFER, THE VALVE CAN BE SELECTED OPEN.

- SHUT: THE USUAL POSITION OF THE SWITCHES, THE APPLICABLE VALVES WILL OPEN WHEN THE MODE SELECT SWITCH IS SET TO AUTO REFUEL. 1.

REFUEL PANEL INDICATOR (RPI):

- THIS SHOWS THE FUEL QUANTITY IN EACH TANK, THE TOTAL ACTUAL FEED ON BOARD, THE PRESELECTED FUEL QUANTITY AND THE TYPE OF FUEL OPERATION OR A SIMPLE FAULT MESSAGE.

2.

POWER SUPPLY

- NORMAL: THE ELECTRICAL POWER CAN BE EXTERNAL POWER, OR FROM THE ENGINE OR APU GENERATORS.

- BATTERY: THE ELECTRICAL POWER COMES FROM THE AIRCRAFT BATTERY. 3.

SHUT OFF TEST (HIGH LEVEL TEST)

- TESTS THE HI LVL. INDICATION AND VALVE OPERATION. 4.

OVERFLOW

- AN AMBER LIGHT ILLUMINATES IF A TANK OVERFLOW OCCURS. 5.

FAULT

- AN AMBER LIGHT ILLUMINATES IF A FAULT OCCURS. 6.

APU EMERGENCY

- SHUTDOWN: THE APU IS SHUTDOWN (USED IF A FUEL SPILLAGE OR OVERFLOW OCCURS).

7.

PRESELECT

- CONTROLS THE QUANTITY OF FUEL SET FOR AN AUTO REFUEL. THE QUANTITY SELECTED IS SHOWN ON THE RPI.

8.

MODE SELECT

- SELECT THE TYPE OF FUEL OPERATION REQUIRED. WHEN NOT IN USE THE SWITCH POSITION IS OFF.

9.

HI LVL >

- A BLUE LAMP ILLUMINATES IF THE RELATED TANK HIGH LEVEL IS REACHED. 10.

(7)

NOTE

REFUEL / DEFUEL / TRANSFER SYSTEM (CONTROL / INDICATING)

Text 1 Text 2 TEST FAILED TEST OK SHUTOFF TEST CKPT REFL FAULT CKPT REFUEL END CKPT REFUEL CKPT RFL IDLE XFR FAULT XFR XFR IDLE DEFUEL FAULT DEFUEL DEFUEL IDLE MAN RFL FAULT MAN REFUEL MAN REFUEL IDLE AUTO REFL FAULT AUTO REFUEL END AUTO REFUEL AUTO RFL IDLE OFF MODE CROSSFEED8SHUT CROSSFEEDASHUT CROSSFEEDSSHUT DEFUEL VLV SHUT CTR PMP OFF DEFUEL VLVS SHUT RTK PMP OFF LTK PMP OFF CTR PMPS OFF RTK PMPS OFF LTK PMPS OFF FOB<PRESELECT CTR OTY>TARGET RTK OTY>TARGET LIK OTY>TARGET TANKS>TARGET FOB>PRESELECT ALL TANKS HILVL DEFUEL VLV OPEN DEFUEL VLVS OPEN FQI FAULT CTR VLVS SHUT RTK VLV SHUT LTK VLV SHUT CKPT TRANSFER CTR VLV OPEN RTK VLV OPEN LIK VLV OPEN CTR HI LVL FAULT RTK HI LVL FAULT LTK HI LVL FAULT HI LVL FAULTS CTR PMP ON RTK PMP ON LKT PMP ON R OVERFLOW L OVERFLOW R OVERFLOW FAULT L OVERFLOW FAULT R JTSN VLV OPEN L JTSN VLV OPEN STATUT Messages Text 1 Text 2 Page 433

(8)

NOTE

WATER DRAINS (SERVICING)

INDIRECT WATER DRAIN VALVE

REMOTE DIRECT WATER DRAIN VALVE GRAVITY PURGER TOOL

SUCTION PURGER TOOL

FOR THE INDIRECT WATER DRAIN VALVE, IN CASE OF LOW FUEL QUANTITY, IT IS RECOMMENDED TO DRAIN WATER WITH A SUCTION PROCEDURE AND NOT A GRAVITY PROCEDURE

ENG 2

OVERPRESSURE PROTECTOR DISK-WHITE CROSS

WATER DRAIN VALVE HOUSING PRIMARY SEALING MECHANISM INLET HOLES INLET HOLES ENG 1 DIRECT WATER DRAIN VALVE PRIMARY SEALING MECHANISM INDIRECT WATER DRAIN VALVE HOUSING

INLET PIPE WATER DRAIN VALVE HOUSING PRIMARY SEALING MECHANISM Page 434

(9)

NOTE

A B A B CRDC TWDC CPIOM MEASUREMENT MANAGEMENT MEASUREMENT MONITOR CPIOM MEASUREMENT MANAGEMENT MEASUREMENT MONITOR CPIOM MEASUREMENT MANAGEMENT MONITOR CPIOM MEASUREMENT MANAGEMENT MONITOR SIDE 1 SIDE 2 OVERFLOW/LOW LEVEL

FUEL USED A/C ATTITUDE BLOCK FUEL

FQMS ENG 1 IN-TANK ENG2 EQUIPMENT IRP AFDX NETWORK Electronic Control Box (ECB) Propulsion Control System (PCS) REFUEL ON END ON END UF E L F U E L CTR TK STBY MAINL TK STBY MAINR TK R TK XFR A U T O ON FAULT ON FAULT ON FAULT N O FAULT OFF FAULT OFF FAU FFLTLL OFF FAULT OFF FAU FFLTLL FUEL JETTISON ACTIVE ARM ON OPEN N O OPEN ON ON Air data Inertial Reference System (ADIRS) Flight Management System (FMS) HI LVL

INCREASE DECREASE PRESELECT 88888888 PRESELECT (PFQ) FAULT OVERFLOW L Y POWER SUPPLY 88888888 ACTUAL (FOB) 8888888888888888 STATUS 8888888888888888 MAN REFUEL XFR DEFUEL AUTO REFUEL OFF MODE SELECT 88888 88888 88888 R. WING OPEN SHUT R.WING CTR CTR L. WING L.WING 100 000 Kg 65 000 Kg FOB > PRESELECT AUTO REFUEL END 15000 35000 15000 SHUTOFF TEST TEST NORMAL TE NO SHUTDOWN NORMAL APU EMERGENCY SHUTDOWN SH NO S ALTN GAUGING ALTN NORMAL AL NO CDS FUEL ALL ENG FF FU FU FU OVFLW OVFLW LEAK 1 2 KG KG/MIN 1 6 0 1 4 X Xº C º C LO LVL LO LVL 9 3 6 0 9 3 6 0 2 4 0 0 4 3 5 0 ALL ENG8 7 5 0 4 3 5 0 XX APU JETTISON JETTISON FUEL PAGE

FQMS - FUEL QUANTITY MANAGEMENT SYSTEM (ARCHITECTURE)

FQMS SIDES 1 & 2 - ONE SIDE ACTIVE

(10)

NOTE

ENG

1 ENG2

CAPACITIVE PROBES PROBE DUAL

TEMPERATURE UNITS POINT LEVEL SENSORS

FUEL PROPERTIES MEASUREMENT UNITS TWDC 1 TWDC 3 TWDC 2 FUNCTION - FUEL HEIGHT FUNCTION - FUEL HEIGHT - FUEL TEMPERATURE FUNCTION - PRESENCE OR ABSENCE OF FUEL AT CRITICAL LEVELS FUNCTION

- UPLIFTED FUEL TEMPERATURE - UPLIFTED FUEL DENSITY - UPLIFTED FUEL PERMITTIVITY

F P M U F P M U (18) (1) (2) (2) (17) (6) (2) (2) (2) (17) (2) (6)

FQMS - FUEL QUANTITY MANAGEMENT SYSTEM (DATA ACQUISITION)

(11)

NOTE

FQMS _{MAIN FUEL PUMP}WING TANK CENTER TANK_{& WING TANK}

STANDBY FUEL PUMPS ENGINE FEED SYSTEM VALVE ACTUATORS STANDBY PUMPS CENTER

PUMPS _STANDBYMAIN

CENTER PUMPS STDBY PUMPS LPSOV MANUAL CONTROL CROSSFEED VALVES AUTOMATIC CONTROL CROSSFEED VALVES MANUAL CONTROL PUMP PRESSURE SWITCHES FEEDBACK PUMP PRESSURE SWITCHES FEEDBACK AFDX NETWORK AT AT CRDC CRDC RCCB RELAYS PRIMs/SECs SSPCs 1 FAULT FIRE 1 FAULT FIRE F U E L F U E L CROSSFEED A L TK STBY MAIN R TK R TK XFR L TK XFR CROSSFEED B AUT O ON FAULT ON FAULT OFF FAULT OFF FAU FFLTLL OFF FAULT OFF FAU FFLTLL ON OPEN ON OPEN ON OPEN ON OPEN

ENGINE FEED SYSTEM (ARCHITECTURE)

(12)

NOTE

ENGINE FEED - CENTER TANK PUMPS

P AND AND FLAPS FLAPS OFF FAULT OFF FAULT MAN FAULT MAN FAULTAUL OFF FAULT OFF FAULT

CENTER TANK FUEL PUMP ELEMENT

CENTER TANK FUEL PUMP DRAIN PLUG

AT ZERO ON ON CENTER TANK FUEL PUMP RUNNING CENTER TANK FUEL PUMP RUNNING CONTINUOUSLY FQMS AUTOMATIC CONTROL MANUAL CONTROL

GFI VISUAL INDICATOR

MAN SFCCs CENTER TANK FUEL PUMP PUSH-BUTTON CENTER TANK FUEL PUMP PUSH-BUTTON CENTER TANK FUEL PUMP MANUAL OVERRIDE FLAPS LEVER POSITION (230VAC) (154VAC) FFSU ENG 1 NOT EMPTY CENTER FUEL TANK

CENTER TANK REAR FACE

(13)

NOTE

ENGINE FEED SYSTEM (FFSU LOCATION)

Z120 A FIXED FREQUENCY SUPPLY UNIT FIXED FREQUENCY SUPPLY UNIT A Page 439

(14)

NOTE

ASSOCIATED MAIN PUMP

LOW PRESSURE

WING TANK STANDBY FUEL PUMP RUNNING

WING TANK MAIN FUEL PUMP PUSH-BUTTON WING TANK STANDBY FUEL PUMP PUSH-BUTTON AND OR STBY OFF FAULT OFF FAU F F LTLL MAIN OFF FAULT OFF FAU F F LTLL ON MANUAL CONTROL

ENGINE FEED - MAIN & STANDBY PUMPS

MAIN PUMP OPERATION

WING TANK MAIN FUEL PUMP RUNNING ON EMERGENCY ELECTRICAL CONFIGURATION WING TANK STANDBY PUMP WING TANK MAIN PUMP LANDING PHASE (FLAPS/SLATS EXTENDED, AIRSPEED BELOW 175 KTS,

LANDING GEAR DOWN) WING TANK

MAIN FUEL PUMP PUSH-BUTTON AND AND MAIN OFF FAULT OFF FAU F F LTLL MANUAL CONTROL LH SHOWN RH SIMILAR ENG 1 P M S

L WING REAR SPAR

PROTECTIVE CAGE

STANDBY PUMP NORMAL OPERATION

FQMS AUTOMATIC TEST ON ON GROUND FWS FLIGHT PHASE 1 OR 2 * INITIAL PERIOD OF 5 MINUTES

STANDBY PUMP AUTOMATIC OPERATION

WING TANK STANDBY FUEL PUMP RUNNING * PREFLIGHT OR TAXI-OUT WING TANK STANDBY FUEL PUMP PUSH-BUTTON

AND

STBY OFF FAULT OFF FAU F F LTLL WING TANK FUEL PUMP DRAIN PLUG Page 440

(15)

NOTE

ENGINE FEED SYSTEM (LP, CROSSFEED, SCAVENGE VALVES LOGIC)

ON LOW PRESSURE_{SHUT-OFF VALVE}

OPEN NOT RELEASED ENGINE MASTER SWITCH FIRE PUSH-BUTTON AND 1 FAULT FIRE MANUAL CONTROL MANUAL CONTROL ON ON CROSSFEED VALVES OPEN CROSSFEED VALVES PUSH-BUTTONS CROSSFEED A CROSSFEED B ON OPEN ON OPEN ON OPEN ON OPEN

PRIM/SEC AUTOMATIC CONTROL EMERGENCY ELECTRICAL CONFIGURATION CROSSFEED A CROSSFEED B ON OPEN ON OPEN ON OPEN ON OPEN FUEL SCAVENGE VALVE OPEN CENTER FUEL TANK

BECOMES EMPTY IN FLIGHT WING FUEL TANKS REACH LOW LEVEL

OR

FQMS AUTOMATIC CONTROL

MECHANICAL VISUAL POSITION INDICATOR (LOCKED IN CLOSED POSITION

FOR DEACTIVATION)

CROSSFEED VALVES OPERATION LP VALVE OPERATION

SCAVENGE VALVE OPERATION

(16)

NOTE

ENGINE FEED SYSTEM (LP, CROSSFEED VALVES LOCATION)

B VALVE-CROSSFEED B VALVE-CROSSFEED A LEFT ENGINE FEED GALLERY RIGHT ENGINE FEED GALLERY

WING FRONT SPAR (OUTBOARD OF ENGINE)

FUEL LP VALVE

A

(17)

NOTE

APU FEED SYSTEM (LOGIC)

ON

MANUAL CONTROL

PRESSED APU MASTER

SWITCH APU FUEL VENT

PUSH-BUTTON APU FIRE PUSH-BUTTON

NOT RELEASED

NOSE LANDING GEAR GROUND SERVICE PANEL

APU EMERGENCY SHUTDOWN SWITCH NOT SHUTDOWN NOT SHUTDOWN IRP APU EMERGENCY SHUTDOWN SWITCH ELECTRONIC CONTROL BOX FUEL DEMAND OR AND

APU ISOLATION VALVE CLOSED APU LOW PRESSURE VALVE CLOSED APU ISOLATION VALVE OPEN

APU LOW PRESSURE VALVE OPEN

CRDCs AND RELAYS AUTOMATIC CONTROL APU FEED LINE

DAMAGE WIRES ONE OR BOTH

DAMAGED

APU FUEL PUMP ON

APU FUEL PUMP OFF

AND AND AND ENG 1 ENG2 ENG 1 ENG2

APU FEED LINE DAMAGE WIRES

ONE OR BOTH DAMAGED APU FEED LINE

DAMAGE WIRES NOT DAMAGED FUEL PRESSURE FROM ENGINE FEED GALLERY INSUFFICIENT Page 443

(18)

NOTE

APU FEED SYSTEM (COMPONENTS LOCATION)

DRAIN PLUG APU FUEL PUMP

CTR TK REAR FACE

(19)

NOTE

BLOCK FUEL FMS CRDC REFUEL, DEFUEL, TRANSFER SYSTEM VALVE ACTUATORS

AUTOMATIC CONTROL OF THE FQMS IN:

- AUTOMATIC REFUEL

PROTECTIONS FROM THE FQMS IN: - AUTOMATIC/MANUAL REFUEL - PRESSURE/SUCTION DEFUEL - GROUND TRANSFER

AUTOMATIC REFUEL INITIATED FROM THE ICP

OPERATOR ACTION FROM THE IRP IN CASE OF: - AUTOMATIC REFUEL - MANUAL REFUEL - PRESSURE DEFUEL - SUCTION DEFUEL - GROUND TRANSFER SSPCs HI LVL

INCREASE DECREASE PRESELECT 88888888 PRESELECT (PFQ) FAULTOVERFLOW L Y POWER SUPPLY 88888888 ACTUAL (FOB) 8888888888888888 STATUS 8888888888888888 MAN REFUEL XFR DEFUEL AUTO REFUEL OFF MODE SELECT 88888 88888 88888 R. WINGOPEN SHUT R.WING CTR CTR L. WING L.WING 100 000 Kg 65 000 Kg FOB > PRESELECT AUTO REFUEL END 15000 35000 15000 SHUTOFF TEST SHUTDOWN NORMAL APU EMERGENCY SHUTDOWN SH NO S ALTN GAUGING ON END FLIGHT GRAVITY TRANSFER IRP FQMS R TK XFR ON FAULT TRANSFER

PUSH- BUTTON STATUS

L TK XFR

ON

FAULT

REFUEL - DEFUEL SYSTEM (ARCHITECTURE)

“READY TO REFUEL” LIGHT

MECHANICAL VISUAL POSITION INDICATOR (LOCKED IN CLOSED POSITION

FOR DEACTIVATION) AFDX NETWORK

(20)

NOTE

REFUEL – DEFUEL - TRANSFER SYSTEM (COMPONENT LOCATION)

REFUEL COUPLINGS AND ISOLATION VALVE

MANUAL OVERRIDE

L WING TK INLET VALVE ACTUATOR

A B DIFFUSERS DIFFUSERS A B VALVE 2 - INLET, CTR TK

VALVE 2 - SURGE PRESS RELIEF, CTR TK

VALVE 1 - INLET, CTR TK

VALVE 1 - SURGE PRESS RELIEF, CTR TK

(21)

NOTE

JETTISON SYSTEM (ARCHITECTURE)

DUAL POWER SUPPLY ACTUATOR

MOTOR

VALVE POSITION INDICATOR POSITION INDICATOR SWITCH

MECHANICAL VISUAL POSITION INDICATOR (LOCKED

IN CLOSED POSITION FOR DEACTIVATION)

SINGLE POWER SUPPLY ACTUATOR - ONE MOTOR

- MECHANICAL VISUAL POSITION INDICATOR FOR DEACTIVATION

DUAL POWER SUPPLY ACTUATOR: - TWO MOTORS

- MECHANICAL VISUAL POSITION INDICATOR

- DEACTIVATION WITH A LOCKING TOOL

SINGLE POWER SUPPLY ACTUATOR ARM ON ON ACTIVE ON OPEN ON OPEN AFDX NETWORK OPEN JETTISON STOPPED MANUALLY

JETTISON FINAL GROSS WEIGHT

JETTISON STARTED MANUALLY FQMS AUTOMATIC CONTROL (START/STOP) CRDC JETTISON SYSTEM VALVE ACTUATORS FMS SSPCs FQMS Page 447

(22)

NOTE

JETTISON SYSTEM (COMPONENTS LOCATION)

L WING REAR SPAR CTR TK REAR FACE

CTR TK JETTISON VALVE L WING TK JETTISON VALVE

(23)

NOTE

ENGINE / APU / MLG FIRE PROTECTION OVERVIEW

APU AREA MLGB AREA ENG 1 AREA UP TO 6 ZONES Fire Detector CM APU - MLGB B CM ENG 1B CM APU - MLGB A CM ENG 1A Fire Extinguishing Bottle ENG 2 AREA UP TO 6 ZONES CM ENG 2B CM ENG 2A CPIOM J21 LOOP A ENG 1 APU MLGB CPIOM J24 LOOP B ENG 2 APU MLGB CPIOM J23 LOOP A ENG 2 CPIOM J22 LOOP B ENG 1 Loop B Loop A AFDX Communication

ATA 26

FIRE PROTECTION SYSTEMS

(24)

NOTE

SDS OVERVIEW

CIDS DIRECTOR SDF LAV G LAV E LAV B LAV C LAV A LAV D LAV F LAV H LAV I S/D S/D S/D S/D S/D S/D S/D S/D S/D DEU - B DEU - B DEU - B DEU - B ICP RESET SWITCHES DISCHARGE PUSHBUTTONS INDICATIONS LAVATORIES CCRC AFT LDCC FWD LDCC MAIN AVIONICS CONNECTIVITY RACK IFEC FCRC VCS FWS CDS CMS _WARNINGCABIN S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D S/D SDS 2 SDS 1 FEDC FEDC AFDX NETWORK Page 450

(25)

NOTE

ENGINES - APU - MLG FIRE PROTECTION (CONTROL & INDICATING)

MAINTENANCE PANEL-NLG FLT INT SVCE INT COCKPIT CALL APU SHUT OFF APU FIRE FLTLL INTINT E INT COCKPIT CALL SVCE INT F I R E F I R E AGENT 1 AGENT 2 FIRE

TEST ENG 1 APU AGENT 1 AGENT 2 ENG 2 AGENT DISCH SQUIB DISCH SQUIB FIRE FI FREREE DISCH SQUIB FIRE F FIREREE PUSH DISCH SQUIB DISCH SQUIB OFF ON OFF ON 135 VM ENG START CRANK IGN START NORM 2 FAULT FIRE 1 FAULT FIRE

CARGO SMOKE

AGENT TO FWD _{AGENT TO AFT}

MLG BAY 222 VM DISH DISH SMOKE SMOKE DISH DISH SMOKE SMOKE BTL2 BTL1 FIREFIRE

ENG & APU FIRE

ENG FIRE

MLG FIRE

APU FIRE

CARGO SMOKE

AGENT TO FWD _{AGENT TO AFT}

SH SH DIS DIS SMOKE SMOKE SH SH DIS DIS SMOKE SMOKE BTL2 BTL1 Page 451

(26)

NOTE

AVIONICS - CARGO - CABIN SYS FIRE PROTECTION (CONTROL & INDICATING)

SDS 2 SDS 1 AVIONICS SMOKE SDS RESET SD COND PAGE

CABIN SYSTEM SMOKE

CARGO SMOKE

CARGO SMOKE

AGENT TO FWD AGENT TO AFT

MLG BAY 222 VM DISH DISH SMOKE SMOKE DISH DISH SMOKE SMOKE BTL2 BTL1 FIREFIRE MLG BAY 222 VM FIRE FIRE Page 452

(27)

NOTE

WARNING DISPLAY

FAP

SMOKE LAVATORY SMOKE

AAP Lavatory Lav 11 EVAC Reset Smoke Reset EVAC Lav Reserv Misc Lav Maint Window Dimm CABIN INDICATING CABIN LOUDSPEAKERS AIP ACP ReeeeesetLL

LAVATORY FIRE PROTECTION (CONTROL & INDICATING)

(28)

NOTE

(29)

NOTE

CRANK STARTIGN NORM 2 FAULT FIRE 1 FAULT FIRE FF ON 1 FAULT FIRE SD FWS/CDS WD CMS ENG 2 FIRE DETECTION ZONES ENG 1 FIRE DETECTION ZONES LOOP A LOOP B ZONE 1 ZONE 2 ZONE 3 LOOP A LOOP B LOOP A LOOP B LOOP A LOOP B LOOP A LOOP B ENG 2 CONVERSION MODULE ENG 1 CONVERSION MODULE O 135 VM ENG START C T

CRANK STARTIGN NORM OFF ON 2 FAULT FIRE CPIOM FPF (ENG 1) CHANNEL B CHANNEL A FAN LEFT FIRE DET 411 VU CAUT MASTER CAUT MASTER WARN MASTER WARN MASTER CPIOM FPF (ENG 1) FIRE TEST ENG 1 FIRE THR LEVERS ...IDLE PARK BRAKE ...ON ENG 2 MASTER LVR ...OFF ENG 2 FIRE P/B ...PUSH AGENT 1 - 2 ...DISCH ALL ENG MASTERS ...OFF ATC VHF 1 ...NOTIFY CABIN CREW ...NOTIFY IF EVAC RORD : EVAC COMMAND ...INITIATE APU ...OFF

ENGINE FIRE PROTECTION (DETECTION ARCHITECTURE)

A F D X N E T W O R K FAN LEFT FIRE DET FAN RIGHT FIRE DET FAN RIGHT FIRE DET IPC FIRE DET IPC FIRE DET CORE FIRE DET CORE FIRE DET PYLON FIRE DET PYLON FIRE DET Page 455

(30)

NOTE

ENGINE FIRE PROTECTION (COMPONENT LOCATION)

C

A

B

DET-FIRE, ENG FAN L ZONE 1 LOOP A

DET-FIRE, ENG COREZONE 3

B

C

A

ZONE 3 ZONE 3 4001WD1 (4001WD2) LOOP B 4002WD2 (4002WD2) LOOP A 4021WD1 (4021WD2) LOOP B 4032WD1 (4032WD2) LOOP A 4011WD1 (4011WD2) LOOP A 4031WD1 (4031WD2) LOOP B 4012WD1 (4012WD2) LOOP B 4032WD1 (4032WD2)

DET-FIRE, ENG FAN RZONE 1

DET-FIRE, ENG IPC ZONEZONE 2

B

C FWD FWD

C

7WD1 (7WD2) 6WD1 (6WD2) Page 456

(31)

NOTE

ENGINE FIRE PROTECTION (COMPONENT LOCATION)

A

B 453EL (463EL)

B

CONVERSION MODULE-ENG 1(2) FIRE DET A A Z450 Z460 8WD1 (8WD2) Page 457

(32)

NOTE

ENGINE FIRE PROTECTION (EXTINGUISHING ARCHITECTURE)

WHEN RELEASED, THE ENG FIRE P/BSW ISOLATES THE ENGINE FROM THE FIRE SOURCES (ELECTRICAL, FUEL, HYDRAULIC, BLEED AIR)

ENG1 SHOWN, ENG2 SIMILAR

CARTDRIGE SQUIBS ELECTRICALLY ENERGIZED BY HOT BUS

HOT BUS HOT BUS ENG 1 - BOTTLE 1 DISCHARGE HEAD CARTRIDGE PRESSURE SWITCH CONVERSION MODULE ENG 1 FIRE DET ENG 1 - BOTTLE 2 PRESSURE SWITCH CPIOM FPF (ENG 1) CHANNEL B CHANNEL A CPIOM ENGINE FIRE-EXTINGUISHING BOTTLES ENG 1 - BOTTLE 1 SQUIB/DISCH LIGHTS AND TEST ENG 1 - BOTTLE 2 SQUIB/DISCH LIGHTS AND TEST

FPF (ENG 1) SQUIBS 1 & 2 DISCHARGE HEAD CARTRIDGE SQUIBS 1 & 2 Page 458

(33)

NOTE

APU FIRE PROTECTION (DETECTION ARHITECTURE)

FPF

APU FIRE DETECTION OPERATIONAL WITH A/C ENERGIZED WITH BATTERIES

CONVERSION MODULE APU/MLGB APU AREA CMS LGERS GROUND SERVICE PANEL EXTERNAL HORN ONLY ON GROUND F I R E AGENT 2 FIRE TEST ENG 1 APU AGENT 2 ENG 2 DISCH SQUIB DISCH SQUIB F I R E AGENT 2 ENG 1 AGENT 2 ENG 2 DISCH SQUIB F FIRE F FIREREE DISCH SQUIB AFDX NETWORK SD FWS/CDS WD CHANNEL A CHANNEL B NLG AREA APU FIRE DETECTOR LOOP A CPIOM FPF 411 VU CAUT MASTER CAUT MASTER WARN MASTER WARN MASTER APU SHUT OFF APU FIRE APU SHUT OFF APU FIRE THR LEVERS ...IDLE PARK BRAKE ...ON ENG 2 MASTER LVR ...OFF ENG 2 FIRE P/B ...PUSH AGENT 1 - 2 ...DISCH ALL ENG MASTERS ...OFF ATC VHF 1 ...NOTIFY CABIN CREW ...NOTIFY IF EVAC RORD : EVAC COMMAND ...INITIATE APU ...OFF 0 APU C APUGEN B GEN A APU FU 500 KG N1 0 N2 EGT V HZ BLEED 0 PSI 10 0 OFF OFF 00 00 15 10 2 5 0 APU FIRE DETECTOR LOOP B Page 459

(34)

NOTE

APU FIRE PROTECTION (COMPONENTS LOCATION)

RESPONDER ASSEMBLY LOOP A DET-FIRE, APU LOOP A LOOP B SENSING ELEMENT DET-FIRE, APU LOOP B Z310 Z190

CONVERSION MODULE-MLG BAY FIRE DET

21WG

22WG 10WP

(35)

NOTE

CONVERSION MODULE APU/MLGB

ON GROUND

FIRE P/BSW RELEASED OUT

AUTO SHUTDOWN ON GROUND CPIOM FPF CMS LGERS AFDX NETWORK FIRE EMERGENCY STOP RELAYS APU

FUEL LP & ISOLATION VALVES ECB

APU EXTINGUISHER

BOTTLE

DISCHARGE HEAD CARTRIDGE SQUIBS 1 & 2 PRESSURE SWITCH HOT BUS HOT BUS HOT BUS HOT BUS F I R E R E

AGENT 1 AGENT 2 FIRE TEST ENG 1 APU AGENT 1 AGENT 2 AGENT DISCH SQUIB DISCH SQUIB DISCH SQUIB FIRE F F FIREREE PUSH DISCH SQUIB DISCH SQUIB CHANNEL B CHANNEL A APU BOTTLE AUTO DISCHARGE RELAYS

F I R E R E AGENT 1 AGENT 2 ENG 1 AGENT 1 AGENT 2 DISCH SQUIB DISCH SQUIB DISCH SQUIB DISCH SQUIB CARTRIDGE SQUIBS ELECTRICALLY ENERGIZED BY HOT BUS

APU FIRE PROTECTION (EXTINGUISHING ARCHITECTURE)

(36)

NOTE

PRESSURIZED ENGINE FIRE-EXTINGUISHING BOTTLE DISCHARGE HEAD RUPTURE DISC CARTRIDGE DISCHARGE OUTLET PRESSURE SWITCH TEST POINT (ALLEN KEY) FWD PRESSURE SWITCH

APU FIRE EXTINGUISHER BOTTLE RUPTURE DISC DISCHARGE HEAD CARTRIDGE DISCHARGE OUTLET APU COMPARTMENT FRONT FIREWALL

ENGINE & APU FIRE PROTECTION (SERVICING)

HANDLES

WARNING

- BEFORE YOU TOUCH THE POWER DEVICE CARTRIDGE, MAKE SURE THAT YOU ARE GROUNDED AND THAT YOU HAVE INSTALLED A SHUNT DEVICE ON IT.DSF

- USE A CAP OR PLUG AS A SHUNT DEVICE (THE CAP OR PLUG WILL SHUNT THE PINS TOGETHER ON THE CARTRIDGE).

- DO NOT USE A FOIL SHUNT.

TEST POINT ALLEN KEY

- BEFORE YOU TOUCH THE POWER DEVICE CARTRIDGE, MAKE SURE THAT YOU ARE GROUNDED AND THAT YOU

HAVE INSTALLED A SHUNT DEVICE ON IT.L

- USE A CAP OR PLUG AS A SHUNT DEVICE (THE CAP OR PLUG WILL SHUNT THE PINS TOGETHER ON THE CARTRIDGE).

- DO NOT USE A FOIL SHUNT.

WARNING

(37)

NOTE

MLG FIRE PROTECTION (DETECTION ARCHITECTURE)

FWS/CDS WD CMS LOOP A LOOP B LOOP A LOOP B APU/MLGB CONVERSION MODULE MLGB LH FIRE-DET MLGB RH FIRE-DET MLGB RH FIRE-DET FIRE TEST ENG 1 ENG 2 ENG 1 ENG 2 AFDX NETWORK SD 1 2 5 6 3 4 7 8 °C PSI WHEEL G G G G Y Y Y Y 120 123 120 120 120 120 120 120 G ACCU 3.5 0 Y ACCU 3.5 0 ALTN EMER NORM Y SYS BRK ALTN EMER NORMG SYS BRK X 1000 PSI MAX 1 0 CAUT MASTER WARN MASTER CARGO SMOKE AGENT TO FWD AGENT TO AFT FIRE

MLG BAY FIRE FIRE DISCH SMOKE BTL2 BTL1 DISCH SMOKE CARGO SMOKE

DISCH SMOKE BTL2 BTL1 DISCH SMOKE CHANNEL A CHANNEL B CPIOM FPF MLG BAY FIRE THR LEVERS ...IDLE PARK BRAKE ...ON ENG 2 MASTER LVR ...OFF ENG 2 FIRE P/B ...PUSH AGENT 1 - 2 ...DISCH ALL ENG MASTERS ...OFF ATC VHF 1 ...NOTIFY CABIN CREW ...NOTIFY IF EVAC RORD :

EVAC COMMAND ...INITIATE APU ...OFF

MLGB LH FIRE-DET MLGB

(38)

NOTE

MLG FIRE PROTECTION (COMPONENT LOCATION)

DET-FIRE, MLG BAY R LOOP B DET-FIRE, MLG BAY R LOOP A DET-FIRE, MLG BAY L LOOP A DET-FIRE, MLG BAY L LOOP B Z140 FR56 FR60 3WP 5WP 4WP 2WP Page 464

(39)

NOTE

CABIN & LAV FIRE PROTECTION (DETECTION ARCHITECTURE)

AFDX NETWORK COCKPIT WARNINGS CABIN WARNINGS SDS 2 CIDS DIRECTOR SDF FCRC SMOKE DETECTORS LAVATORY SMOKE DETECTOR FCRC SMO ADDITIONAL ATTENDANT PANEL CABIN LOUDSPEAKERS ATTENDANT INDICATION PANEL

AREA CALL PANEL RESET PANEL RESET PANEL FAP CCRC SMOKE DETECTORS POWER SUPPLY SMOKE CCRC SMOKE SMOKE FCRC SMOKE SMOKE LAVATORY SMOKE

DEU B

CIDS CabinStatusMusic LightsDoors/Slides Water/WasteSmokeDetect CabinStatusPaxCallLights Screen Off Caution Pre Ann Temp Smoke Detection Seat Sett

CIDS CabinStatusMusic LightsDoors/Slides Water/WasteSmokeDetect CabinStatusPaxCallLights Screen Off Caution Pre Ann Temp Smoke Detection Pos. 02 Lav 1 RH Pos. 06 Pos. 08 Pos. 10 Pos. 12 Pos. 14 Pos. 16 Pos. 18 Pos. 20 Lav 74 P P Pos. 24 P Po Pos. s. 26s 2 Pos. 282888 Pos. 300 Pos. 322 Pos. 344 Pos. 366 Pos. 388 Pos. 400 Pos. 422 Pos. 44 Pos. 46 Pos. 48 Pos. 50 Pos. 52 Pos. 54 Pos. 56 Pos. 58 Pos. 60 Pos. 62 Pos. 64 Pos. 66 Pos. 68 Pos. 70 Pos. 72 Seat Sett CIDS Caution Screen Off Caution

Caution Smoke Detection

Music LightsDoors/Slides Cabin

Status PreAnn SlidesDoors/TempTempTTWater/WasteSmokeDetectSeatSett CabinStatusPaxCallLights

Alert

Smoke detected in: Lav 1 RH

SmokeReset

Alert

Smoke detected in: Lav 1 RH Lavatory Lav 11 EVAC Reset Reset Smoke Reset EVAC Lav Reserv Misc Lav Maint Window Dimm CAUT MASTER WARN MASTER WD SDS 1 R Page 465

(40)

NOTE

CCRC

FCRC

PORTABLE FIRE EXTINGUISHER _LAVATORY

DISCHARGE TUBE

FUSIBLE PLUG WASTE BIN

PRESSURE GAUGE

CABIN & LAV FIRE PROTECTION (EXTINGUISHING)

(41)

NOTE

CARGO FIRE PROTECTION (DETECTION ARCHITECTURE)

RESET PANEL SDS 2 SDS 1 RESET PANEL CARGO SMOKE

AGENT TO FWD AGENT TO AFT FIRE

MLG BAY FIRE DISCH SMOKE CH DIS SMOKE BTL2 BTL1 DISCH SMOKE CH DIS SMOKE FIRE MLG BAY FIRE

SMOKE ALARM IF:

- AT LEAST TWO DETECTORS IN A SAME COMPARTMENT DETECT SMOKE OR

- FOR A PAIR OF DETECTORS, ONE IS INOPERATIVE AND THE OTHER DETECTS SMOKE AFDX NETWORK FWS VCS CMS SYSTEM TEST PAIR OF AMBIENT TYPE SMOKE DETECTORS CIDS DIRECTOR SDF SD WD SMOKE CARGO SMOKE

SMOKE AFT CARGO SMOKE

HOT AIR 2 1 RAM AIR MIX AIR TO CKPT AVNCS COND VENT 25 CRG RESET BULK 20 CRG 19 23 °C 2 PACK 1 PACK 20 SMOKE AFT/BULK CARGO COMPARTMENT FWD CARGO COMPARTMENT CAUT MASTER CAUT MASTER WARN MASTER WARN MASTER Page 467

(42)

NOTE

CARGO FIRE PROTECTION (EXTINGUISHING ARCHITECTURE)

CARGO SMOKE

DISCH SMOKE DISCH SMOKE BTL2 BTL1 DISCH SMOKE DISCH SMOKE BOTTLE 1 BOTTLE 2 FEDC 1 FEDC 2 FLOW METERING EQUIPMENT DIVERTER VALVE HIGH-RATED

BOTTLE FLOW-METERED_BOTTLE _{AFT/BULK CARGO SPRAY NOZZLES}

FWD CARGO SPRAY NOZZLES

FWD AFT/BULK CIDS DIRECTOR SDF AFDX NETWORK CMS SYSTEM TEST DISCHARGE HEAD CARTRIDGE TCPS SQUIBS 1 & 2 DISCHARGE HEAD CARTRIDGE TCPS PRESSURE SWITCH SQUIBS 1 & 2 FWD DISCHARGE HEAD CARTRIDGE SQUIBS 1 & 2 SQUIBS

1 & 2 AFT/BULK DISCHARGEHEAD CARTRIDGE

THE SIZE OF FLOW METERED BOTTLE 2 DEPENDS ON THE ETOPS OPTIONS

HIGH-RATED BOTTLE 1

FLOW-METERED BOTTLE 2

DIVERTER VALVE

FLOW METERING EQUIPMENT

(43)

NOTE

CARGO FIRE PROTECTION (COMPONENT LOCATION)

FR22 FR27 FR26 FR23 FR35 FR34 FR41 FR40 FR21 DET-SMK CSDM, FWD LDCC DET-SMK CSDM, FWD LDCC DET-SMK CSDM, FWD LDCC DET-SMK CSDM, FWD LDCC 130WH 120WH 110WH 100WH FR77 DEE CSDM, 133 DET-SMK CSDM, AFT LDCC DET-SMK CSDM, AFT LDCC DET-SMK CSDM, AFT LDCC DET-SMK CSDM, BULK LDCC FR65 FR64 FR71 FR70 FR76 FR83FR82 FR63 240WH 220WH 210WH 200WH Z130 Z150 Z160 Page 469

(44)

NOTE

CONVERTER-FIRE EXTING 1,LDCC CONVERTER-FIRE EXTING 2,LDCC FIRE EXTINGUISHER FLOW METERING EQPT FIRE EXTINGUISHER DIVERTER VALVE FR73 FR76 20WX 4000WX 4080WX 4010WX 21WX 4060WX

CARGO FIRE PROTECTION (COMPONENT LOCATION)

(45)

NOTE

AVIONICS & ADDITIONAL ELECTRONICS COMPARTMENT FIRE PROTECTION (DETECTION ARCHITECTURE)

MAIN AVIONICS CORE RACK

& IFEC FWS

SD WD

MAIN AVIONICS IFEC

AIR EXTRACTION DUCTS

CONNECTIVITY RACK CMS SYSTEM TEST VCS AFDX NETWORK

AIR EXTRACTION DUCTS

SDS 2 SDS 1 411 VU CAUT MASTER CAUT MASTER WARN MASTER WARN MASTER

SMOKE AVNCS SMOKE SMOKE IFEC SMOKE SMOKE PAX BBAND SMOKE

HOT AIR 2 1 RAM AIR MIX AIR TO CKPT AVNCS COND SMOKE L R 25 CRG BULK 20 CRG 19 23 °C 2 PACK 1 PACK CIDS DIRECTOR SDF

RESET PANEL _{RESET PANEL}

VENT

AVNCS

SMOKE EXTRACTAVNCS

A U T O CAB FANS COOLG A U T O OFF FAULT OFF OFF OVRD FAULT SMOKE

CAB SYS SMOKE

IFEC PAX BBAND

OFF SMOKE OFF SMOKE OFF SMOKE FF OF SMOKE 1 MAN START 2 ENG ON ON 1 MAN START 2 ENG ON ON Page 471

(46)

NOTE

3WA Z170 Z130 Z120 3WA FR18 FR19 DET-SMK,FWD AVNCS COMPT 01 DET-SMK,FWD AVNCS COMPT 02 DET-SMK,FWD AVNCS COMPT 03 DET-SMK,FWD AVNCS COMPT 04 DET-SMK, IFEC 01 DET-SMK,CORE CONNECTIVITY RACK 01 DET-SMK,CORE CONNECTIVITY RACK 02 DET-SMK, IFEC 02 FR85 FR86

AVIONIC & ADDITIONAL ELECTRONICS COMPARTMENT FIRE PROTECTION (COMPONENT LOCATION)

3WA

1WA

2WA 4WA

11WA 12WA 14WA 13WA

(47)

ATA 49

AIRBORNE AUXILIARY POWER

_{APU SYSTEMS LAYOUT}

AIR INTAKE FLAP ACTUATOR SURGE CONTROL VALVE OIL COOLER DMM EGT IGNITION UNIT T2 SPEED SENSOR IGV ACTUATOR

PRIMARY MANIFOLD SUPPLY SECONDARY MANIFOLD SUPPLY ECD OIL LEVEL SENSOR G E A R B O X FLOW DIVIDER VALVE SHUT-OFF VALVE FCU METERING VALVE FUEL TEMP HP PUMP LP PUMP BV / IGV /SCV SUPPLY BV / IGV /SCV RETURN FUEL PRESS SW LOW APU LP VALVE APU PUMP A/C FUEL APU ISOL VALVE AGLC SLC BAT 2 BAT BUS BAT BUS BAT 1 1 : BEARING SCAVENGE 2 : STARTER / GENERATOR SCAVENGE GEN FILTER OTS 1 2 LOP OTS LUBRICATION MODULE OIL OIL PUMP SGCU SPU STARTER GENERATOR THERMOSTAT VALVE AIRCRAFT PNEUMATIC SYSTEM BLEED VALVE MODU LE 28 VDC EXTER NAL AIR 230 V A C PRE S SURE

NOTE

(48)

F I R E F I R E

AGENT 1 AGENT 2 FIRE TEST ENG 1 APU AGENT 1 AGENT 2 ENG 2 AGENT DISCH SQUIB DISCH SQUIB F FIRE PUSH TEST TEST DISCH SQUIB F FIRE DISCH SQUIB DISCH SQUIB HI LVL

INCREASE DECREASE PRESELECT 88888888 PRESELECT (PFQ) FAULT OVERFLOW NORMAL BATTERY POWER SUPPLY 88888888 ACTUAL (FOB) 8888888888888888 STATUS 8888888888888888 MAN REFUEL XFR DEFUEL AUTO REFUEL OFF MODE SELECT 88888 88888 88888 R. WING OPEN SHUT R.WING CTR CTR L. WING L.WING 100 000 Kg NO BA 65 000 Kg FOB > PRESELECT AUTO REFUEL END 15000 35000 15000 SHUTOFF TEST TEST NORMAL TE NO SHUTDOWN NORMAL APU EMERGENCY SHUTDOWN SH NO S ALTN GAUGING ALTN NORMAL AL NO

ELEC PANEL AIR PANEL

APU MASTER SW & START P/B

ENG / APU FIRE PANEL MAINTENANCE PANEL MASTER SW APU START ON AVAIL ON FAULT

INTEGRATED REFUEL PANEL

NLG CONTROL PANEL

BAT 1 BAT EMER 1 BAT 2 ELM GALLEY

EXT 1 BUS TIE A U T O APU GEN BAT EMER 2 EXT 2 DRIVE 2 1 COMMERCIAL AC 2A BUS AC 2B BUS AC 1B BUS AC 1A BUS GEN 1A 1B 2B 2A

DRIVE DRIVE DRIVE

E L E C E L E C 225 VM GEN GEN GEN SIDE 1 & 2 OFF FAULT DISC FAULT ON AVAIL OFF FAULT DISC FAULT OFF OFF FAULT OFF FAULT DISC FAULT DISC FAUL F F LLT ON AVAIL OFF FAULT DISC FAULT DISC FAUL F F LLT OFF OFF OFF PAX SYS OFF ISOL OFF FAULT ISOL ISOL OFF FAULT OFF FAULT OFF FAULT OFF FAULT A I R A I R XBLEED HOT COLD COCKPIT HOT COLD PURS SEL CABIN HI LO MAN AIR FLOW NORM OPEN CLOSE AUTO CKPT HI VENT PACK 1 ENG 1 BLEED

HOT AIR 1 HOT AIR 2

ENG 2 BLEED APU BLEED WINDSHIELD DEFOG PACK 2 RAM AIR ON ON OFF FAULT OFF FAU F F LTLL OFF FAULT OFF FAU F F LTLL ON FAULT ON FAU F F LTLL OFF FAULT OFF FAU F F LTLL OFF FAULT ON ON OFF FAULT OFF FAULT OFF FAU F F LTLL H H H H H H H H H H H H

APU EMERGENCY SHUT DOWN

APU CONTROLS

ECON MODE APU ON

NOTE

(49)

APU SD PAGE

ADVISORIES

APU

KG

%

PSI

HZ

V

%

°C

GEN

62

230

400 BLEED

44

480 APU FU

0

10 N

100

0

5 ₇

9

545 EGT

AVAIL

FLAP OPEN

NOTE

(50)

APU INSTALLATION

APU EXHAUST DRAIN PORT

APU COMPARTMENT DRAIN MASTS APU ENGINE DRAIN MASTS RH MAINTENANCE DOOR

TO OPEN THE APU DOORS, THE OVERPRESSURE DOOR SHOULD BE OPENED FIRST TO ACCESS THE INTERNAL LOCKING DEVICE.

LH MAINTENANCE DOOR LOCKING DEVICE OVERPRESSURE DOOR

NOTE

(51)

APU FUEL SYSTEM (ARCHITECTURE)

LUBE UNIT GEARBOX CMS A F D X N E T W O R K ECB S ACTUATORS FUEL SYSTEM WET CRANK TEST PRIMARY SECONDARY FUEL CONTROL UNIT FLOW DIVIDER VALVE SHUT OFF VALVE S METERING VALVE DELTA P SWITCH _GEAR PUMP FILTER BOOST PUMP LOW PRESSURE SWITCH DRAIN PORT D FUEL NOZZLES (14) TM ECOLOGY VALVE APU SHUTDOWN CDS APU PAGE FUEL PRESS LO 230 230 APU START

NOTE

(52)

APU FUEL SYSTEM (COMPONENTS LOCATION)

A Z310 FR105 FR109 FR112 C B FR107 FR108 FR104

C

B

A

FUEL ATOMIZERS PRIMARY FUEL MANIFOLD SECONDARY FUEL MANIFOLD FWD FUEL FILTER

FLOW DIVIDER VALVE

PRESSURIZING SHUT-OFF VALVE CONNECTION TO FUEL SUPPLY LINE PRESSURE RELIEF VALVE SHUT-OFF SOLENOID METERING MODULE CONNECTION TO FUEL MANIFOLDS CONNECTION TO

ELECTRONIC CONTROL BOX

NOTE

(53)

ECB MONITORING SG SCAVENGE FILTER DELTA P SWITCH OIL TANK CHIP DETECTOR OIL SUPPLY FILTER DELTA P SWITCH LOW OIL PRESSURE SWITCH SG SCAVENGE OIL TEMTERATURE SENSOR OIL TANK LEVEL SENSOR OIL SUPPLY TEMPERATURE SENSOR

APU OIL SYSTEM (MONITORING, SERVICING)

PRESSURE FILL PORT (OPTIONAL) SSURE PORT GRAVITY FILL CAP PRESSURE OVERFILL PORT (OPTIONAL) ELECTRICAL CHIP DETECTOR AND DRAIN PLUG OIL LEVEL SENSOR SIGHT GAGE FULL MARK ADD MARK OVERPRESSURE DOOR APU RH DOOR MONITORING SERVICING

NOTE

(54)

APU OIL SYSTEM (COMPONENTS LOCATION)

Z310 FR105 FR104 FR106 FR107 FR108 FR112 AIR / OIL SEPARATOR FILTER-LUBE, APU COLLECTOR - CHIP 3, APU

VALVE-THERMOSTAT BYPASS, APU COLLECTOR-CHIP 4, APU OIL TANK COLLECTOR-CHIP 1, APU FILTER-GEN OIL, APU COOLER-OIL, APU

A

B

PUMP-OIL, APU COLLECTOR - CHIP 2, APU

B

VALVE-PRESSURE REGULATION, APU OIL

5100KT12 5100KT11 5100KT6 59KT43 59KT44 5100KT10 5100KT9 59KT42 59KT41 5100KT8

NOTE

(55)

APU AIR SYSTEM (ARCHITECTURE)

TM FDBK TM FDBK FUEL FUEL FUEL FDBK PNEUMATIC SYSTEM APU COMPARTMENT PRESSURE MODULE _INLET TEMPERATURE SENSOR IGV IGV COMPARTMENT COOLING DUCT AIR INTAKE FLAP

EXTERNAL AIR OIL COOLER ECB S BOMU CRDC ADIRS PACK BAS APU MASTER SW ON ON FAULT FAULT APU BLEED ON FAULT ON INLET DUCT TOTAL PRESSURE SENSOR DELTA P SENSOR SURGE CONTROL VALVE APU BLEED VALVE ECON MODE APU ON ON A F D X N E T W O R K

NOTE

(56)

APU AIR SYSTEM (COMPONENT LOCATION)

B

VALVE-BLEED, APU VALVE-SURGE CONTROL, APU PRESS

SENSOR-LOAD COMPRESSOR, APU

FR105 FR107 FR108 59KH18 59KH22 59KH7

NOTE

(57)

APU START SYSTEM (ARCHITECTURE)

EPDS 230 VAC BUS CONTROL AND MONITORING SG FCU IGNITION PLUG AFDX NETWORK LGERS CMS SG STATUS IGNITION UNIT ENABLE FLAP OPENING POSITION

AIR INTAKE FLAP

SG SUPPLY FUEL ON IGNITION ON DRY/WET CRANK TEST CRDCs ICP APU START MASTER SW ON ON AVAIL AVAIL ON ON FAULT FAULT SGCU BAT1 28 VDC BUS BAT2 SPU MONIT ORING START SIGNAL ECB

NOTE

(58)

APU START SYSTEM (COMPONENT LOCATION)

A FR112 FR106 FR104 Z310 Z120 B D FR13 FR16 FR17 FR1 FR14 FR18 D SPU-APU SG-APU SGCU-APU B C A C 30KA 21KA 20KA

NOTE

(59)

APU SYSTEM (INTERFACE)

AFDX NETWORK APU SYSTEMS

OIL SYSTEM IGN/START SYSTEM AIR SYSTEM AIR INTAKE SYSTEM FUEL SYSTEM APU EMERGENCY SHUT DOWN REFUEL PANEL APU SHUT OFF NLG GROUNDSERVICE PANEL

START AND NORMAL SHUTDOWN START EMERGENCY SHUTDOWN APU E F FIRE F PUSH

FIRE PANEL _EMERGENCY

SHUTDOWN EMERGENCY SHUTDOWN CONTROL AND MONITORING EMERGENCY SHUTDOWN

THE ECB IS LOCATED IN A COMPARTMENT BEHIND THE

BULK CARGO FIRE PROTECTION SYSTEM ICP APU START MASTER SW ON ON AVAIL AVAIL ON ON FAULT FAULT APU PANEL ECB

ECB IS PERMANENTELY ENERGIZED WHEN A/C IS ENERGIZED

(EVEN WITH MASTER SWITCH OFF)

NOTE

(60)

APU SYSTEM (COMPONENTS LOCATION)

A Z170 FR85 FR86 FR93

A

B

FR85 FR86 FR87

B

ECB-APU

NOTE

(61)

NOTE

ATA 70

STANDARD PRACTICES - ENGINES

_{ENGINE SYSTEM LAYOUT}

ANTI-ICE NAI PRV

NAI

PRSOV TURBINE OVHT

TURBINE OVHT TRANSLAT COWL EGT HP3 IGN A N1T VIB N2 N3 N1 IGN B NACELLE TEMP ACTUATOR (X6) (X2) PMA SCV STARTER BLEED AIR SCAVENGE PUMPS (X10) OBV XDCR (X2) LOW OIL PRESS SW FOHE FUEL SYSTEM SAOHE (X2) PRESS PUMP TEMP SENSOR QTY XMTR OIL DEBRIS SENSOR T20 LOW FUEL PRESS SW FBH BYPASS VALVE A/C FUEL LP VALVE OIL SYSTEM HP/IP TCC ACTUATORS VSV ACTUATORS TO FUEL SPRAY NOZZLES FUEL FLOW XMTR HP FUEL FILTER FUEL TEMP SENSOR HMU HP SOV FMV VSV DRAIN VALVE DRAIN HP FUEL PUMP LP LP FILTER MASTER SWITCH FOHE ENG 1 ENG 2 Page 487

(62)

NOTE

© Airbus SAS 2014. All rights reserved. Confidential and proprietary document. RAIN RPLNT WIPER INTMT FAST INTMT MEDIUM SLOW FAST OFF INTMT SLOW FAST OFF SLOW FAST OFF WIPER RAIN RPLNT INTMT FAST INTMT SLOW FAST OFF INTMT SLOW FAST OFF SLOW FAST OFF EXT LT NAV WING ON LOGOON O 1 BEACONON NAV STROBE O SEAT BELTS EMER EXIT LT ON ARM SIGNS O NO SMOKING MASTER SW APU START ON AVAIL ON FAULT REMOTE C/B CTL ELEC ON GND HYD YELLOW ELEC PMP A U TO GREEN ELEC PMP A U TO OFF FAULT ON OFF FAULT ON ON CKPT DOOR CTLR STRIKE TOP MID 1 2 BOT CHAN HORN OFF COMMANDEVAC PURS MECH CALL CALLS EMER AFT EXIT MID FWD PURS ALL DFDR ACMS RCDR EVENT TRIGGER EMER GEN FAULT OIS DATA TO AVNCS GATELINK OFF OFF OIS ADIRS IR3 IR2 IR1 OFF ATT NAV OFF ATT OFF ATT NAV ON BAT F/CTL 211VM PRIM 3 SEC 3 SEC 1 PRIM 1 VENT AVNCS SMOKE AVNCS EXTRACTCOOLGCAB FANS

SMOKE INT LT ANN LT T STBY COMPASS ANTI ICE 2 1 ENG WING PROBE & WINDOW HEAT ON ON FAULT ON FAULT ON FAULT RESET

CKPT EQPT POWER SUPPLY 232VM 222VM 1 5 3 4 5 2 W 6 V U T S R W V U T S RPACK 2VCS2 FMC-B TR 2

AICS2FWS2LGCIS2BSCS2AESU2

2 CIDS2 AVNCS SDS 2 SLATS 2 FQMS 2 FLAPS 2 EMER TR2 WHC 2 KBD 2 CCD 2 & MAINT & MAINT F I R E FIRE TEST ENG 1 APU ENG 2 DISCH SQUIB DISCH SQUIB DISCH SQUIB DISCH SQUIB B OOM SET CVR ERASE TEST 255VM 245VM AIR COND FANS RESET FAULT OXYGEN RESET ON FAULT CABIN PRESS

CABIN ALT CABIN V/S

MODE INC DEC TRGT AU TO MODE DN UP TRGT 215 VM MAN MAN 1MAN START2 ENG ON TOWING ON BAT CHARGE POWER LOW MED HIGH GND HF DATALINK SVCE INT OVRD CARGO SMOKE

AGENT TO FWD AGENT TO AFTFIRE

MLG BAY BTL2 BTL1 CKPT DOOR LOCKG SYS GND CONNECTION COM ON FADEC1GND PWR 2 ENG F/CTL SEC 2 PRIM 2 H Y D H Y D PUMP SUPPLY GREEN YELLOW GREENENG1YELLOW ENG2 235 VM

PUMP SUPPLY SUPPLYPUMP SUPPLYPUMP

ISOL OVHT ISOL OVHT ISOL OVHT ISOL OVHT F U E L F U E L L CROSSFEED A STBY

MAINL TK MAINR TKSTBY

CROSSFEED B R ON FAULT MAN FAULT OFF FAULT OFF FAULT OFF FAULT OFF FAULT OFF FAULT ON OPEN ON OPEN CTR TK BAT EMER 2 EMER 1 OFF 26.8

CARGO AIR COND

ISOL VALVES BULK 5 15 HEATER OFF FAULT OFF FAULT AI R AI R XBLEED COLD COCKPIT COLD CABIN HI LO AIR FLOW NORM CLOSE AUTO CKPT HI VENT ENG 1 BLEED HOT AIR 1 HOT AIR 2

APU BLEED WINDSHIELD DEFOG PACK 2 OFF FAULT ON ON OFF FAULT 221 VM CABIN LAVATORY OCCPD

BAT 1BAT EMER 1 BAT 2 ELM GALLEY

EXT 1 BUS TIE APU GEN BAT EMER 2 EXT 2 DRIVE 2 1COMMERCIAL GEN 1A 1B 2B 2A

DRIVE DRIVE DRIVE

E L E C L E 225 VM GEN GEN GEN SIDE 1 & 2 OFF FAULT ON AVAIL OFF FAULT OFF OFF FAULT OFF FAULT ON AVAIL OFF FAULT OFF OFF OFF PAX SYS OFF ISOL OFF FAULT OFF FAULT OFF FAULT OFF FAULT OFF FAULT RESET

CKPT EQPT POWER SUPPLY 231VM 1 1 3 5 2 3 4 5 2 F 6 E D C B A F E D C B A PACK1VCS1SCSFMC-AFMC-C TR 1

AICS1FWS1LGCIS1BSCS1AESU1

1 CIDS1 SDS 1 SLATS 1 FQMS 1 FLAPS 1 EMER TR1 WHC 1FCUPRINTER KBD 1 CCD 1 265VU OXYGEN AU TO CREW SUPPLY

ENGINE CONTROLS

F I R E F I R E AGENT 1 AGENT 2 FIRE

TEST ENG 1 APU AGENT 1 AGENT 2 ENG 2 AGENT DISCH SQUIB DISCH SQUIB DISCH SQUIB F FIRE PUSH PUSH DISCH SQUIB DISCH SQUIB

ENG / APU FIRE PANEL

1 MAN START 2 ENG ON ON ON

ENG MAN START FADEC 1 GND PWR 2 ENG ON ON ON ON FADEC GND PWR THRUST CONTROL LEVERS TO GA FLX CL 0 M C T T H R A TO GA FLX CL 0 M C T T H R A OFF ON OFF ON 135 VM ENG START

CRANK STARTIGN

NORM 2 FAULT FIRE 1 FAULT FIRE

ENG START PANEL RESET PANELS

(63)

NOTE

ENGINE INDICATING

ENG

0 °C 500 NAC N 3 0.3 3 0. N 2 0.2 2 0. N 1 V I B 6 0. 6 0. P S I ₂₂₀ 220 ° C 118 118 QT O I L 4 18. 18.4 FF 9120 9120 % N3 92.6 6 92. % N2 93.8 8 93. KG/H

ENG

P S I IGN 37 38 N 3 0.3 3 0. N 2 0.2 2 0. N 1 V I B XX 2 4. P S I ₂₂₀ 7 ° C 118 118 QT O I L XX 18.4 FF ₉₁₂₀ XX CLOGGED % N3 92.6 6 92. % N2 93.8 0 106. KG/H °C EGT °C EGT % N1 % THR 751 0 50. 10 5 0 7 84. 811 0 50. 10 5 0 7 84. PACKS/NAI 9 83. % FLEX 59°C 1

ENGINE DISPLAY (ED) (NORMAL) ENGINE DISPLAY (ED) (ABNORMAL)

ENG SD PAGE (NORMAL) ENG SD PAGE (ABNORMAL)

(64)

NOTE

POWER PACK RESERVOIR EPDS QUICK DISCONNECT FOR BACK-UP EXTERNAL PUMP FAN COWL OPENING ACTUATORS T/R COWL OPENING ACTUATORS FAN COWL PROXIMITY SWITCH FAN COWL CONTROL SWITCHES T/R COWL CONTROL SWITCHES SFCC SOLENOID VALVES EIF SOLENOID CONTROL LOGIC CONVERSION MODULE (ATA26) POWER SUPPLY DEMAND SLAT INHIBITION REFILL PORT SLAT INHIBITION

ENGINE PDOS (ARCHITECTURE)

(65)

NOTE

MANUAL CRANK OF THE LP SYSTEM MANUAL CRANK OF THE IP SYSTEM

MANUAL CRANK OF THE HP SYSTEM

EXTERNAL GEARBOX FRONT FACE CENTRIFUGAL BREATHER

ENGINE LP / IP / HP MANUAL CRANK (MAINTENANCE)

(66)

NOTE

© Airbus SAS 2014. All rights reserved. Confidential and proprietary document. ZONE 2 TURBINE INDEPENDENT DRAINS (BETWEEN THRUST REVERSER COWLS) FUEL MANIFOLD DRAIN TANK OIL TANK SCUPPER FUEL SUPPLY PIPE SHROUD FUEL PUMP ENGINE DRIVEN PUMP GREEN ENGINE DRIVEN PUMP YELLOW STARTER VFG VFG PYLON TCC ACTUATORS VSV ACTUATORS FRONT BEARING HOUSING VENT VALVE CENTRIFUGAL BREATHER OUTLET DRAIN MAST FUEL OIL DIFFERENT FLUIDS PDOS SUMPS