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A/THR FUEL PUMPS ANTI SKID
N/W. STEER AUTO BRK L/G RETRACT
CAB PR 1+2 PACK 1+2
(1) AL2t landing gear extension, control reverts to direct law in pitch as well as in roll (Refer to
00011770 **Not found**).
(2) 7 full brake applications are available.
ENG 1(2) FADEC FAULT
Applicable to:
,
,
MSN,,,,
ENG INDICATIONS................................................................................................................. CHECK
L2 Due to the fact that engine indications are lost, other system pages such as HYD SD page, ELEC
AC SD page or BLEED SD page must be used to check engine status.
L1�� IF ENG FAIL CONFIRMED:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 172/194
FCOM 19 AUG 10
ENG 1(2) FADEC FAULT
Applicable to:
CONFIRM ENG STATUS.
ON SYS PAGES:
L2 Due to the fact that engine indications are lost, other system pages such as HYD SD page, ELEC
AC SD page or BLEED SD page must be used to check engine status.
L1�� IF ENG FAIL CONFIRMED:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
ENG 1(2) FADEC HI TEMP
Applicable to:
, ,
MSN
�� On the ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (ASSOCIATED ENGINE)...............................................................................OFF
ENG MODE SEL.................................................................................................................NORM
FADEC GND PWR.................................................................................................. CHECK OFF
�� In flight:
�� If the ECU temp is above the overheat threshold:
FADEC OVHT
L2 Reducing engine power should decrease temperature in the ECU area.
If overheating is severe enough, ECU failure could result in a significant loss of engine
functions.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 173/194
FCOM 19 AUG 10
ENG 1(2) FADEC OVHT
Applicable to: MSN
4566,,
�� On the ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (ASSOCIATED ENGINE)...............................................................................OFF
ENG MODE SEL.................................................................................................................NORM
FADEC GND PWR ................................................................................................. CHECK OFF
�� In flight:
L2 Reducing engine power should decrease temperature in area of ECU.
If overheating is severe enough, EEC failure could result with consequent loss of engine
function.
L1 ENG INDICATIONS...........................................................................................................CHECK
�� IF ABN ENG OPERATION:
THR LEVER (AFFECTED)..............................................................................................IDLE
ENG MASTER (AFFECTED)........................................................................................... OFF
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
ENG THRUST LOCKED
Applicable to: ALL
L2 The thrust is frozen on one or more engine after a failure or an involuntary autothrust
disconnections.
This caution is automatically repeated every 5 s until thrust levers are moved.
L1 THR LEVERS...........................................................................................................................MOVE
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 174/194
FCOM 19 AUG 10
ENG TAILPIPE FIRE
　
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