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Applicable to:
, ,
MSN
Internal engine fire may be encountered during engine start or engine shutdown.
It may be seen by the ground crew, or the EGT may fail to decrease after the MASTER sw is turned
OFF.
CAUTION External fire agents can cause severe corrosive damage and should, therefore, only
be considered after having applied the following procedure:
MAN START (if manual start performed)..................................................................................... OFF
ENG MASTER (affected) .............................................................................................................OFF
Note: Do not press the engine fire pb, since this would cut off the FADEC power supply, which
would prevent motoring sequence.
AIR BLEED PRESS ........................................................................................................ ESTABLISH
Select the APU, or opposite BLEED, to motor the engine.
If APU BLEED is not available, and the opposite engine is shut down, connect external pneumatic
power (if readily available).
BEACON ...................................................................................................................................... ON
ENG MODE SEL.................................................................................................................... CRANK
MAN START..................................................................................................................................ON
The start valve automatically reopens, when N2 is below 20 %
�� When burning has stopped:
MAN START ..........................................................................................................................OFF
ENG MODE SEL ............................................................................................................... NORM
Maintenance action is due.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 175/194
FCOM 19 AUG 10
ENG TAILPIPE FIRE
Applicable to: MSN
4566,,,
Internal engine fire may be encountered during engine start or engine shutdown.
It may be seen by the ground crew, or the EGT may fail to decrease after the MASTER sw is turned
OFF.
CAUTION External fire agents can cause severe corrosive damage and should, therefore, only
be considered after having applied the following procedure:
MAN START (if manual start performed)..................................................................................... OFF
ENG MASTER (affected) .............................................................................................................OFF
Note: Do not press the engine fire pb, since this would cut off the FADEC power supply, which
would prevent motoring sequence.
AIR BLEED PRESS ........................................................................................................ ESTABLISH
Select the APU, or opposite BLEED, to motor the engine.
If APU BLEED is not available, and the opposite engine is shut down, connect external pneumatic
power (if readily available).
BEACON ...................................................................................................................................... ON
ENG MODE SEL.................................................................................................................... CRANK
MAN START..................................................................................................................................ON
The start valve automatically reopens, when N2 is below 10 %.
�� When burning has stopped:
MAN START ..........................................................................................................................OFF
ENG MODE SEL ............................................................................................................... NORM
Maintenance action is due.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 176/194
FCOM 19 AUG 10
HIGH ENGINE VIBRATION
Applicable to:
, ,
MSN
The VIB advisory on ECAM (N1 ≥ 6 units, N2 ≥ 4.3 units) is mainly a guideline to induce the crew to
monitor engine parameters more closely.
VIB detection alone does not require engine shut down.
Note: 1. High engine vibrations may be accompanied by cockpit and cabin smoke and/or the
smell of burning. This may be due only to compressor blade tip contact with associated
abradable seals.
2. High N1 vibrations are generally accompanied by perceivable airframe vibrations. High
　
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