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L2 If the A/THR is engaged, adjust the thrust lever (of the affected engine) to align the thrust lever
command with actual N1 and disconnect A/THR.
L1 ENG (AFFECTED) SLOW RESPONSE
L2 Depending on the type of failure, one of the above two messages is displayed.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 112/194
FCOM 19 AUG 10
ENG 1(2) COMPRESSOR VANE (Cont'd)
STATUS
AVOID RAPID THR CHANGES
ENG (affected) SLOW RESPONSE
ENG 1(2) COMPRESSOR VANE
Applicable to:
L2 Low Pressure Compressor Bleed Valve (LPCBV) or Variable Stator Vane (VSV) failure.
Engine stall may occur at any thrust change.
L1 AVOID THR CHANGES (not displayed if LPCBV goes to open position).
L2 If autothrust engaged, adjust thrust lever (of affected engine) to align thrust lever command with
actual EPR and disconnect autothrust.
L1 AVOID RAPID THRUST CHANGES (displayed when the VSV position disagrees with the
command).
L2 Engine stall may occur at any rapid thrust change.
L1 IF ENG STALL:
THR LEVER 1(2)................................................................................................................... IDLE
ENG MASTER 1(2).................................................................................................................OFF
ON GROUND:
THR LEVER 1(2)................................................................................................................... IDLE
ENG MASTER 1 (2)............................................................................................................... OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
L2 Apply after ENG SHUT DOWN procedure.
AVOID THR CHANGES
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 113/194
FCOM 19 AUG 10
ENG 1(2) COMPRESSOR VANE
Applicable to: MSN,,,
L2 Low Pressure Compressor Bleed Valve (LPCBV) or Variable Stator Vane (VSV) failure.
Engine stall may occur at any thrust change.
L1 AVOID THR CHANGES (not displayed if LPCBV goes to open position).
L2 If autothrust engaged, adjust thrust lever (of affected engine) to align thrust lever command with
actual EPR and disconnect autothrust.
L1 AVOID RAPID THRUST CHANGES (displayed when the VSV position disagrees with the
command).
L2 Engine stall may occur at any rapid thrust change.
AVOID THR CHANGES
ENG COMPRESSOR VANE
Applicable to:
, ,
MSN
L2 Engine 1 and 2 VBV or VSV motor fault detected on the standby ECU channel.
L1Crew awareness.
ENG 1(2) FUEL CTL FAULT
Applicable to: , , MSN
L2 Failure of Fuel Metering Valve.
L1 On ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
AVOID RAPID THR CHANGES, or
ENG (AFFECTED) SLOW RESPONSE
L2 Depending on the type of failure, one of the above two messages is displayed.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 114/194
FCOM 19 AUG 10
ENG 1(2) FUEL CTL FAULT
Applicable to:
L2 Failure of Fuel Metering Valve. Depending on the type of failure, one of the following two messages
is displayed:
L1 AVOID RAPID THR CHANGES, or
ENG (AFFECTED) SLOW RESPONSE
ENG 1(2) FUEL CTL FAULT
Applicable to:
L2 Failure of Fuel Metering Valve. Depending on the type of failure, one of the following two messages
is displayed:
L1 AVOID RAPID THR CHANGES, or
ENG (AFFECTED) SLOW RESPONSE
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 115/194
FCOM 19 AUG 10
ENG 1(2) FUEL CTL FAULT
Applicable to: MSN
4566,,,
FMV position disagreement:
L2Crew awareness.
L1
L2 Fuel Metering Valve position disagreement between the commanded position and the real one.
L1 Failure of FMV command or FMV position feedback:
ENG 1(2) MIN FUEL FLOW.
L2 FADEC is no longer able to control the fuel flow. It automatically sets a fail safe minimum fuel
flow corresponding to idle or sub-idle fuel flow which may result in an engine shut-down.
L1 THR LEVER (AFFECTED).................................................................................................... IDLE
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(155)
