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�� In flight:
�� IF ENG (affected) NOT AT IDLE:
ENG MASTER (AFFECTED).....................................................................................OFF
�� On the ground:
ENG MASTER (AFFECTED)........................................................................................... OFF
STATUS
APPR PROC
REV (AFFECTED).................................................. DO NOT USE
�� AFTER TOUCH DOWN:
THR LEVER (AFFECTED)...............................................IDLE
ENG MASTER (AFFECTED) ...........................................OFF
ENG (affected) MIN FUEL FLOW.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 116/194
FCOM 19 AUG 10
ENG 1(2) OVSPD PROT FAULT
Applicable to:
, ,
MSN
L2Crew awareness.
Note: If the warning appears during engine start, shut down the engine. Restart the engine. If
the warning still appears, maintenance action is due.
ENG 1(2) OVSPD PROT FAULT
Applicable to: MSN
4566,,,
L2 The automatic fuel flow restriction in case of engine N1 or N2 overspeed may not be available.
Fault was detected during last engine shut down.
Some cases of spurious fault detection have been experienced.
The caution can be considered as spurious if it disappears after application of the following
procedure:
Enter a new FLT NBR on INIT page on MCDU (‐ to change the maintenance phase)
‐ Start the affected engine and wait for 4 min at idle
‐ Then switch off the affected ENG GEN and shutdown the engine.
Crew awareness.
ENG 1(2) HOT FUEL
Applicable to: MSN
4566,,,
GEN 1(2)..................................................................................................................................... OFF
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 117/194
FCOM 19 AUG 10
ENG 1(2) HOT FUEL (Cont'd)
STATUS
CAT 3 SINGLE ONLY. INOP SYS
GEN 1(2)
MAIN GALLEY (1)
CAT 3 DUAL
(1) (Only if APU GEN not in line)
ENG 1(2) CTL VALVE FAULT
Applicable to:
L2 Failure of Burner staging valve or HP Turbine clearance system or RACC system.
L1MAX N2......................................................................................................................................96 %
L2 Retard associated thrust lever to limit N2 to 96 %.
MAX ENG (AFFECTED) N2.................................................. 96 %
ENG 1(2) CTL VALVE FAULT
Applicable to: ,
L2 Failure of Burner staging valve or HP Turbine clearance system or RACC system.
L1MAX N2......................................................................................................................................96 %
L2 Retard associated thrust lever to limit N2 to 96 %.
MAX ENG (AFFECTED) N2.................................................. 96 %
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 118/194
FCOM 19 AUG 10
ENG 1(2) CTL VALVE FAULT
Applicable to: ,
MSN
L2 Failure of Burner staging valve or HP Turbine clearance system or RACC system.
L1MAX N2......................................................................................................................................96 %
L2 Retard associated thrust lever to limit N2 to 96 %.
MAX ENG (AFFECTED) N2.................................................. 96 %
ENG 1(2) SENSOR FAULT
Applicable to:
L2 PS3, T25, T3, N1, N2 data not available on both ECU channels.
L1�� On ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
�� In flight:
AVOID RAPID THR CHANGES.
AVOID RAPID 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 119/194
FCOM 19 AUG 10
ENG 1(2) SENSOR FAULT
Applicable to: ,
L2 PS3, T25, T3, N1, N2 data not available on both ECU channels.
L1�� On ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
　
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