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�� In flight:
AVOID RAPID THR CHANGES.
AVOID RAPID THR CHANGES.
ENG 1(2) SENSOR FAULT
Applicable to: ,
MSN
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 120/194
FCOM 19 AUG 10
ENG 1(2) SENSOR FAULT
Applicable to: MSN
4566,,,
L2N1 or N2 or fuel metering valve position disagree between both EEC channels or Loss of N1 or N2
sensors.
L1 AVOID RAPID THR CHANGES
�� On ground:
THR LEVER (AFFECTED).................................................................................................... IDLE
ENG MASTER (AFFECTED)..................................................................................................OFF
AVOID RAPID THR CHANGES.
ENG 1(2) PROBES FAULT
Applicable to:
, ,
MSN
L2 P0, PT2, T12 data not available on both ECU channels.
Crew awareness.
ENG 1(2) FUEL RETURN VALVE
Applicable to:
, ,
MSN
�� VALVE NOT OPEN
L2 The valve is failed closed.
Crew awareness.
L1�� VALVE NOT CLOSED
L2 The valve is failed open.
Crew awareness.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 121/194
FCOM 19 AUG 10
ENG 1(2) AIR EXCHANGER FAULT
Applicable to: MSN
4566,,,
L2 Failure of air/oil heat exchanger valve on ground.
Depending of the failure one of the following messages is displayed:
L1 AIR VALVE OPEN
Refer to 99 Duref Cible MEL.
AIR VALVE CLOSED
ENG 1(2) FUEL HEAT SYS
Applicable to: MSN
4566,,,
FUEL RETURN VALVE OPEN.
FUEL DIVERTER VALVE.
TEMPS SENSORS
L2Maintenance 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 122/194
FCOM 19 AUG 10
ENG DUAL FAILURE
Applicable to:
L2 The ENG DUAL FAILURE warning inhibits the ELEC EMER CONFIG warning.
The FCOM Volume 3 includes all steps of the ECAM ENG DUAL FAILURE procedure.
However, to facilitate handling of all the ECAM procedures associated with a dual engine failure,
it is recommended using the QRH ENG DUAL FAILURE paper procedure that also includes the
DITCHING and FORCED LANDING procedures. When applying the QRH ENG DUAL FAILURE
paper procedure:
If one or more engines are recovered, apply the corresponding ‐ ECAM procedure instead
‐ If no engines are recovered, continue to apply the QRH ENG DUAL FAILURE paper procedure.
If time permits, clear ECAM alerts, and check the STATUS SD page.
L1 LAND ASAP
ENG MODE SEL............................................................................................................................IGN
L2 An immediate relight attempt is made.
L1 THR LEVERS............................................................................................................................. IDLE
OPTIMUM RELIGHT SPD........................................................................................................300 KT
L2 The optimum airspeed to allow an effective windmilling start attempt is 300 kt.
In case of a speed indication failure (volcanic ash), the pitch attitude for optimum relight speed is
4.5 degrees down. For weight above 50 000 kg/110 000 lb , raise the nose by 1 degree for every
additional 10 000 kg/22 000 lb (e.g. if weight is 60 000 kg/132 000 lb pitch is 3.5 ° down).
At 300 kt, the aircraft can fly up to about:
‐ 2.0 nm per 1 000 ft at 50 000 kg/110 000 lb
‐ 2.2 nm per 1 000 ft at 60 000 kg/132 000 lb
‐ 2.4 nm per 1 000 ft at 70 000 kg/154 000 lb
L1 EMER ELEC PWR (IF EMER GEN NOT IN LINE)...............................................................MAN ON
L2 Pressing EMER ELEC PWR MAN ON pb allows extension of RAT and emer gen coupling.
L1 VHF 1/HF 1 �� /ATC 1.............................................................................................................. USE
L2‐ In Elec emer configuration only VHF 1, HF 1 �� and ATC 1 are supplied.
L12‐ Notify traffic control of the nature of the emergency and state intention.
If there is no contact with air traffic control, switch to code A7700 or transmit a distress message
　
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