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L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
L2Note: In case of GPWS (EGPWS ) alerts, reduce speed with care below VLS with flaps
extended (at light weights VMC may be reached before αMax) when applying the
GPWS (EGPWS ) procedure.
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 51/194
FCOM 19 AUG 10
ENG 1(2) FAIL (Cont'd)
L1 IF NO ENG RELIGHT AFTER 30 S:
ENG MASTER (AFFECTED ENGINE)............................................................................ OFF
IF DAMAGE:
ENG FIRE P/B (AFFECTED ENGINE)...................................................................PUSH
AGENT 1 (AFTER 10 SECONDS IN FLIGHT)..................................................... DISCH
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
If damage or if engine relight unsuccessful.
If high vibration occurs and continues after engine shutdown, reduce airspeed
and descent to a safe altitude
Attempt to determine and use a practical airspeed and altitude for minimum
vibrations.
IF NO DAMAGE:
ENG (AFFECTED) RELIGHT........................................................................ CONSIDER
L2 If there is no damage, an engine relight can be considered. To restart the engine, Refer
to PRO-ABN-70 ENG RELIGHT (in flight)apply ENG procedure.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 52/194
FCOM 19 AUG 10
ENG 1(2) FAIL
Applicable to:
, ,
MSN
L2 An engine flame-out may be recognized by a rapid decrease in EGT, N2, FF, followed by decrease
in N1.
Engine damage may be accompanied by:
‐ Loud noise,
‐ Significant increase in aircraft vibrations and/or buffeting,
‐ Repeated or uncontrollable engine stalls,
‐ Associated abnormal indications such as hydraulic fluid loss, or no N2 indication.
L1 LAND ASAP
Before takeoff or after landing:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
IF DAMAGE:
ENG FIRE P/B (AFFECTED ENGINE)......................................................................... PUSH
AGENT 1...................................................................................................................... DISCH
IF NO DAMAGE:
L2 If conditions permit, do not restart the engine. A new engine start would erase FADEC
troubleshooting data.
L1 ENG (AFFECTED) RELIGHT...............................................................................CONSIDER
L2 If no damage, a new start sequence may be initiated.
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
If damage or if engine relight is unsuccessful.
L1 In flight:
ENG MODE SEL..................................................................................................................... IGN
L2 Selection of continuous ignition confirms the immediate relight attempt made by the FADEC.
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 53/194
FCOM 19 AUG 10
ENG 1(2) FAIL (Cont'd)
L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
L2Note: In case of GPWS (EGPWS ) alerts, reduce speed with care below VLS with flaps
extended (at light weights VMC may be reached before αMax) when applying the
GPWS (EGPWS ) procedure.
L1 IF NO ENG RELIGHT AFTER 30 S:
ENG MASTER (AFFECTED ENGINE)............................................................................ OFF
IF DAMAGE:
ENG FIRE P/B (AFFECTED ENGINE)...................................................................PUSH
AGENT 1 (AFTER 10 SECONDS IN FLIGHT)..................................................... DISCH
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
If damage or if engine relight unsuccessful.
If high vibration occurs and continues after engine shutdown, reduce airspeed
and descent to a safe altitude
Attempt to determine and use a practical airspeed and altitude for minimum
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(136)
