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L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Apply the after ENG SHUT DOWN procedure (Refer to PRO-ABN-70-B After ENG
1(2) SHUT DOWN ) If damage, or if engine relight is unsuccessful.
In flight:
If ENG FIRE pb not pressed:
ENG START SEL..............................................................................................................IGN
L2 Selection of continuous ignition confirms the FADEC’s immediate relight attempt.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 4/196
FCOM 19 AUG 10
ENG 1(2) FAIL (Cont'd)
L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
L2Note: In the case of GPWS (EGPWS ) alerts, reduce speed with care below VLS with
the flaps extended (at light weights VMC may be reached before α max), 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
L2 If the ENG FIRE pb is pushed, the FADEC is no longer supplied.
L1 AGENT 1 AFT 10 S.....................................................................................................DISCH
L+R INR TK SPLIT............................................................................................................ ON
L2Note: If no fuel leak is evident, set both INR TK SPLIT pb-sw back to the normal
position.
L1 IF NO DAMAGE:
ENG (AFFECTED) RELIGHT...............................................................................CONSIDER
L2 Apply the ENG RELIGHT (in flight) procedure (Refer to PRO-ABN-70 ENG RELIGHT (in
flight)).
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Apply the After ENG SHUT DOWN procedure (Refer to PRO-ABN-70-B After ENG
1(2) SHUT DOWN ) If damage, or if engine relight is unsuccessful.
If high engine vibrations occur and continue after engine shutdown, reduce airspeed
and descend to a safe altitude.
Attempt to define, and use, a practical airspeed and altitude for minimum vibrations.
For performance reasons, the landing is in CONF 3. CONF 3 should be selected, as
the landing configuration, on the MCDU.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 5/196
FCOM 19 AUG 10
ENG 1(2) FAIL
Applicable to: ,
L2 An engine flame-out may be recognized by a rapid decrease in EGT, N2, FF, followed by a
decrease in N1.
Engine damage may be accompanied by:
‐ Explosions
‐ Significant increase in aircraft vibrations and/or buffeting
‐ Repeated, or uncontrollable engine stalls
‐ Associated abnormal indications, such as hydraulic fluid loss, no N2 or N3 indication.
L1 In case of an N1 shaft rupture:
SHAFT FAILURE
L2 The FADEC automatically shuts down the engine.
L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
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
L+R INR TK SPLIT............................................................................................................ ON
IF NO DAMAGE:
ENG (AFFECTED) RELIGHT...............................................................................CONSIDER
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Apply the after ENG SHUT DOWN procedure (Refer to PRO-ABN-70-B After ENG
1(2) SHUT DOWN ) If damage, or if engine relight is unsuccessful.
In flight:
ENG START SEL.................................................................................................................... IGN
L2 Selection of continuous ignition confirms the FADEC’s immediate relight attempt.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(125)
