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FCOM 19 AUG 10
ENG RELIGHT (Cont'd)
(IN FLIGHT)
IN FLIGHT ENGINE RELIGHT ENVELOPE
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 9/196
FCOM 19 AUG 10
ENG RELIGHT
(IN FLIGHT)
Applicable to: ,
MAX GUARANTEED ALTITUDE.........................................................................................30 000 FT
ENG MASTER (affected engine).................................................................................................. OFF
THR LEVER (affected engine).......................................................................................... check IDLE
MAN START pb (affected engine)................................................................................................OFF
Note: Auto start is recommended in flight.
Be aware that, unlike the procedure for auto start on the ground, the crew must take
appropriate action in case of abnormal start.
ENG START SEL...........................................................................................................................IGN
X BLEED.................................................................................................................................. OPEN
If outside windmilling start envelope, FADEC opens starter valve.
WING ANTI ICE (for starter assisted start).................................................................................. OFF
ENG MASTER...............................................................................................................................ON
Note: Engine light up must be achieved within 30 s after fuel flow increases.
‐ Monitor N2
‐ If uncertain about successful relight, move the thrust lever forward and check engine
response.
�� When idle reached (AVAIL indication pulses in green):
ENG START SEL................................................................................................................NORM
TCAS MODE SEL �� ............................................................................................Check TA/RA
Check that the selector is at TA/RA since if the ENG SHUT DOWN procedure has been
applied, the TCAS mode selector may have been set at TA position.
Affected SYS................................................................................................................ RESTORE
Restore affected systems and set XBLEED selector at AUTO.
�� If no relight:
ENG MASTER (affected engine)............................................................................................OFF
Wait 30 s before new start attempt (to drain the engine).
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 10/196
FCOM 19 AUG 10
ENG RELIGHT (Cont'd)
(IN FLIGHT)
(1) STARTER ASSIST or QUICK RELIGHT if SHUT DOWN time ≤ 30 s.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 11/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) SHUT DOWN
Applicable to:
LAND ASAP
L2 Displayed, if more than one engine shuts down.
L1�� If ENG FIRE pb not pressed:
ENG START SEL.................................................................................................................... IGN
L2Continuous ignition is selected to protect the remaining engines.
L1
L2Note: If the Y ELEC PUMP is running after ENG 3 failure (engine failure before flaps retraction),
switch OFF the pump, when in clean configuration.
L1 L/G (DISPLAYED DURING THE TAKEOFF PHASE).....................................................................UP
FUEL IMBALANCE..............................................................................................................MONITOR
TCAS MODE SEL �� ....................................................................................................................TA
L12
SECONDARY FAILURES
* HYD
* ELEC
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 12/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) SHUT DOWN (Cont'd)
NL2ote: ‐ In case a second
engine fails,
the *HYD and
*ELEC secondary
failures are not
automatically
recalled, if cleared,
after the first engine
failure
‐ In some conditions
with full asymmetric
power, the
aircraft may be
control-limited
before reaching
the limit of the
protection system.
　
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