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L2 Apply the ENG RELIGHT (in flight) procedure
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUTDOWN
Apply the After ENG SHUTDOWN procedure if engine relight is not successful.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 13/98
FCOM 19 AUG 10
FUEL ENG 1(2) FEEDLINE BURST (Cont'd)
STATUS
DO NOT OPEN WING X FEED
�� FOR GRVTY FEED:
�� If flight time from takeoff more than 30 min:
MAX FL...............................................................200/MEA
�� If flight time from takeoff less than 30 min:
MAX FL...............................................................150/MEA
�� IF JP4/JET B FUEL:
MAX FL.......................................................... 70/MEA
�� AT GRVTY FEED CEILING:
ENG 1(2) RELIGHT.............................................. CONSIDER
L(R) FUEL GRVTY FEED ONLY
INOP SYS
FUEL AFT XFR
L(R) FUEL PUMPS
FUEL L + R CTR PUMPS LO PR
Applicable to: ,
L + R CTR PUMPS.......................................................................................................................OFF
�� WHEN EITHER INR < 17 T:
CTR TANK XFR.....................................................................................................................MAN
CTR TK XFR BY GRVTY
CTR TK UNUSABLE IF < 15 T
L2Note: The trim tank fuel is directly transferred to the inner tanks.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 14/98
FCOM 19 AUG 10
FUEL L + R CTR PUMPS LO PR (Cont'd)
STATUS
CTR TK UNUSABLE IF < 15 T INOP SYS
FUEL AFT XFR (1)
F CTR PUMPS
(1) (only if CTR TK not empty)
GRVTY FUEL FEEDING
Applicable to:
ENG START SEL...........................................................................................................................IGN
AVOID NEGATIVE G FACTOR
�� DETERMINE GRVTY FEED CEILING:
Refer to the following table to determine the flight altitude limitation.
Flight conditions at the time of gravity feeding Gravity feed ceiling
Flight time from takeoff more than 30 min (Fuel deaerated) 20 000 ft (1)
Flight time from takeoff less than
30 min (Fuel non–deaerated) 15 000 ft (1)
(1) In case JP4 or JET B fuel is used, the gravity feed ceiling is the highest altitude between 4 000 ft above sea level
and 2 000 ft above the takeoff airport altitude.
DESCEND TO GRVTY FEED CEILING (if applicable)
�� WHEN REACHING GRVTY FEED CEILING:
FUEL X FEED 1+2+3+4....................................................................................................CLOSE
Crossfeed valves close, except in EMER ELEC configuration.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 15/98
FCOM 19 AUG 10
GRVTY FUEL FEEDING
Applicable to: ,
ENG START SEL...........................................................................................................................IGN
AVOID NEGATIVE G FACTOR
�� DETERMINE GRVTY FEED CEILING:
Refer to the following table to determine the flight altitude limitation.
Flight conditions at the time of gravity feeding Gravity feed ceiling
Flight time from takeoff more than 30 min(Fuel deaerated) 20 000 ft
Flight time from takeoff less than
30 min (Fuel non-deaerated)
15 000 ft
8 000 ft for JP4 or JET B
DESCEND TO GRVTY FEED CEILING (if applicable)
�� WHEN REACHING GRVTY FEED CEILING:
WING X FEED...................................................................................................................CLOSE
INR UNUSABLE IF < 2 T (4 400 lb)
2 000 kg (4 400 lb) of fuel per affected tank cannot be used by gravity.
FUEL ENG 1(2)(3)(4) LP VALVE FAULT
Applicable to:
L2 Valve position disagree.
Crew awareness.
FUEL ENG 1(2) LP VALVE FAULT
Applicable to: ,
L2 Valve open or closed disagree
Crew awareness
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 16/98
FCOM 19 AUG 10
FUEL APU LP VALVE FAULT
Applicable to: ALL
L2 Valve position disagree.
Crew awareness.
FUEL X FEED 1(2)(3)(4) FAULT
Applicable to:
L2 Valve position disagree.
Crew awareness.
STATUS
INOP SYS
F. X FEED1(2)(3)(4) FUEL AFT
XFR (1)
(1) (Only if F..X FEED 2 or 3 is failed)
FUEL WING X FEED FAULT
　
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