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PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 23/98
FCOM 19 AUG 10
FUEL JETTISON FAULT
Applicable to: MSN ,
,
L2 Jettison system is inhibited
L1 JETTISON NOT AVAIL
FUEL L(R) WING TK LO LVL
Applicable to:
CTR TANK XFR........................................................................................................................... MAN
OUTR TK XFR..............................................................................................................................ON
T TANK MODE...........................................................................................................................FWD
L2 If the trim tank pump is failed or not installed, check the pitch attitude is below 3 ° before the
forward transfer selection. After forward transfer, fuel consumption is increased by approximately
1 %.
L1�� IF NO FUEL LEAK:
X FEED 1+2 (3+4)....................................................................................................................ON
L2 Inner and outer engine collector cells are not located at the same level inside the wing.
Note: The crossfeed valves of the non affected side can also be opened provided it is
confirmed that there is no leak.
L12
STATUS
LVL OFF FOR MAN FWD XFR
Displayed if the trim tank pump is failed or not installed.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 24/98
FCOM 19 AUG 10
FUEL L(R) WING TK LO LVL
Applicable to:
�� If the center tank is not empty:
CTR TANK XFR.....................................................................................................................MAN
OUTR TK XFR..............................................................................................................................ON
�� If the TRIM TK not empty:
T TANK MODE...................................................................................................................... FWD
L2 Fuel consumption is increased by approximately 1 %.
L1�� IF NO FUEL LEAK AND IF FUEL IMBALANCE:
WING X FEED..........................................................................................................................ON
L(R) STBY PUMP (SIDE WITH LO LVL)...............................................................................OFF
LEFT (RIGHT) PUMPS 1 + 2 (SIDE WITH LO LVL)............................................................. OFF
L12
STATUS
LVL OFF FOR MAN FWD XFR
Displayed, if the trim tank pump is failed.
FUEL L(R) WING TK LO LVL
Applicable to:
CTR TANK XFR........................................................................................................................... MAN
OUTR TK XFR..............................................................................................................................ON
T TANK MODE...........................................................................................................................FWD
L2 If the trim tank pump is failed or not installed, check the pitch attitude is below 3 ° before the
forward transfer selection. After forward transfer, fuel consumption is increased by approximately
1 %.
L1�� IF NO FUEL LEAK:
X FEED 1+2 (3+4)....................................................................................................................ON
L2 Inner and outer engine collector cells are not located at the same level inside the wing.
Note: The crossfeed valves of the non affected side can also be opened provided it is
confirmed that there is no leak.
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 25/98
FCOM 19 AUG 10
FUEL L(R) WING TK LO LVL (Cont'd)
�� If the center tank is not empty:
CTR TANK XFR.....................................................................................................................MAN
OUTR TK XFR..............................................................................................................................ON
�� If the TRIM TK not empty:
T TANK MODE...................................................................................................................... FWD
L2 Fuel consumption is increased by approximately 1 %.
L1�� IF NO FUEL LEAK AND IF FUEL IMBALANCE:
WING X FEED..........................................................................................................................ON
L(R) STBY PUMP (SIDE WITH LO LVL)...............................................................................OFF
　
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