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Note: If the trim tank pump is failed or not installed, this part of the procedure is replaced by:
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................................... FWD
L1�� WHEN EITHER INR < 17 T:
L + R CTR PUMPS..................................................................................................................ON
L12
STATUS
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed if the trim tank pumps is failed or not installed.
FUEL WING TK OVERFLOW
Applicable to:
L + R CTR PUMPS.......................................................................................................................OFF
L2 To stop the center to inner transfer.
L1 T TANK MODE (ONLY IF CTR TANK EMPTY)..........................................................................FWD
L2 To force transfer into the center tank and prevent forward transfer into the inner tanks.
Note: If the trim tank pump is failed, this part of the procedure is replaced by:
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................................... FWD
L1�� WHEN EITHER INR < 17 T:
L + R CTR PUMPS..................................................................................................................ON
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 21/98
FCOM 19 AUG 10
FUEL WING TK OVERFLOW (Cont'd)
L12
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed if the trim tank pump is failed.
FUEL WING TK OVERFLOW
Applicable to:
L + R CTR PUMPS.......................................................................................................................OFF
L2 To stop the center to inner transfer.
L1 T TANK MODE (ONLY IF CTR TANK EMPTY)..........................................................................FWD
L2 To force transfer into the center tank and prevent forward transfer into the inner tanks.
Note: If the trim tank pump is failed or not installed, this part of the procedure is replaced by:
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................................... FWD
L1�� WHEN EITHER INR < 17 T:
L + R CTR PUMPS..................................................................................................................ON
L + R CTR PUMPS.......................................................................................................................OFF
L2 To stop the center to inner transfer.
L1 T TANK MODE (ONLY IF CTR TANK EMPTY)..........................................................................FWD
L2 To force transfer into the center tank and prevent forward transfer into the inner tanks.
Note: If the trim tank pump is failed, this part of the procedure is replaced by:
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................................... FWD
L1�� WHEN EITHER INR < 17 T:
L + R CTR PUMPS..................................................................................................................ON
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 22/98
FCOM 19 AUG 10
FUEL WING TK OVERFLOW (Cont'd)
L12
STATUS
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed if the trim tank pumps is failed or not installed.
L12
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed if the trim tank pump is failed.
FUEL WING TK OVERFLOW
Applicable to:
T TANK FEED............................................................................................................................ISOL
L2 To prevent forward transfer into the inner tanks.
L1�� WHEN EITHER INR < 17 T:
T TANK FEED..................................................................................................................... AUTO
FUEL JETTISON FAULT
Applicable to: ,
L2 Jettison system is inhibited
L1 JETTISON NOT AVAIL
A330/A340 FLIGHT CREW
OPERATING MANUAL
　
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