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inadvertent fuel transfer from center to outer tanks
L1 If trim tank temp is less than -40 °C (auto recall at -47 °C):
IF JET A FUEL (not displayed at -47 °C):
T TANK MODE.........................................................................................................FWD
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 66/98
FCOM 19 AUG 10
FUEL FUEL LO TEMP (Cont'd)
L2Note: If trim tank pump fails, or is not installed, this part of the procedure is replaced
by:
WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................FWD
If the CG is forward 26 % MAC, the CG should be monitored during the
forward transfer, to ensure that forward CG limits are not exceeded.
Fuel consumption increases by approximately 1 %.
L1 IF NECESSARY:
TAT........................................................................................................................INCREASE
L2Consider descending to a lower altitude and/or increasing Mach to increase TAT.
L12
WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Only appears, if trim tank pump fails, or is not installed.
L12
WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Only appears, if the trim tank pump fails
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 67/98
FCOM 19 AUG 10
FUEL FUEL LO TEMP
Applicable to:
L2 This caution appears, as soon as the inner tank temperature is less than -37 °C, or outer or trim
tank temperature is less than -40 °C. However, at this threshold: Crew action is required for JET A
FUEL only, and no crew action is required for other fuel types.
For all other fuel types: This caution will automatically be recalled, if the temperature reaches
-44 °C (inner tank temp), or -47 °C (outer or trim tank temp).
Regardless of the fuel type, the flight crew may consider delaying application of the rest of
procedure, until reaching the minimum fuel temperature specific to their fuel type Refer to LIM-28
FUEL TEMPERATURE.
L1 FUEL FREEZE PT...................................................................................................................CHECK
On ground, before takeoff:
IF JET A FUEL:
DELAY T.O.
L2 Do not takeoff, until the temperature is within limits.
L1 In flight:
If inner tank temp is less than -37 °C (auto recall at -44 °C):
L2Crew awareness.
L1 If outer tank temp is less than -40 °C (auto recall at -47 °C):
IF JET A FUEL (not displayed at -47 °C):
OUTR TK XFR............................................................................................................ ON
If trim tank temp is less than -40 °C (auto recall at -47 °C):
IF JET A FUEL (not displayed at -47 °C):
T TANK MODE.........................................................................................................FWD
L2Note: If trim tank pump fails, or is not installed, this part of the procedure is replaced
by:
WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE....................................................................................FWD
Fuel consumption increases by approximately 1 %.
L1 IF NECESSARY:
TAT........................................................................................................................INCREASE
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 68/98
FCOM 19 AUG 10
FUEL FUEL LO TEMP (Cont'd)
L2Consider descending to a lower altitude and/or increasing Mach to increase TAT.
L12
WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Only appears, if the trim tank pump fails
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 69/98
FCOM 19 AUG 10
FUEL FCMC 1+2 FAULT
Applicable to:
L2 Transfers are controlled using the T TANK MODE pb-sw, and the OUTR XFR pb-sw.
L1 FCMC 1+2.............................................................................................................................. RESET
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(138)
