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MINIMUM FUEL QUANTITY FOR TAKEOFF : 5400 kg (11900 lb).....................................................................3/4
MINIMUM FUEL QUANTITY FOR TAKEOFF : 5200 kg (11460 lb).....................................................................3/4
TEMPERATURE LIMIT USING JP 4 TO ENSURE ADEQUATE JET PUMP PERFORMANCE..........................3/4
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
FUEL
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A330/A340 FLEET LIM-28-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
FUEL
A330/A340 FLEET LIM-28 P 1/4
FCOM 19 AUG 10
FUEL AND ADDITIVE SPECIFICATIONS
Applicable to:
‐ See CFM specification.
‐ The fuel system has been certified with JET A, JET A1, JP 8, JET B, JP4 and JP 5.
FUEL AND ADDITIVE SPECIFICATIONS
Applicable to: ,
‐ See engine specification.
‐ The fuel system has been certified with JET A, JET A1, JET B, JP 4, JP 5, JP 8, N°3 JET and
TS-1.
MAXIMUM ALLOWED WING FUEL IMBALANCE
Applicable to:
Maximum allowed wing fuel imbalance in either inner or outer tanks at takeoff, landing and in flight.
INNER TANKS (OUTER BALANCED) OUTER TANKS (INNER BALANCED)
Tank content
(heavier tank)
Maximum allowed
imbalance
Tank content
(heavier tank)
Maximum allowed
imbalance
FULL 34 500 kg
(76 100 lb)
2 300 kg
(5 100 lb)
FULL 3 000 kg
(6 600 lb)
1 300 kg
(2 850 lb)
HALF 17 000 kg
(37 500 lb)
3 700 kg
(8 200 lb)
1 400 kg
(3 100 lb)
1 400 kg
(3 100 lb)
6 100 kg
(13 400 lb)
6 100 kg
(13 400 lb)
_ _
The variation is linear between these values. (No limitation below 6 100 kg (13 400 lb) for the inner
tanks and 1 400 kg (3 100 lb) for the outer tanks).
Note: In exceptional conditions (i.e., fuel system failures) the above-mentioned maximum fuel
imbalance values may be exceeded without significantly affecting the aircraft handling
qualities. The aircraft remains fully controllable in all phases of the flight.
MAXIMUM ALLOWED WING FUEL IMBALANCE
Applicable to: ,
Maximum allowed wing fuel imbalance in either inner or outer tanks at takeoff, landing and in flight.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
FUEL
A330/A340 FLEET LIM-28 P 2/4
FCOM 19 AUG 10
INNER TANKS (OUTER BALANCED) OUTER TANKS (INNER BALANCED)
Tank content
(heavier tank) Authorized asymmetry Tank content
(heavier tank) Authorized asymmetry
FULL 2 900 kg
(6 400 lb) FULL 1 480 kg
(3 260 lb)
HALF 4 800 kg
(10 500 lb)
2 400 kg
(5 290 lb)
1 580 kg
(3 480 lb)
7 500 kg
(16 500 lb)
7 500 kg
(16 500 lb)
1 730 kg
(3 810 lb)
1 730 kg
(3 810 lb)
The variation is linear between these values. (No limitation below 7 500 kg (16 500 lb) for inner tanks
and 1 730 kg (3 810 lb) for outer tanks).
Note: In exceptional conditions (i.e., fuel system failures) the above-mentioned maximum fuel
imbalance values may be exceeded without significantly affecting the aircraft handling
qualities. The aircraft remains fully controllable in all phases of the flight.
FUEL TEMPERATURE
Applicable to:
Maximum fuel temperature : JET A, JET A1, JP 8 and JP 5 : +60 °C
JP 4, JET B : +49 °C
Minimum fuel temperature : Freezing point +5 °C in inner tank.
Freezing point in outer or trim tank.
If the actual fuel freezing point of the fuel being used for the flight is unknown, the fuel specification
freezing point provided hereafter must be used :
JET A1 JET A JET B JP 4 JP 8 JP 5
-47 °C -40 °C -50 °C -58 °C -47 °C -46 °C
FUEL TEMPERATURE
Applicable to: ,
Maximum fuel temperature : JET A, JET A1, JP 5, JP 8, N°3 JET and TS-1: +55 °C
JP 4, JET B : +49 °C
Minimum fuel temperature : Freezing point or -44 °C below30 000 ft or -54 °C above 30 000 ft
whichever is the higher in inner tank.
Freezing point in outer or trim tank.
If the actual fuel freezing point of the fuel being used for the flight is unknown, the fuel specification
freezing point provided hereafter must be used :
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
FUEL
A330/A340 FLEET LIM-28 P 3/4
FCOM 19 AUG 10
JET A JET A1 JP 5 JP 8 N°3 JET TS-1 JP 4 JET B
-40 °C -47 °C -46 °C -47 °C -47 °C -50 °C -58 °C -50 °C
FUEL MANAGEMENT
Applicable to: ,
Tanks must be emptied in the following ‐ order : Center tank, then wing tanks.
　
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