See engine specification
The fuel system has been certified with JET A1, JET A, JP 5, and JP 8.
| GENERAL |
This Topic is relevant to the whole fleet
FUEL AND ADDITIVE SPECIFICATIONS
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See engine specification |
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The fuel system has been certified with JET A1, JET A, JP 5, and JP 8. |
MAXIMUM ALLOWABLE WING FUEL IMBALANCE
Maximum allowed wing fuel imbalance in either inner or outer tanks at takeoff, landing and in flight.
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INNER TANKS
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OUTER TANKS
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Tank content (heavier tank)
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Authorized asymmetry
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Tank content (heavier tank)
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Authorized asymmetry
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FULL
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2 900 kg (6400 lb)
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FULL
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1 480 kg (3260 lb)
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HALF
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4 800 kg (10500 lb)
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2400 kg (5290 lb)
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1 580 kg (3480 lb)
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7 500 kg (16500 lb)
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7 500 kg (16500 lb)
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1 730 kg (3810 lb)
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1 730 kg (3810 lb)
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The variation is linear between these values.
(No limitation below 7500 kg (16500 lb) for inner tanks and 1730 kg (3810 lb) for outer tanks).
FUEL TEMPERATURE
| Maximum fuel temperature | : | JET A, JET A1, JP 8 and JP 5 :
+ 55°C |
| Minimum fuel temperature | : | Freezing point |
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 :
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JET A1
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JET A
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JP 5
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JP 8
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- 47°C
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- 40°C
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- 46°C
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- 47°C
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MINIMUM FUEL QUANTITY FOR TAKEOFF : 5 200 kg (11460 lb)
WING TK LO LVL warning must not be displayed on ECAM for takeoff.
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