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┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 203 I ┃I REV 25 ┃
┃ A~7-~'M" .4321 ┃DESCRIPTION ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
The fuel system :
- stores fuel in the tanks
- supplies fuel in the correct quantities to the fuel tanks during refueling
- supplies fuel to the engines and the auxiliary power unit (APU)
- circulates fuel to cool the integrated drive generator (IDG)
- keeps fuel in the outer wing for wing bending and flutter relief.
The fuel is stored in the wings and the center section. The wings have inner and outer
tanks.
There is a vent surge tank outboard of the outer tank in each wing.
When the aircraft has been refueled to maximum capacity, the fuel can expand by 2 % (20~
temperature rise) without spilling.
There is an overpressure protector in each vent outer and inner tank and between the
center tank and the left inner tank.
INNER CENTER INNER
TANK TANK TANK
┏━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┓
┃USABLE FUEL ┃
┣━━━━━━━━━━━━━┳━━━━━━┳━━━━━━┳━━━━━━┳━━━┫
┃ ┃OUTER TANKS ┃INNER TANKS ┃CENTER TANK ┃TOTAL ┃
┣━━━━━┳━━━━━━━╋━━━━━━╋━━━━━━╋━━━━━━╋━━━┫
┃ ┃(liters) ┃880 x 2 ┃6924 x 2 ┃8250 ┃23858 ┃
┃VOLUME ┃ ┃ ┃ ┃ ┃ ┃
┃ ┣━━━━━━━╋━━━━━━╋━━━━━━╋━━━━━━╋━━━┫
┃ ┃(US gallons) ┃232 x 2 ┃1829 x 2 ┃2180 ┃6302 ┃
┣━━━━━╋━━━━━━━╋━━━━━━╋━━━━━━╋━━━━━━╋━━━┫
┃ ┃(KG) ┃691 x 2 ┃5435 x 2 ┃6476 ┃18728 ┃
┃WEIGHT * ┃ ┃ ┃ ┃ ┃ ┃
┃ ┣━━━━━━━╋━━━━━━╋━━━━━━╋━━━━━━╋━━━┫
┃ ┃(Lg) ┃1520 x 2 ┃11982 x 2 ┃14281 ┃41285 ┃
┗━━━━━┻━━━━━━━┻━━━━━━┻━━━━━━┻━━━━━━┻━━━┛
* Fuel density ~ 0.785 kg/I or 6.551 Ib/US Ga
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.28.10 P 2 ┃
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual3(123)
