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DSC-28-20 CONTROLS AND INDICATORS
OVERHEAD PANEL......................................................................................................................................... 1/24
REFUELING CONTROL PANEL........................................................................................................................ 4/24
MAINTENANCE PANEL................................................................................................................................... 8/24
ECAM FUEL PAGE........................................................................................................................................ 10/24
ECAM UPPER DISPLAY................................................................................................................................ 22/24
DSC-28-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS.......................................................................................................................... 1/16
DSC-28-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
PRELIMINARY PAGES - TABLE OF CONTENTS
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A318/A319/A320/A321 FLEET DSC-28-PLP-TOC P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - GENERAL
A318/A319/A320/A321 FLEET DSC-28-10-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to:
MSN,
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.
GENERAL
Applicable to: ,
, MSN,,
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).
‐ Controls the transfer of fuel from the center tank to the wing tanks.
‐ Circulates fuel to cool the Integrated Drive Generator (IDG).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - GENERAL
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A318/A319/A320/A321 FLEET DSC-28-10-10 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - TANKS
A318/A319/A320/A321 FLEET DSC-28-10-20 P 1/2
FCOM 19 AUG 10
TANKS
Applicable to:
MSN,
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 °C
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.
USABLE FUEL
OUTER TANKS INNER TANKS CENTER TANK TOTAL
VOLUME (US(l igtearlslo)ns)02 xx 22 1649 xx 22 2800 23682
WEIGHT (1) (KG) 691 x 2 5 435 x 2 6 476 18 728 (LB) 1 520 x 2 11 982 x 2 14 281 41 285
(1) Fuel density : 0.785 kg/l or 6.551 lb/US Gal.
TANKS
Applicable to: ,
, MSN,,
Tanks in the wings and the center section store fuel.
There is a vent surge tank outboard of each wing tank.
When the aircraft has been refueled to maximum capacity, the fuel can expand by 2 % (20 °C
temperature rise) without spilling.
There is an overpressure protector in each vent and wing tank, and between the center tank and the
left wing tank.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - TANKS
A318/A319/A320/A321 FLEET DSC-28-10-20 P 2/2
FCOM 19 AUG 10
USABLE FUEL
WING TANKS CENTER TANK TOTAL
VOLUME (US(l igtearlslo)ns) 22 xx 2707 2806 23600
WEIGHT(1) (KG) 2 x 6 084 6 437 18 605 (LB) 2 x 13 410 14 190 41 010
(1) Fuel density : 0.785 kg/l or 6.551 lb/US Gal.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - ENGINE FEED
A318/A319/A320/A321 FLEET DSC-28-10-30 P 1/12
FCOM 19 AUG 10
GENERAL
Applicable to:
MSN,
The main fuel pump system supplies fuel from the center tank or the inner wing tanks to the engines.
The system has six main fuel pumps.
GENERAL
Applicable to: ,
, MSN,,
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 3(49)
