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fuel boost pump switches, any fuel tank can supply fuel to the
APU.
Defuel System
The defuel system permits the removal of fuel from each tank. It
also permits the transfer of fuel between tanks on the ground.
FUEL SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
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Fuel Quantity Indicating System
The fuel quantity indicating system (FQIS) shows fuel weight of
the main tanks and the center tank on the common display
system (CDS) and the P15 refuel panel.
Total fuel weight shows in the flight management computer
system (FMCS) data on the CDU.
Fuel Temperature Indicating System
Main tank 1 fuel temperature shows on the fuel control panel.
FUEL SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
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FUEL SYSTEM - GENERAL DESCRIPTION
FUEL SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
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FUEL SYSTEM - GENERAL DESCRIPTION
FUEL SYSTEM - GENERAL DESCRIPTION
EFFECTIVITY
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28-00-00-001
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FUEL SYSTEM - GENERAL DESCRIPTION
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Fuel Tank Arrangement
These are the fuel tanks:
* Main tank 1
* Main tank 2
* Center tank.
Surge tanks collect fuel overflow only. The fuel overflow in the
left wing surge tank drains to main tank 1. The fuel overflow in
the right wing surge tank drains to main tank 2. If the fuel level is
high enough in the surge tank fuel drains out the vent scoop.
Component Location
Main tank 1 is in the wing box of the left wing. Main tank 2 is in
the wing box of the right wing. The center tank is in the fuselage
and the left and right wing root.
Capacity
The capacity of main tank 1 is 8,630 lbs (3,915 kgs). The capacity
of main tank 2 is 8,630 lbs (3,915 kgs). The capacity of the center
tank is 28,803 lbs (13,066 kgs). Fuel tank capacity does not
include surge tanks.
The capacity of each surge tank is 235 lbs (107 kgs).
FUEL STORAGE - GENERAL DESCRIPTION
EFFECTIVITY
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28-10-00-000
FUEL STORAGE - GENERAL DESCRIPTION
FUEL STORAGE - GENERAL DESCRIPTION
EFFECTIVITY
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28-10-00-000
FUEL STORAGE - GENERAL DESCRIPTION
FUEL STORAGE - GENERAL DESCRIPTION
EFFECTIVITY
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FUEL STORAGE - GENERAL DESCRIPTION
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General
Wing fuel tank access panels permit entry into each fuel and
surge tank. The wing fuel tank access panels are on the bottom
wing skin. One center tank access panel permits entry into the
center tank through the fuselage. This panel is in the left air
conditioning compartment.
Wing ribs divide the fuel tanks into bays. Wing fuel tank access
panels are between the wing ribs. Access across wing ribs to
adjacent bays is through cutouts.
Wing rib 8, in main tank 1 and main tank 2, has check valves.
The check valves let fuel flow inboard but do not let fuel flow
　
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