Fuel System Flashcards

1
Q

APU Fuel Feed

A

An APU fuel pump is provided to start the APU when the main tank pumps are off or normal AC power is unavailable.

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2
Q

Automatic Fuel Feed Sequence

A
  • Is fully automatic
  • with fuel in all tanks, the center tank
    Pumps provide feed to the engines
  • wing tank pumps operate continuously
    and are fitted with “Pressure Relief
    Sequencing Valves” to ensure that the
    center tank pumps, when running, have
    preferential priority.
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3
Q

When do the wing transfer valves open

A

When either wing inner compartment fuel quantity decreases below 1650 pounds

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4
Q

When do engine low pressure valves colse

A

Engine masters with is turned off

When engine fire switch is released

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5
Q

How does suction feed work

A

Suction valves in each inner wing tank are closed when boost pump pressure is normal. They open when pump pressure is low, allowing the engines to be gravity fed from the wing tanks only.

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6
Q

In flight, with fuel MODE SEL in AUTO and fuel in the center tank, the center tank pumps

A

Run only if slats are retracted

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7
Q

In flight, with the MODE SEL in MAN, and the CTR TK pumps ON, what is the effect on the center tank pumps?

A

The center tank pumps run continuously until turned off with the CTR TK pump switches.

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8
Q

A fuel pump FAULT light indicates

A

Fuel pump low fuel pressure

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9
Q

Resetting tripped wing tank fuel boost pump circuit breaker is prohibited.

A

At all times

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10
Q

A fuel MODE SEL FAULT light indicates

A

Center tank has more than 550 pounds of fuel and the left or right wing tank has less than 11,000 pounds

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11
Q

The cross feed valve is normally in the ____________ position

A

Closed

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12
Q

What do the double dashes ver the last two digits of the fuel on board (FOB) indication mean

A

The fuel quantity indication is still operative, but inaccurate

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13
Q

What would cause an amber half box to appear around the E/WD FOB display when the fuel quantity is not fully usable?

A

Both transfer valves on the side fail to open

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14
Q

Engines can gravity feed from

A

The wing tanks only

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15
Q

The over-pressure burst disk will rupture if

A

The internal and external pressure differential exceeds a predetermined value

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16
Q

If a fuel imbalance greater than 3300 pounds is detected, indications of the wing inner and outer tanks with the highest fuel level will

A

Pulse Green

17
Q

A low level fuel warning may be triggered during steep decent, acceleration or deceleration. The transfer valves may ___________
With more than ________________ pounds of fuel in one of the inner fuel tanks

A

OPEN

1650 Pounds

18
Q

When either inner wing compartment fuel quantity reaches

______________ pounds. At least one transfer valve in each wing opens

A

1650 pounds

19
Q

The fuel recirculation system uses fuel for

A

IDG Cooling

20
Q

IDG heat exchanger return fuel is routed to the fuel return valve and then to the

A

Wing tank outer compartments

21
Q

When fuel is supplied from the center tank, and recirculated fuel has filled the wing tank, the center tank pump shuts off until _______________ pounds of fuel has been burned out of the wing tanks

A

1100 pounds