*Fuel-Fuel Panel Flashcards

1
Q

*What is the normal in-flight fuel management scheme?

A

Use center tank first, then the wings

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2
Q

*How many fuel pumps are installed?

A

-2 in each inner wing tank.
-2 in the center tank.
-1 APU pump to provide fuel to the APU when the tank pumps are off.
-2 center tank transfer pumps (Tails 246-257 and 276)

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3
Q

*When the Center Tank Pump MODE Select pb is in the AUTO mode (lights out), what is the logic for center tank operation?

4
*different from training supplement. (pg. 77)

A

-With fuel in the center tank the pumps will:
1-Perform a momentary self-test after engine start.
2-The pumps stop operating after slat extension and resume operation after slat retraction.
3-The pumps are automatically shut off 5 minutes after the center tank empties.
4-They will also shut off momentarily to make room in the wing tanks for IDG cooling return fuel.

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4
Q

What is the center tank fuel pump logic when in MAN mode?

A

The tanks operate continuously when they are selected ON with electric power avail. No auto shutoff logic.

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5
Q

*What will cause a FUEL MODE SEL FAULT light?

A

-Center tank contains more than 550 lbs and either main tank has less than 11,000 lbs.

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6
Q

*When do the main tank outer cells drain into the inner tanks?

A

When the inner tank quantity reaches approximately1650 lbs.

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7
Q

*If only one inner tank reaches that low level (approx. 1650), what happens to the other transfer valve?

A

All 4 transfer valves open.

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8
Q

*Once opened to transfer fuel, how are the Fuel Transfer Valves closed?

A

Automatically at the next refueling operation.

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9
Q

*What does an amber FAULT light in the FUEL PUMP pb indicate?

A

Low fuel delivery pressure

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10
Q

If the wing tank pumps fail, is gravity feeding possible?

A

Yes.

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11
Q

Can the center tank gravity feed?

A

No.

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12
Q

*Can fuel be transferred from one tank to anther?

A

Only on the ground. FCOM procedure.

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13
Q

*When does the APU fuel pump run?

A

When the wing or center tank pumps are off or when the aircraft is on battery power only.

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14
Q

*What does an amber boxed ECAM FOB indicate?

A

Some fuel is unusable.

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15
Q

*How is the IDG cooled?

A

By fuel from the HP fuel pump drawn in from the fuel manifold and then returned to its respective outer fuel tank. When full the outer tank will spill over to the inner tank.

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16
Q

*If the IDG return fuel fills the wing tanks, what occurs?

A

The center tank pumps turn off until the wing tank quantity reduces by 1100 lbs.

17
Q

*Why are the outer wing tanks drained last?

A

Structural wing bending moment relief.

18
Q

*What does the REFUEL message on the ECAM mean?

A

The refueling control panel door is not closed.

19
Q

*What controls the flow of fuel from the center tank to the inner tanks on aircraft that have jet pumps?

A

The Fuel Level Sensing Control Unit (FLSCU).