Fuel System Flashcards

1
Q

What are the fuel quantities for Gravity refueling?

A

Total: 14,810 lbs
Mains: 7,405
Center: N/A

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2
Q

How is the fuel moved from the center tank to the main tanks?

A

Transfer injectors

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3
Q

How is the fuel moved from the main tanks to the collector tanks?

A

Scavenge ejectors

Gravity line used as backup

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4
Q

How is the fuel moved from the collector tanks to the engine driven high pressure fuel pump?

A

Main ejectors

backed up by boost pumps

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5
Q

What is the function of the electric boost pumps?

A

To provide initial fuel for engine start and to back-up the main ejectors

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6
Q

What is the flight deck indication of a high pressure fuel pump failure?

A

Engine flameout

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7
Q

What is the maximum fuel imbalance?

A

300 lbs for takeoff

800 lbs for all other phases

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8
Q

When will the fuel system automatically begin transferring fuel?

A

200 lb fuel imbalance

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9
Q

When are the boost pumps automatically energized?

A

Low pressure from the mind ejectors

if the pumps are armed

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10
Q

Where is the high pressure fuel pump located?

A

N2 accessory gearbox

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11
Q

Where is the bulk fuel temperature taken?

A

Right main tank

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12
Q

What is the minimum bulk fuel temp for takeoff?

A

-30C

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13
Q

What is the minimum bulk fuel temp during flight?

A

Above -40C

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14
Q

How is engine fuel heated?

A

Fuel/oil heat exchanger

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15
Q

What is the minimum engine fuel temperature for takeoff?

A

+5C

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16
Q

What is the takeoff limitation if the center tank has >500 lbs of fuel?

A

Each main tank must have >4400 lbs

17
Q

Which bus powers the refuel/defuel panel and refuel/defuel SOVs?

A

APU Battery Direct Bus

18
Q

Where is the refuel/defuel panel located?

A

The fuselage forward of right wing

19
Q

Where is the single point adapter located?

A

Right wing root

20
Q

What are the fuel quantities for pressure refueling?

A

Total: 19,594 lbs
Mains: 7,492 lbs
Center: 4,610 lbs