Fuel System Flashcards

0
Q

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

A

Scavenge ejectors (gravity line as a backup)

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1
Q

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

A

Transfer ejectors

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2
Q

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

A

Main ejectors (fuel boost pumps are backup)

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3
Q

What is the function of the electric fuel boost pumps?

A

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

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4
Q

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

A

Engine flameout

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5
Q

What is the maximum fuel imbalance?

A

300 lbs for takeoff and 800 lbs all other times

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6
Q

When will the fuel system automatically start transferring fuel?

A

200 lb fuel imbalance

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7
Q

When are the boost pumps automatically energized?

A

Low pressure from the main ejectors (only if the pumps are armed)

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8
Q

Where is the high pressure fuel pump located?

A

N2 accessory gearbox

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9
Q

Where is the bulk fuel temperature taken?

A

Right main tank

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10
Q

What is the minimum bulk fuel temp for takeoff? During flight?

A
  • 30 Celsius / above - 40 Celsius
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11
Q

How is the engine fuel heated?

A

Fuel/oil heat exchanger

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12
Q

What is the minimum engine fuel temp for takeoff?

A

+5 Celsius

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13
Q

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

A

Each main tank must have > 4400 lbs

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14
Q

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

A

APU battery direct bus

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15
Q

Where is the refuel/defuel panel located

A

Fuselage forward of the right wing

16
Q

Where is the single point fuel adapter located?

A

Right wing root