Fuel System Flashcards

0
Q

What are the fuel quantities for gravity refueling?

A

700: Total - 14,580 lbs, Mains - 7,290 lbs
900: Total - 14,810 lbs, Mains - 7,405 lbs

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1
Q

What are the duel quantities for pressure refueling?

A

700/900/900EP - Total 19,594 lbs, Mains 7,492 lbs, Center 4,610 lbs

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2
Q

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

A

Transfer ejectors

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3
Q

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

A

Scavenge ejectors (gravity line used as a 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 lbs fuel imbalance

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9
Q

When are the boost pumps automatically energized?

A

Low pressure from the main 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 bulk fuel temperature taken?

A

Right main tank

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12
Q

What is the minimum bulk fuel temperature for takeoff (Jet A)?

A

-30 degrees C

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13
Q

What is the minimum bulk fuel temperature during flight (Jet A)?

A

-40 degrees C

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14
Q

How is the engine fuel heated?

A

Fuel/oil heat exchanger

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15
Q

What is the minimum engine fuel temperature for takeoff?

A

+5 degrees C

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 fuel/defuel panel and fuel/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