Fuel System Flashcards

1
Q

How is fuel moved from the center tank to the wing tanks

A

Tansfer ejectors

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2
Q

How is fuel moved from the wing tanks to the collecter tanks

A

Scavenge ejectors, and gravity

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3
Q

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

A

Main ejectors

Backed up by DC powered boost pumps

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4
Q

What is the function of the electric boost pumps

A

To supply fuel to the engines when main ejector pressure is low

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5
Q

Will an engine continue to run with a failed engine driven fuel pump

A

No

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6
Q

Max fuel imbalance

A

300 lbs for takeoff

800 lbs in all other phases

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7
Q

How many ways can we crossflow fuel

A

3

Automatically, manually, and gravity

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8
Q

When will the auto crossflow system begin transferring fuel

A

200 lb fuel imbalance

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9
Q

When will the auto crossflow system stop transferring fuel

A

When the fuel quantity of the low tank exceeds the other tank by 50 lbs

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10
Q

When are the boost pumps automatically energized

A

When low pressure is detected at the main ejectors

If the boost pumps are armed

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11
Q

Where is bulk fuel temperature measured

A

Right main tank

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12
Q

What is the minimum bulk fuel temperature for takeoff

A

-30 degrees C

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13
Q

What is the minimum bulk fuel temperature during flight

A

-40 degrees C

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14
Q

How is fuel heated

A

Fuel/heat exchanger

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15
Q

What is the minimum engine fuel temperature for takeoff

A

+5 C

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16
Q

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

A

Each wing tank must be above 4,400 lbs

17
Q

Which bus powers the refuel/defuel panel and SOVs

A

APU battery direct bus

18
Q

Where is the refuel/defuel panel located

A

On the fuselage, forward of right wing

19
Q

Where is the single point adapter located

A

Right wing root

20
Q

What message will be displayed on the EICAS whenever the refuel/defuel panel is switched on

A

AUTO XFLOW INHIB status message