FUEL SYSTEM Flashcards

(20 cards)

1
Q

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

A

Transfer ejectors

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2
Q

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

A

Scavenge ejectors and gravity

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3
Q

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

A

Main ejectors (backed up by DC electric boost pumps)

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4
Q

What is the function of the electric boost pumps?

A

To supply fuel to the engine 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 take off
800 lbs for all other phases

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7
Q

How many ways are available to cross flow fuel?

A
  1. Auto, manual, and gravity
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8
Q

When will the auto cross flow system begin transferring fuel?

A

200 lb fuel imbalance

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9
Q

When will the auto cross flow 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

Low pressure 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 temp for takeoff (Jet A)?

A

-30 C

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13
Q

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

A

Above -40 c

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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

+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 refuel/defuel SOVs?

A

APU battery direct bus

18
Q

Where is the refuel/defuel panel located?

A

On the fuselage, forward of the right wing

19
Q

Where is the single point adapter located?

A

Right wing root

20
Q

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

A

AUTO XFLOW INHIBIT status message