Fuel Flashcards

1
Q

How many fuel tanks does the airplane have?

A

2 integral tanks

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2
Q

Where is the fuel temperature taken?

A

Left tank (fuel synoptic page to read)

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3
Q

What types of fuel pumps are in each wing?

A

Primary Ejector Pump
ACMP
DCMP (Right tank only)
3 scavenge ejector pumps

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4
Q

What is the Primary Ejector Pump?

A

Venturi pump with no moving parts and no electrical power used by the respective engine.

Powered by motive flow.

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5
Q

What is the purpose of the ACMP?

A
  • Engine start
  • Crossfeed operations (Low1 or Low2)
  • Back-up pump in case of primary ejector pump failure
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6
Q

What is the purpose of the DCMP?

A

Used for APU or engine start if AC Power or the ACMP is not available

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7
Q

What is the purpose of the scavenge pumps?

A

Maintains fuel level in the collector box

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8
Q

What pump(s) is used once an engine is started?

A

Primary (main) ejector pump

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9
Q

What is the purpose of the collector bay/tank?

A

Keeps the fuel pumps submerged.

Ensures constant fuel flow to the respective engine.

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10
Q

What is the surge/vent tank?

A

Collects fuel during wing-down maneuvers and returns it to the main tanks once the wings are level.

Equalizes tank pressure with the atmosphere in flight and during refueling.

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11
Q

Can fuel be transferred from tank-to-tank or be dumped overboard?

A

No transferring or dumping.

However, you can open a crossfeed valve and supply fuel from both tanks to one engine.

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12
Q

What happens when the crossfeed switch is selected to LOW 1?

A

Crossfeed valve is opened.

Commands the ACMP 2 to β€˜ON’ to provide fuel from the right tank to both engines.

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13
Q

What is the only way to close the engine fuel SOV?

A

Pull the associated engine fire extinguishing handle.

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14
Q

When will the FUEL 1(2) LO LEVEL EICAS be presented?

A

660lbs of fuel remaining in the associated collector tank.

Fuel Low Level caution (gauge indications turn yellow only) occurs at 1320 lbs. in associated tank.

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