fuel system 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 tank temperature taken?

A

left tan

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3
Q

what type 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

back up pump in case of primary ejector pump failure

engine start

cross feed operations

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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 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 box?

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 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

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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 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

660 lbs of fuel remaining in the associated tank

Fuel low level caution (gauge indications turns yellow only) occurs at 1320 lbs. in associated tank

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15
Q
A
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