E175 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 tank

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3
Q

What types of fuel pumps are in each wing?

A
  • Primary ejector pump
  • ACMP
  • DCMP (right tank)
  • 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
  • backup pump in case primary ejector pump fails
  • engine start
  • xfeed 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(s) is used once an engine is started

A

Associated primary ejector pumps

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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. The only exception is by performing a maintenance function on the ground

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12
Q

What happens when the xfeed switch is selected to LOW1?

A
  • xfeed 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

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