Fuel system Flashcards

1
Q

If a GPU cart is not available for starting the APU what fuel pump is used?

A

DC pump

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2
Q

When Ground power is powering the aircraft and you start the APU which pump is providing fuel for APU start?

A

AC Pump

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3
Q

How many fuel tanks does the Aircraft have?

A

2 Integral tanks

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4
Q

What is the purpose of the collector tank?

A

To keep the pumps submerged in fuel. you dont want them cavitating and not delivering proper fuel.

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5
Q

Explain how each fuel tank is set up?

A

collector tank on the inboards, and a surge tank on the outboards.

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6
Q

Where would fuel indications be displayed?

A

on the EICAS and Fuel synoptic page on MFD

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7
Q

With the engines running, which pumps are supplying fuel to the engine?

A

Primary Ejector pump

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8
Q

How is the Primary Ejector pump powered?

A

By motive flow from engine driven pump

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9
Q

What is the purpose of the AC fuel pumps?

A

Backup if the primary ejector pump or engine driven pump fails.engine starting and crossfeed - APU fuel when no engines running

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10
Q

If fuel is low on one tank can it be transfered to the other?

A

no.

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11
Q

Where is DC pump located?

A

Right Tank

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12
Q

why do we have a DC pump?

A

provides pressurized fuel for APU start

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13
Q

What is the purpose of scavange pumps

A

to keep fuel in the collector tank.

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14
Q

what fuel pump Logic for fuel pumps:

A

Primary ejector pump, AC fuel pump and DC pump.

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15
Q

how would you correct a fuel imbalance?

A

turn the crossfeed switch to the Low side for the respective low tank.

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16
Q

how does crossfeed work?

A

It turns on opposite tank pump and opens the crossfeed valve

17
Q

Will setting the AC pump (1)(2) to anything other than auto override the fuel crossfeed commands?

A

yes

18
Q

With either engine running, which pump is supplying APU with pressurized fuel?

A

Primary Ejector pumps.

19
Q

How can aircraft be fueled?

A

Overwing or pressure fuel

20
Q

what is the company Limit for max fuel imbalance?

A

790

21
Q

when would the EICAS Display FUEL IMBALANCE?

A

800 LBS

22
Q

When would FUEL IMBALANCE Message go away?

A

when fuel imbalance less than 100 lbs

23
Q

Where is Fueling Door located?

A

under right wing

24
Q

When would the AC pump come on Automatically if in the AUTO setting?

A

Crossfeed operations, engine starting or APU starting with AC source or primary Ejector failure

25
Q

What are alternate means of checking fuel on the ground?

A

Magnetic fuel indicators

26
Q

the Fuel crossfeed must be Off for takeoff and landing? T/F

A

True

27
Q

Can you refuel the aircraft if power is OFF?

A

yes, Fuel panel is on Hot Battery Bus 2

28
Q

Where is fuel Temperature taken from?

A

Left tank

29
Q

What fuel pumps are in each wing?

A

1 primary ejector pumps, 1 AC fuel pump, 1 DC fuel pump (right wing) and 3 scavange pumps each wing

30
Q

What is a primary ejector pump?

A

Venturi type pump which uses the motive flow of engine driven pump