Fuel Flashcards

1
Q

How does fuel reach the collector tanks in each wing?

A

Gravity flow through flapper valves and when the engines are running through a scavenge ejector

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2
Q

How many water drain valves are there in each wing?

A

Three (Six total)

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3
Q

Where are the water drain valves located?

A
  • Collector tank
  • Wing tank
  • Surge tank
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4
Q

What is the purpose of the NACA scoop?

A

Provides static ventilation of the tanks. Relieves air pressure differential caused by refueling, thermal expansion, or variation of altitude during flight.

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5
Q

What is the purpose of the surge bay?

A

Provide additional expansion volume to prevent fuel spillage.

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6
Q

How much fuel does the surge bay hold?

A

8 gallons or 53.6 pounds of fuel

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7
Q

The engines are provided fuel from which tank?

A

Collector tank

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8
Q

Fuel for the APU is provided from which tank?

A

Right collector tank

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9
Q

What feeds the APU line fuel?

A

Right standby pump or the right ejector

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10
Q

Where are the ejectors located?

A

Bottom of the collector tanks

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11
Q

What provides the motive flow for the ejectors to operate?

A

High pressure output of the engine driven fuel pumps

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12
Q

Where are the scavenge pumps located?

A

Lowest inboard point of each wing tank

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13
Q

What is necessary for the scavenge pumps to operate?

A

Motive flow output of fuel from the engine driven high pressure fuel pumps

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14
Q

Where is the engine fuel shutoff valve?

A

Forward of the engine rotor burst area

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15
Q

Where is the fuel heater/oil cooler located?

A

Engine accessory gearbox

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16
Q

The purpose of the standby fuel pumps are … (4)

A
  • Provide pressure during engine start
  • Provide fuel pressure in the event of an ejector failure
    provided the standby pump switch is in L/R AUTO
  • Provide fuel to the APU line
  • Crossfeeding of fuel
17
Q

Should pressure return to the ejector output after failing to deliver sufficient pressure, the standby boost pump will remain on for …

A

An additional 10 seconds

18
Q

How many fuel quantity probes are located in each wing tank?

A

Nine

19
Q

What controls each side of the fuel system?

A

One channel of a dual-channel computer. If one side channel fails, the other channel automatically assumes control

20
Q

What provides aircraft attitude to each channel of the fuel computer?

A

AHRS (IRS)

21
Q

What determines fuel quantity in the tanks? (4)

A
  • Fuel density
  • Fuel probe readings
  • Aircraft attitude and acceleration
  • WOW signal
22
Q

The fuel temperature probe is located …

A

Right wing tank

23
Q

What provides a cutoff signal to the refuel valve when the tank is full?

A

Fuel level sensor at the top of each wing tank

24
Q

What is displayed on the Fuel Synoptic Page if an input value is invalid?

A

Magenta dashes

25
Q

A green fuel temperature is indicated above the right wing quantity at what temperature?

A

Above - 38C

26
Q

A WING FUEL TEMP LOW caution comes on …

A

Below - 38C