Fuel System Flashcards

1
Q

What is the source of motive flow for the transfer ejectors?

A

The high pressure output of the main ejectors

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2
Q

What is the source of motive flow for the main and scavenge ejectors?

A

The high pressure engine driven fuel pump

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3
Q

What will supply fuel pressure to the engines if the main ejector pressure is low?

A

DC electric boost pumps

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4
Q

What is the function of the scavenge ejectors?

A

Operate by motive flow and transfer fuel from the wing tanks to the collector tanks

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5
Q

What is the function of the collector tanks?

A

Keeps a full supply of fuel available tot eh engines at all aircraft attitudes

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6
Q

What is the location of the collector tanks?

A

Forward section of the center tank

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7
Q

How does the fuel move through the system to the engines?

A

Center tanks to the wing tanks to the collector tanks to the engines

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8
Q

What is the function of the transfer ejectors?

A

Transfers fuel from the center tank to the wing tanks

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9
Q

When does the fuel automatically transfer from the center tanks to the wing tanks?

A

The system starts transfer when the wing tank capacity drops to 94%

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10
Q

When is the fuel transfer from the center tank to the wing tanks completed?

A

When the wing tank is full, or the center tank is empty

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11
Q

What is the function of the fuel crossflow pump?

A

A bi-directional pump that is used to transfer fuel between the wing tanks

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12
Q

What is the function of the automatic power crossflow system?

A

Provides automatic transfer between tanks to compensate for an imbalance of more than 200lbs. The process ends when the previously low tank exceeds the high tank by 50lbs.

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13
Q

What is the function of the XFLOW AUTO OVERRIDE switchlight?

A

Inhibits the automatic fuel crossflow system

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14
Q

What is the function of the gravity crossflow system?

A

Opens a valve connected between both wing tanks to allow gravity to equalize tank quantities

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15
Q

When will the boost pump automatically activate if the switchlights are in the armed position?

A

Should a main ejector pressure fall below 10psi, then both fuel pumps are activated

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16
Q

Which tank normally supplies the APU with fuel?

A

The left collector tank

17
Q

What is the location of the fuel/defuel panel?

A

On the right side of the fuselage forward of the right wing

18
Q

What is the maximum refueling pressure?

A

50psi

19
Q

What is the maximum defueling pressure?

A

4psi

20
Q

What is the function of the Magnetic Fuel Level Indicators?

A

Provides a manual/secondary way of measuring the fuel in each tank

21
Q

What is the location of the MLI’s?

A

The wing MLI’s (4) are located on the underside of the wings and the center tank indicator is located on the underside of the wing box

22
Q

How many MLI’s are there total?

A
  1. 2 for each wing, and 1 for the center tank