Fuel Flashcards

0
Q

How are the fuel tanks normally vented

A

The tanks are vented to atmosphere by 2 NACA scoops vents

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1
Q

Where is the aircraft fuel stored

A

In the two main wing tanks and one center collector tank

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2
Q

How are fuel system faults annunciated

A

Both a and b are correct: switch lights on the overhead fuel panel & on EICAS in the form of messages

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3
Q

What is used to provide the fuel system computer with fuel quantity information

A

Both a and b: six fuel quantity probes with compensator units in each of the main tanks & three probes in the center tank

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4
Q

How may the fuel level be manually checked on the ground

A

By means of magnetic level indicators

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5
Q

What type of ejector pumps are used to move fuel from main tanks to the collector tanks

A

Scavenge ejectors

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6
Q

What maintains fuel symmetry between the main tanks

A

Automatically controlled by the bi-directional x flow pump

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7
Q

How are the center collector tanks kept full

A

Gravity feed lines and scavenge ejectors

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8
Q

What is used to back up the main ejectors

A

Two electric boost pumps

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9
Q

The electric fuel boost pumps

A

All of the above: are energized during engine start, can feed fuel to either engine from one collector tank, back up the main ejector pumps

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10
Q

From what source is the APU fuel feed supplied

A

From left collector tank via APU fuel pump

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11
Q

Where is bulk fuel temperature taken

A

Right main wing tank

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12
Q

How is pressure refueling and suction refueling accomplished and how is it controlled

A

Accomplished through the single point refuel/defuel adapter. Controlled from the refuel/defuel control panel

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13
Q

If a fuel asymmetry condition exists between main tanks, what visual caution message is presented on EICAS

A

FUEL IMBALANCE

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14
Q

What fuel system information is displayed on the EICAS primary page

A

Individual tank quantities, total fuel quantity, fuel flow per engine

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15
Q

How many magnetic level indicators are there and where are they located

A
  1. There are two under each main wing tank, and one under the center collector tank
16
Q

For automatic pressure refueling, what does the refuel/defuel control panel permit

A

All of the above: pre selection of fuel quantity desired, built in test BITE feature, refuel/ defuel shut off valves to close automatically if the maximum fuel level is reached

17
Q

What is the purpose of the fuel drain valves that are installed at the lowest point of each tank

A

To permit gravity defueling