FUEL SYSTEMS M11.10 Flashcards

1
Q

What is the flash point of JET A1 fuel?

A

+38°C

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2
Q

What is meant by the term
“Integral tank”?

A

The tank is part of the structure of the wing

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3
Q

What is the purpose of a knit aluminium gasket on a fuel tank access panel?

A

To provide electrical bonding to the access panel

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4
Q

What is the maximum refuel pressure allowed when carrying out a pressure refuel?

A

50psi

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5
Q

What is the purpose of the trim tank?

A

To reduce drag and increase fuel economy

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6
Q

Which parameter is measured by fuel quantity probes used for tank gauges?

A

Capacitance

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7
Q

What does it look like if water is suspended in fuel?

A

The water gives the fuel a milky appearance

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8
Q

Which mode(s) of pressure refuelling can be carried out from the flight deck?

A

Automatic ONLY

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9
Q

Which fuel type is commonly used on commercial aircraft in Europe?

A

JET A1

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10
Q

During an override refuel of a particular tank the over-ride plunger of the solenoid control fuel valve is released…

A

…The valve will close if the solenoid is de-energised

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11
Q

What happens to the fuel that enters the fuel tank venting system and is not immediately drained back into its tank?

A

It goes into the vent surge tanks and then back in to the main tank when conditions allow

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12
Q

How is a fuel leak in an aircraft Centre tank indicated?

A

By a leak monitor connected to a drain valve

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13
Q

A fuel scavenge system uses jet pumps. When are these jet pumps operated?

A

Whenever the main booster pumps are running

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14
Q

A jettison system has anti-corona discharge nozzles where the fuel actually leaves the aircraft. What is the purpose of these nozzles?

A

To ensure that the fuel does not vapourise as it leaves the aircraft so that it drops…

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15
Q

Which fuel has a freezing point of -40°C?

A

JET A

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16
Q

Where are the fuel tank drain valves located?

A

At the lowest point in the tank

17
Q

Which statement is true regarding fuel tank venting systems?

A

The air pressure in fuels is kept slightly above ambient pressure to prevent the fuel from vaporising and to ensure a positive supply to the booster pumps

18
Q

How is fuel prevented from splashing around inside wing during flight manoeuvres?

A

The ribs in the wings have restricted openings that act as baffles
(Small holes in the ribs)