Fuel indications Flashcards

1
Q

What is the primary purpose of monitoring fuel pressure in an aircraft engine?

A

To give the flight crew an early warning of a fuel system malfunction.

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2
Q

Where is the low-pressure sensor typically positioned in an aircraft fuel system?

A

After the outlet from the low-pressure filter.

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3
Q

What does a differential pressure sensor across the fuel filter indicate?

A

It gives a warning of an impending filter blockage and the risk of cavitation.

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4
Q

What kind of gauge is used in light reciprocating engine aircraft to monitor fuel pressure?

A

A direct reading Bourdon tube pressure gauge.

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5
Q

How do modern aircraft with more complex fuel systems measure fuel pressure?

A

They use a sensor with a transducer that sends electrical signals to a flight deck gauge.

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5
Q

What type of fuel pressure gauge is used in complex and larger reciprocating engine aircraft?

A

A differential fuel pressure gauge, typically a bellows type.

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6
Q

What is the purpose of the low fuel pressure warning light?

A

To alert the flight crew when the fuel pressure falls outside the normal operating range.

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7
Q

Where is the low-pressure warning switch located in most turbine-powered aircraft?

A

At the outlet of each fuel boost pump.

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8
Q

Why is monitoring fuel temperature critical in an aircraft?

A

To inform the flight crew when the temperature causes ice to form in the fuel system and filter.

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9
Q

What type of sensor is commonly used to monitor fuel temperature in large high-performance turbine aircraft?

A

A resistance-type electric fuel temperature sender.

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10
Q

How can low fuel temperature be corrected in some aircraft?

A

By using a fuel heater.

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11
Q

What are the two indications provided by the fuel flow indicating system?

A

The actual fuel flow to the engines and the fuel used since the engine was started.

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12
Q

How is the actual fuel quantity calculated during a flight?

A

By subtracting the amount of used fuel from the amount of fuel in the tanks at take-off.

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13
Q

What is the purpose of the fuel-used indication?

A

To show the mass of fuel burned since the last engine start, allowing comparison of engine performance.

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14
Q

Where is the fuel flow transmitter located in an aircraft engine?

A

Between the fuel control unit and the fuel nozzles.

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15
Q

What is the fundamental law of physics that all fuel flow transmitters are based on?

A

Force = Mass x Acceleration.

16
Q

What are the two common types of fuel flow transmitters used today?

A

Synchronous mass flow and motorless mass flow transmitters.

17
Q

How does a synchronous mass flow transmitter measure fuel flow?

A

The fuel mass turns a turbine against a spring, and the deflection angle is measured.

18
Q

What is the key difference between synchronous mass flow and motorless mass flow transmitters?

A

Motorless mass flow transmitters use the fuel itself to generate acceleration without an electric motor.

19
Q

How does a motorless mass flow transmitter measure the mass fuel flow?

A

By measuring the angle between the rotating drum and the rotating impeller, which is proportional to the mass fuel flow.