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Aircraft Fuel System Questions

Authored by Edomias Tadesse

Engineering

Professional Development

Used 1+ times

Aircraft Fuel System Questions
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15 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In a magnetic float switch, what component's movement brings the armature closer to the magnet to operate the micro-switch?

The counterweight

The float

The striker

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the primary function of the flexible diaphragm within a fuel pressure switch?

To amplify small pressure changes.

To isolate the electrical switch mechanism from the fuel.

To cool the microswitch during operation.

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In an electrically operated Low-Pressure (LP) valve, what component cuts off power to the motor at the fully-open and fully-closed positions?

The electro-magnetic brake

The reversible electric motor

The limit switches

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Under what condition does a suction valve in the fuel system open?

When booster pump pressure is applied to the pipeline.

When suction is applied to the pipeline by the engine-driven pump.

When the cross-feed valve is commanded open.

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the "interference spider" found in some non-return valves?

To filter solid contaminants from the fuel.

To prevent the valve from being installed in the wrong direction.

To create a vortex for better fuel flow.

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Where is an air release valve typically installed in the engine fuel feed line?

At the lowest point to collect water.

At the point closest to the engine fuel pump.

At the highest point to trap air.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

For redundancy, how are the two actuators on a critical electrically driven fuel valve typically powered?

From the same electrical bus.

From different electrical sources.

By a dedicated backup battery.

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