Subject S - Turbine Powered Auxiliary Power Units Flashcards

1
Q

What is the typical relationship between an aircraft auxiliary power unit (APU) generator and the engine driven generator?

A

They are identical

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2
Q

Where does the APU fuel supply normally come from?

A

The airplanes main fuel supply.

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3
Q

How is the APU rotated during startup?

A

With an electric starter

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4
Q

What is the function of an APU air inlet Plenum?

A

It is to stabilize the pressure of air before it enter the compressor.

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5
Q

When operating at high loads what is the speed of an APU?

A

The APU remains at or near rated speed regardless of load condition.

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6
Q

What is the effect of the pneumatic power when being used in conjunction with maximum APU shaft power output?

A

The pneumatic loading will be automatically regulated

to maintain a safe exhaust gas temperature.

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7
Q

Before shut down how would APU cooling be accomplished?

A

By closing the bleed air valve, thus removing the load.

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8
Q

When is most of the load placed on an APU?

A

When the bleed air is opened.

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9
Q

What regulates fuel scheduling during APU start and under varying pneumatic bleed and electrical loads?

A

Fuel scheduling is maintained by automatically by the APU fuel control system.

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10
Q

How is most troubleshooting accomplished on modern APU’s?

A

by gather information from the FADEC.

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11
Q

What is the primary function of the load compressor on APUs equipped with a free turbine and load compressor?

A

To provide bleed air for aircraft pneumatic systems.

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12
Q

To Prevent rotor seizure “shock cooling”, how long should an APU idle before shut down

A

3 to 5 minutes

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