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Aircraft Systems: Section 5

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Aircraft Systems: Section 5
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23 questions

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1.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

Detonation occurs because of

lack of cylinder pressure

low temperatures

too much cylinder pressure

2.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

When an engine-driven fuel pump and electric auxiliary pump are _____, either pump could supply fuel to the engine.

connected in series

located above the fuel selector valve

connected in parallel

located below the fuel selector valve

3.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

All certificated aircraft are required to have a means of indicating to the pilot the quantity of fuel in ____

each tank

the tanks that are specifically listed on the fuel selector

the tanks approved for takeoffs and landings

the auxiliary tanks only

the main tank only

4.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

Water is _____ than avgas.

heavier

lighter

more volatile

less dense

5.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

An auxiliary fuel pump could typically be used to purge _____ from the fuel system.

vapor

air

small contaminants of rust and dirt

oil

water

6.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

Which example best describes a direct-reading fuel gauge type of system?

a cork float with a wire sticking through a hole in the fuel tank cap

a sender transmitter resistor mounted outside of the tank, operated by an arm connected to a float

several probes across each tank from top to bottom

7.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

When a fuel is burned that has too little lead, common issues could include fouled spark plugs and valves sticking in their guides.

True

False

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