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part 2 faa

Authored by Juliana747 undefined

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part 2 faa
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20 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the

Fuel strainer drain

Lowest point in the fuel system

Fuel strainer drain and the fuel tank sumps

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If a pilot suspects that the engine (with a fixed pitch propeller) is detonating during climb-out after takeoff, the initial corrective action to take would be to

Lean the mixture

Lower the nose slightly to increase airspeed

Apply carburetor heat

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Excessively high engine temperatures will

Cause damage to heat-conducting hoses and warping of the cylinder cooling fins

Cause loss of power, excessive oil consumption, and possible permanent internal engine damage

Not appreciably affect an aircraft engine

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Excessively high engine temperatures, either in the air or on the ground, will

Increase fuel consumption and may increase power due to the increased heat

Result in damage to heat-conducting hoses and warping of cylinder cooling fans

Cause loss of power, excessive oil consumption, and possible permanent internal engine damage

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with

The mixture set too rich

Higher-than-normal oil pressure

Too much power and with the mixture set too lean

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges?

Using fuel that has a lower-than-specified fuel rating

Using fuel that has a higher-than-specified fuel rating

Operating with higher-than-normal oil pressure

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

For internal cooling, reciprocating aircraft engines are especially dependent on

A properly functioning thermostat

Air flowing over the exhaust manifold

The circulation of lubricating oil

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