Ch 2 - Airplane, Instruments, Engines & Systems - Questions 101 - 146 Flashcards

1
Q

What steps must be taken when flying with glass cockpits to ensure safe flight?

A

Regularly scan both inside and outside, use all appropriate checklists and cross-check with other forms of information.

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2
Q

An aircraft which is equipped with an Electronic Flight Display (EFD) can

A

Offer new capabilities and simply the basic flying task.

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3
Q

You are flying an aircraft equipped with an electronic flight display and the air data computer fails. What instrument is affected?

A

Airspeed Indicator.

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4
Q

An abnormally high engine oil temperature indication may be caused by

A

The oil level being too low.

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5
Q

Excessively high engine temperature will

A

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

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6
Q

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

A

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

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7
Q

For internal cooling, air cooled engines are especially dependent on

A

The circulation of lubricating oil.

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8
Q

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

A

Too much power and with the mixture set too lean.

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9
Q

What action can a pilot take to aid in cooling an engine that is overheating during a climb?

A

Reduce rate of clim and increase airspeed.

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10
Q

What is one procedure to aid in cooling an engine that is overheating?

A

Enrich the fuel mixture.

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11
Q

How is engine operation controlled on an engine equipped with an constant-speed propeller?

A

The throttle controls power output as registered on the manifold pressure gauge and the propeller control resulted engine RPM.

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12
Q

A precaution for the operation of an engine equipped with a constant-speed propeller is to

A

Avoid high manifold pressure settings with low RPM.

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13
Q

What is an advantage of a constant-speed propeller?

A

Pemits the pilot to select the blade angle for the most efficient performance.

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14
Q

One purpose of the dual ignition system on an aircraft engine is to provide for

A

Improved engine performance.

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15
Q

If the ignition switch ground wire becomes disconnected, the magneto

A

May continue to fire.

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16
Q

The reason a 4-cylinder reciprocating engine continues to run after the ignition switch is positioned to OFF maybe be a

A

Broken magneto ground wire.

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17
Q

With regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be

A

More susceptible to icing.

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18
Q

Which condition is most favourable to the development of carburetor icing?

A

Temperature between 20F and 70F and high humidity.

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19
Q

The possibility of carburetor icing exists even when the ambient air temperature is as

A

High as 70F and the relative humid is high.

20
Q

If an aircraft is equipped with a fixed-pitch propeller and a float-typer carburetor, the first indication of carburetor ice would most likely be

A

Decrease RPM

21
Q

In an aircraft is equipped with a fixed-propeller and float-type carburetor, the first indication of carburetor ice would most lily be

A

Loss of RPM.

22
Q

The operating principle of float0type carburetors is based on the

A

Difference in air pressure as the Venturi thereat and the air vent.

23
Q

The presence of carburetor ice is an aircraft equipped with a fixed-pitch propeller can be verified by applying carburetor heat and nothing

A

A decrease in RPM and then a gradual increase in RPM.

24
Q

Generally speaking, the use of carburetor heat tends to

A

Decrease engine performance.

25
Q

Applying carburetor heat will

A

Enrich the fuel/ air mixture.

26
Q

What changes occurs in the fuel/air mixture when carburetor heat is applied?

A

The fuel/air mixture becomes richer.

27
Q

During the run-up at high-elevation airport, a pilot notes a slight engine roughness that is not affected by the magneto check but grows worse during the carburetor heat check. Under these circumstances, what would be the most logical initial action?

A

Check the results contained with cleaner setting of the mixture.

28
Q

The basic purpose of adjusting the fuel/air mixture at altitude is to

A

Decrease the fuel flow in order to compensate decreased air density.

29
Q

While cruising at 9,500 feet MSL, the fuel/air mixture is properly adjusted. What will occur if a descent to 4,500 feet MSL is made without readjusting the mixture?

A

The fuel/air mixture may become excessively lean.

30
Q

Fuel/air ratio is the ratio between the

A

Weight of fuel and weight of air entering the cylinder.

31
Q

Detonation occurs in a reciprocating aircraft engine when

A

The unburned charge in the cylinders explodes instead of burning normally.

32
Q

Detonation may occur at high-power settings when

A

The fuel mixture ignites instantaneously instead of burning progressively and evenly.

33
Q

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

A

Lower the nose slightly to increase airspeed.

34
Q

If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will mist likely cause

A

Detonation.

35
Q

The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as

A

Pre-ignition.

36
Q

What type fuel can be substituted for an aircraft if the recommended octane is not available?

A

The next higher octane aviation gas.

37
Q

Filing the fuel tanks after the last flight of the day is considered a good operating procured because this will

A

Moisture condensation by eliminating airspace in the tanks.

38
Q

On aircraft equipped with fuel pumps, when is the auxiliary electric driven pump used?

A

In the event engine -driven fuel pump fails

39
Q

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

A

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

40
Q

What should be the first action after stating an aircraft engine?

A

Adjust for proper RPM and check fro desired indications on the engine gauges.

41
Q

During pre-flight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by

A

Ice from crankcase vapours that have condensed and subsequently frozen.

42
Q

An electrical system failure (battery and alternator) occurs during fight. In this situation, you would

A

Experience avionics equipment failure.

43
Q

A positive indication on an ammeter

A

Shows the rate of charge on the battery.

44
Q

To keep a battery charged, the alternator voltage output should be

A

Higher than the battery voltage.

45
Q

Which of the following is a true statement concerning electrical systems?

A

Lights and radios use the electrical system for power.