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FS1 > ✧ Stage 2 Knowledge Statements > Flashcards

✧ Stage 2 Knowledge Statements Flashcards

1
Q

When hand propping, a ____ ____ must be at the controls in the cockpit.

A

Competent Pilot

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2
Q

____ ignition provides for ____ performance and safety

A

Dual, increased

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3
Q

Carburetors operate based on the difference in ____ between the ____ and the ____ inlet.

A

Pressure, venturi, air

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4
Q

At higher altitudes, the mixture must be ____ to ____ the fuel flow to compensate for ____ air density.

A

Leaned, decrease, decreased

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5
Q

A descent to a ____ altitude without adjusting the mixture will cause the mixture to become ____.

A

Lower, leaner

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6
Q

Carburetor ice is possible when ____ air temperatures are between ____F and ____F with visible ____ or ____ humidity.

A

Outside, 20, 70, moisture, high

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7
Q

The first indication of carb ice on airplanes with a fixed pitch propeller is a loss of ____ ____.

A

Engine RPM.

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8
Q

Carburetor heat ____ the fuel/air mixture.

A

Enriches.

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9
Q

Applying ____ decreases engine performance.

A

Carburetor Heat.

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10
Q

Applying carburetor heat ____ engine performance.

A

Decreases.

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11
Q

When carburetor heat is applied to eliminate ice, there will be a further ____ in ____ followed by a gradual ____ in ____ as the ice melts.

A

Decrease, RPM, increase, RPM

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12
Q

Carburetor-equipped engines are ____ susceptible to icing than fuel-injected engines.

A

More.

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13
Q

After the engine starts, the ____ should be adjusted for proper RPM and the ____ (especially the oil pressure!) should be ____.

A

Throttle, gauges, checked

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14
Q

If you are running up your engine at a ____-____ airport, you may eliminate engine roughness by ____ the mixture.

A

High-altitude, leaning

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15
Q

Detonation is caused by using a ____ octane fuel or excessive engine ____

A

Lower, temperatures

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16
Q

Detonation occurs when the fuel/air mixture ____ instead of ____ ____

A

Explodes, burning evenly

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17
Q

During climb, lowering the nose will ____ cooling and ____ engine workload.

A

Increase, decrease

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18
Q

_____ is the uncontrolled firing of the fuel/air charge in advance of the normal spark.

A

Pre-ignition

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19
Q

An engine is cooled, in part, by ____ ____ through the system to ____ friction and absorb ____ from internal engine parts.

A

Circulating oil, reduce, heat

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20
Q

Excessively ____ engine temperature either in the air or on the ground will cause loss of power, excessive oil consumption, and excessive wear on internal engine parts.

A

High.

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21
Q

Excessively high engine temperature either in the air or on the ground will cause ________, ________, and ________ on internal engine parts.

A

Loss of power, excessive oil consumption, excessive wear.

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22
Q

If the recommended octane is not available for an airplane, the ______ octane aviation gas should be used. This will prevent the possibility of the engine running _____.

A

Next highest, too hot.

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23
Q

All ____ and ____ should be drained _____ to make sure there is no water in the fuel system.

A

Fuel strainer drains, fuel tank sumps, before each flight

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24
Q

In an airplane with fuel pumps, the _____ fuel pump is used for engine _____ or in the event the _____.

A

Auxiliary, priming, engine-driven pump fails.

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25
Q

Filling the fuel tanks at the end of the day prevents _____ by _____ the _____ in the tanks.

A

Moisture condensation, eliminating, air space.

26
Q

Failure of the _____ system usually results in the failure of the avionics system.

A

Electrical.

27
Q

Failure of the electrical system usually results in the failure of the ______.

A

Avionics system.

28
Q

The _______ is a source of pressure for the altimeter, VSI, and airspeed indicator.

A

Pitot-Static system.

29
Q

The pitot-static system is a source of ______ for the ____, ____, and ____.

A

Pressure, altimeter, VSI, airspeed indicator.

30
Q

The pitot tube provides ____ pressure for the ____ only.

A

Impact (ram air), airspeed indicator

31
Q

If only the pitot tube is clogged, only the _____ will be affected.

A

Airspeed indicator

32
Q

The most important airspeed limitation which is not color-coded is the _______ (known as V_).

A

Maneuvering speed, Va

33
Q

The lower limit of the white arc is the _____ speed with wing flaps and landing gear in the _____ position. (Vs0)

A

Power-off stalling speed, landing

34
Q

The upper limit of the white arc is the ______ (V__)

A

Maximum full-flaps-extended speed (VFE)

35
Q

The lower limit of the green arc is the ______ in a ______ (V__)

A

Power-off stalling speed, specific configuration, VS1

36
Q

The upper limit of the green arc is the ______ (V__)

A

Maximum structural cruising speed (Vno)

37
Q

The yellow arc is known as the _____

A

Caution range.

38
Q

The red radial line is the ______ at which the airplane may be operated ______ (or under any circumstance). It’s also known as V__.

A

Maximum speed, in smooth air, Vne

39
Q

Absolute altitude is the ______

A

Altitude above the surface.

40
Q

True altitude is the ____

A

Actual distance above MSL.

41
Q

Indicated altitude is the same as ____ altitude when standard conditions exist.

A

True.

42
Q

Indicated altitude is the same as true altitude ______.

A

When standard conditions exist.

43
Q

Pressure altitude is the altitude _____

A

Indicated when the Kollsman window is set to 29.92”

44
Q

Pressure altitude is equal to true altitude when ______.

A

Standard atmospheric conditions exist.

45
Q

Density altitude is ______ altitude corrected for ______.

A

Pressure, non-standard temperature.

46
Q

Density altitude is ____ to _____ altitude at _____ temperature.

A

Equal, pressure, standard

47
Q

The altimeter indicates ____ altitude at field elevation with the current local altimeter setting.

A

True.

48
Q

On warm days, the altimeter indicates ____ than actual altitude.

A

Lower.

49
Q

On ____ days, the altimeter indicates lower than actual altitude.

A

Warm.

50
Q

Turn coordinators provide an indication of the movement of the aircraft about the _____ and _____ axes.

A

Yaw, roll

51
Q

The relationship of the miniature airplane to the ____ bar should be used for an indication of ______ and ______.

A

Horizon, pitch, bank attitude

52
Q

During flight, compasses are accurate only _______.

A

During straight-and-level flight at a constant airspeed.

53
Q

Deviation in a magnetic compass is caused by the magnetic fields ______ ______ the lines of magnetic force.

A

Within the aircraft, distorting

54
Q

A magnetic compass will indicate a turn toward the ____ during acceleration when on an east or west heading.

A

North.

55
Q

A magnetic compass will indicate a turn toward the north during _____ when on an _____ heading.

A

Acceleration, east or west.

56
Q

A magnetic compass will indicate a turn toward the _____ during deceleration when on an east or west heading.

A

South.

57
Q

A magnetic compass will indicate a turn toward the south during _____ when on an ________ heading.

A

Deceleration, east or west.

58
Q

Acceleration/deceleration errors (do/don’t) occur when heading north or south.

A

Don’t.

59
Q

A magnetic compass will, at the start of a turn, indicate a turn in the _____ when turning from a heading of north.

A

Opposite direction.

60
Q

A magnetic compass will, at the start of a turn, indicate a turn in the opposite direction when turning from a heading of _____.

A

North.

61
Q

A magnetic compass will _____ or _____ the turn when turning from a heading of south.

A

Lead, precede

FS1 (11 decks)

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