ASA Ch 3 Flashcards

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1
Q

Which instrument will become inoperative if the pitot tube becomes clogged?
A: Altimeter
B: Vertical speed
C: Airspeed

A

C: Airspeed

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2
Q

Which instrument(s) will become inoperative if the static vents become clogged?
A: Airspeed only
B: Altimeter only
C: Airspeed, altimeter, and vertical speed

A

C: Airspeed, altimeter, and vertical speed

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3
Q

If the pitot tube and outside static vents become clogged, which instruments would be affected?
A: The altimeter, airspeed indicator, and turn-and-slip indicator
B: The altimeter, airspeed indicator, and vertical speed indicator
C: The altimeter, attitude indicator, and turn-and-slip indicator

A

B: The altimeter, airspeed indicator, and vertical speed indicator

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4
Q

The pitot system provides impact pressure for which instrument?
A: Altimeter
B: Vertical-speed indicator
C: Airspeed indicator

A

C: Airspeed indicator

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5
Q

Which V-speed represents maneuvering speed?
A: VA
B: VLO
C: VNE

A

A: VA

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6
Q

What does the red line on an airspeed indicator represent?
A: Maneuvering speed
B: Turbulent or rough-air speed
C: Never-exceed speed

A

C: Never-exceed speed

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7
Q

Which color identifies the never-exceed speed?
A: Upper limit of the green arc
B: Upper limit of the white arc
C: The red radial line

A

​C: The red radial line

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8
Q

Which color identifies the power-off stalling speed in a specified configuration?
A: Upper limit of the green arc
B: Upper limit of the white arc
C: Lower limit of the green arc

A

​C: Lower limit of the green arc

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9
Q

Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff?
A: VY
B: VA
C: VX

A

C: VX

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10
Q

After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?
A: VY
B: VX
C: VA

A

A: VY

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11
Q

What is the full flap operating range for the airplane?
A: 55 to 100 knots
B: 55 to 208 knots
C: 55 to 165 knots

A

A: 55 to 100 knots

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12
Q

The maximum speed at which the airplane can be operated in smooth air is
A: 100 knots
B: 165 knots
C: 208 knots

A

​C: 208 knots

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13
Q

What is the maximum flaps-extended speed?
A: 65 knots
B: 100 knots
C: 165 knots

A

B: 100 knots

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14
Q

Which color identifies the normal flap operating range?
A: The yellow arc
B: The green arc
C: The white arc

A

​C: The white arc

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15
Q

Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration?
A: Upper limit of the green arc
B: Upper limit of the white arc
C: Lower limit of the white arc

A

​C: Lower limit of the white arc

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16
Q

What is the maximum structural cruising speed?
A: 100 knots
B: 165 knots
C: 208 knots

A

B: 165 knots

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17
Q

What is an important airspeed limitation that is not color coded on airspeed indicators?
A: Never-exceed speed
B: Maximum structural cruising speed
C: Maneuvering speed

A

​C: Maneuvering speed

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18
Q

Which V-speed represents maximum flap extended speed?
A: VFE
B: VLOF
C: VFC

A

A: VFE

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19
Q

Which V-speed represents maximum landing gear extended speed?
A: VLE
B: VLO
C: VFE

A

A: VLE

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20
Q

VNO is defined as the
A: normal operating range
B: never-exceed speed
C: maximum structural cruising speed

A

​C: maximum structural cruising speed

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21
Q

VSO is defined as the
A: stalling speed or minimum steady flight speed in the landing configuration
B: stalling speed or minimum steady flight speed in a specified configuration
C: stalling speed or minimum takeoff safety speed

A

A: stalling speed or minimum steady flight speed in the landing configuration

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22
Q

What is the caution range of the airplane?
A: 0 to 60 knots
B: 100 to 165 knots
C: 165 to 208 knots

A

C: 165 to 208 knots

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23
Q

If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter?
A: The elevation of the nearest airport corrected to mean sea level
B: The elevation of the departure area
C: Pressure altitude corrected for nonstandard temperature

A

B: The elevation of the departure area

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24
Q

Prior to takeoff, the altimeter should be set to which altitude or altimeter setting?
A: The current local altimeter setting, if available, or the departure airport elevation
B: The corrected density altitude of the departure airport
C: The corrected pressure altitude for the departure airport

A

A: The current local altimeter setting, if available, or the departure airport elevation

25
Q

At what altitude shall the altimeter be set to 29.92, when climbing to cruising flight level?
A: 14,500 feet MSL
B: 18,000 feet MSL
C: 24,000 feet MSL

A

B: 18,000 feet MSL

26
Q

Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates
A: calibrated altitude at field elevation
B: absolute altitude at field elevation
C: true altitude at field elevation

A

C: true altitude at field elevation

27
Q

How do variations in temperature affect the altimeter?
A: Pressure levels are raised on warm days and the indicated altitude is lower than true altitude
B: Higher temperatures expand the pressure levels and the indicated altitude is higher than true altitude
C: Lower temperatures lower the pressure levels and the indicated altitude is lower than true altitude

A

A: Pressure levels are raised on warm days and the indicated altitude is lower than true altitude

28
Q

What is true altitude?
A: The vertical distance of the aircraft above sea level
B: The vertical distance of the aircraft above the surface
C: The height above the standard datum plane

A

A: The vertical distance of the aircraft above sea level

29
Q

Under what condition will true altitude be lower than indicated altitude?
A: In colder than standard air temperature
B: In warmer than standard air temperature
C: When density altitude is higher than indicated altitude

A

A: In colder than standard air temperature

30
Q

What is absolute altitude?
A: The altitude read directly from the altimeter
B: The vertical distance of the aircraft above the surface
C: The height above the standard datum plane

A

B: The vertical distance of the aircraft above the surface

31
Q

What is density altitude?
A: The height above the standard datum plane
B: The pressure altitude corrected for nonstandard temperature
C: The altitude read directly from the altimeter

A

B: The pressure altitude corrected for nonstandard temperature

32
Q

What is pressure altitude?
A: The indicated altitude corrected for position and installation error
B: The altitude indicated when the barometric pressure scale is set to 29.92
C: The indicated altitude corrected for nonstandard temperature and pressure

A

B: The altitude indicated when the barometric pressure scale is set to 29.92

33
Q

Under what condition is indicated altitude the same as true altitude?
A: If the altimeter has no mechanical error
B: When at sea level under standard conditions
C: When at 18,000 feet MSL with the altimeter set at 29.92

A

B: When at sea level under standard conditions

34
Q

If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs?
A: 70 foot increase in indicated altitude
B: 70 foot increase in density altitude
C: 700 foot increase in indicated altitude

A

​C: 700 foot increase in indicated altitude

35
Q

Under which condition will pressure altitude be equal to true altitude?
A: When the atmospheric pressure is 29.92” Hg
B: When standard atmospheric conditions exist
C: When indicated altitude is equal to the pressure altitude

A

B: When standard atmospheric conditions exist

36
Q

If a flight is made from an area of low pressure into an area of high pressure without the altimeter setting being adjusted, the altimeter will indicate
A: the actual altitude above sea level
B: higher than the actual altitude above sea level
C: lower than the actual altitude above sea level

A

​C: lower than the actual altitude above sea level

37
Q

If a flight is made from an area of high pressure into an area of lower pressure without the altimeter setting being adjusted, the altimeter will indicate
A: lower than the actual altitude above sea level
B: higher than the actual altitude above sea level
C: the actual altitude above sea level

A

B: higher than the actual altitude above sea level

38
Q

Which condition would cause the altimeter to indicate a lower altitude than true altitude?
A: Air temperature lower than standard
B: Atmospheric pressure lower than standard
C: Air temperature warmer than standard

A

C: Air temperature warmer than standard

39
Q

Altimeter 1 indicates
A: 500 feet
B: 1,500 feet
C: 10,500 feet

A

C: 10,500 feet

40
Q

Altimeter 2 indicates
A: 1,500 feet
B: 4,500 feet
C: 14,500 feet

A

​C: 14,500 feet

41
Q

Altimeter 3 indicates
A: 9,500 feet
B: 10,950 feet
C: 15,940 feet

A

A: 9,500 feet

42
Q

Which altimeter(s) indicate(s) more than 10,000 feet?
A: 1, 2, and 3
B: 1 and 2 only
C: 1 only

A

B: 1 and 2 only

43
Q

Altimeter 3 is indicating a VFR cruising altitude for which direction?
A: 180-359 degrees magnetic
B: 179 degrees true
C: 080 degrees magnetic

A

​C: 080 degrees magnetic

44
Q

If a pilot changes the altimeter setting from 30.11 to 29.96, what is the approximate change in indication?
A: Altimeter will indicate .15” Hg higher
B: Altimeter will indicate 150 feet higher
C: Altimeter will indicate 150 feet lower

A

C: Altimeter will indicate 150 feet lower

45
Q

How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated?
A: By the direction of deflection of the banking scale (A)
B: By the direction of deflection of the horizon bar (B)
C: By the relationship of the miniature airplane (C) to the deflected horizon bar (B)

A

C: By the relationship of the miniature airplane (C) to the deflected horizon bar (B)

46
Q

A turn coordinator provides an indication of the
A: movement of the aircraft about the yaw and roll axis
B: angle of bank up to but not exceeding 30 degrees
C: attitude of the aircraft with reference to the longitudinal axis

A

A: movement of the aircraft about the yaw and roll axis

47
Q

The proper adjustment to make on the attitude indicator during level flight is to align the
A: horizon bar to the level-flight indication
B: horizon bar to the miniature airplane
C: miniature airplane to the horizon bar

A

​C: miniature airplane to the horizon bar

48
Q

To receive accurate indications during flight from a heading indicator, the instrument must be
A: set prior to flight on a known heading
B: calibrated on a compass rose at regular intervals
C: periodically realigned with the magnetic compass as the gyro precesses

A

C: periodically realigned with the magnetic compass as the gyro precesses

49
Q

Deviation in a magnetic compass is cause by the
A: presence of flaws in the permanent magnets of the compass
B: difference in the location between true north and magnetic north
C: magnetic fields within the aircraft distorting the lines of magnetic force

A

C: magnetic fields within the aircraft distorting the lines of magnetic force

50
Q

The angular difference between true north and magnetic north is
A: magnetic deviation
B: magnetic variation
C: compass acceleration error

A

B: magnetic variation

51
Q

Deviation error of the magnetic compass is caused by
A: northerly turning error
B: certain metals and electrical systems within the aircraft
C: the difference in location of true north and magnetic north

A

B: certain metals and electrical systems within the aircraft

52
Q

In the Northern Hemisphere, a magnetic compass will normally indicate a turn towards the north if
A: an aircraft is decelerated while on an east or west heading
B: a left turn is entered from a west heading
C: an aircraft is accelerated while on an east or west heading

A

C: an aircraft is accelerated while on an east or west heading

53
Q

In the Northern Hemisphere, the magnetic compass will normally indicate a turn toward the south when
A: a left turn is entered from an east heading
B: a right turn is entered from a west heading
C: the aircraft is decelerated while on a west heading

A

C: the aircraft is decelerated while on a west heading

54
Q

What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere?
A: The compass will initially indicate a turn to the left
B: The compass will indicate a turn to the right, but at a faster rate than is actually occurring
C: The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the airplane

A

B: The compass will indicate a turn to the right, but at a faster rate than is actually occurring

55
Q

In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate
A: a turn momentarily
B: correctly when on a north or south heading
C: a turn toward the south

A

B: correctly when on a north or south heading

56
Q

In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if
A: a left turn is entered from a north heading
B: a right turn is entered from a north heading
C: an aircraft is accelerated while on a north heading

A

B: a right turn is entered from a north heading

57
Q

In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the east if
A: an aircraft is decelerated while on a south heading
B: an aircraft is accelerated while on a north heading
C: a left turn is entered from a north heading

A

C: a left turn is entered from a north heading

58
Q

During flight, when are the indications of a magnetic compass accurate?
A: Only in straight-and-level unaccelerated flight
B: As long as the airspeed is constant
C: During turns if the bank does not exceed 18 degrees

A

A: Only in straight-and-level unaccelerated flight