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Unit 2 Aviation Review

Total questions: 55

Worksheet time: 42mins

Name
Class
Date
1.

In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward 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

2.

Deviation in a magnetic compass is caused by

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

3.

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

4.

Deviation error of the magnetic compass is caused by

a)

a northerly turning error

b)

certain metals and electrical systems within the aircraft

c)

the difference in location of true north and magnetic north

5.

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

6.

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

7.

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

8.

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

9.

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

10.

The pitot system provides impact pressure for which instrument?

a)

Altimeter

b)

Vertical-speed indicator

c)

Airspeed indicator

11.

Which instrument will become inoperative if the pitot tube becomes clogged?

a)

Altimeter

b)

Vertical speed indicator

c)

Airspeed indicator

12.

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

13.

Which instrument(s) will become inoperative if the static vents become clogged?

a)

Airspeed indicator only

b)

Altimeter only

c)

Airspeed indicator, altimeter, and vertical speed indicator

14.

What is an important airspeed limitation that is not color coded on airspeed indicators?

a)

Never-exceeded speed

b)

Maximum structural cruising speed

c)

Maneuvering speed

15.

What does the red line on an airspeed indicator represent?

a)

Maneuvering speed

b)

Turbulent or rough-air speed

c)

Never-exceed speed

16.

(Refer to pic) What is the caution range of the airplane?

a)

0 to 60 kts

b)

100 to 165 kts

c)

165 to 208 kts

17.

(Refer to pic) The maximum speed at which the airplane can be operated in smooth air is

a)

100 kts

b)

165 kts

c)

208 kts

18.

(Refer to pic) What is the full flap operating range for the airplane?

a)

55 to 100 kts

b)

55 to 208 kts

c)

55 to 165 kts

19.

(Refer to pic) What is the maximum flaps-extended speed?

a)

65 kts

b)

100 kts

c)

165 kts

20.

(Refer to pic) Which marking identifies the never-exceeded speed?

a)

Upper limit of green arc

b)

Upper limit of the white arc

c)

The red radial line

21.

(Refer to pic) 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 green arc

22.

(Refer to pic) Which color identifies the normal flap operating range?

a)

The yellow arc

b)

The green arc

c)

The white arc

23.

(Refer to pic) What is the maximum structural cruising speed?

a)

100 kts

b)

165 kts

c)

208 kts

24.

(Refer to pic) 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 white arc

c)

Lower limit of white arc

25.

(Refer to pic) Altimeter 1 indicates

a)

500 feet

b)

1,500 feet

c)

10,500

26.

Altimeter 3 indicates

a)

9,500 feet

b)

10,950

c)

15,940

27.

(Refer to pic) Which altimeter(s) indicate(s) more than 10,000 feet?

a)

1, 2, and 3

b)

1 and 2 only

c)

1 only

28.

(Refer to pic) Altimeter 2 indicates

a)

1,500 feet

b)

4,500

c)

14,500 feet

29.

(Refer to pic) Altimeter 3 indicates

a)

9,500 feet

b)

10,500 feet

c)

4,500 feet

30.

(Refer to pic) Altimeter 1 indicates

a)

4,500 feet

b)

1,500 feet

c)

500 feet

31.

(Refer to pic) Which altimeter(s) indicate(s) more than 9,000 feet

a)

1, 2, and 3

b)

1 and 2 only

c)

3 only

32.

(Refer to pic) Altimeter 2 indicates

a)

500 feet

b)

1,500

c)

4,500

33.

What is absolute altitude?

a)

The altitude read directly

b)

The vertical distance of the aircraft above the surface

c)

The height above the standard datum plane

34.

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

35.

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

36.

What is pressure altitude?

a)

The indicated altitude corrected for position and installation error

b)

The altitude indicates when the barometric pressure scale is set to 29.92

c)

The indicated altitude corrected for nonstandard temperature and pressure

37.

Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates

a)

calibrated attitude at field elevation

b)

absolute altitude at field elevation

c)

true altitude at field elevation

38.

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 altimeter set 29.92

39.

Under what condition is pressure altitude and density altitude the same value?

a)

At sea level, when the temperature is 0 degrees F

b)

When the altimeter has no installation error

c)

At standard temperature

40.

Under what condition will pressure altitude be equal to true altitude?

a)

When the atmospheric pressure is 29.92 Hg

b)

When the standard atmospheric conditions exist

c)

When indicated altitude is equal to the pressure altitude

41.

If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs?

a)

70-foot increase is indicated altitude

b)

70-foot increase in density altitude

c)

700-foot increase in indicated altitude

42.

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

43.

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 actual altitude above sea level

c)

lower than the actual altitude above sea level

44.

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 actual altitude above sea level

b)

higher than actual altitude sea level

c)

the actual altitude above sea level

45.

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

46.

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

47.

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

48.

(Refer to pic) A turn coordinator provides an indication of the

a)

movement of the aircraft about the yaw and roll axes

b)

angle of bank up to but not exceeding 30 degrees

c)

attitude of the aircraft with reference to the longitudinal axis

49.

(Refer to pic) 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

50.

(Refer to pic) 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

51.

(Refer to pic) 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

b)

By the direction of deflection of the horizon bar

c)

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

52.

What is a benefit of flying with a glass flight deck?

a)

There is no longer a need to carry paper charts in an airplane

b)

Situational awareness is increased

c)

Terrain avoidance guaranteed

53.

What steps must be taken in glass flight decks to ensure safe flight?

a)

Use the moving map for primary means of navigation, use the MFD to check engine systems and weather, back up with supplementary forms of info

b)

Regularly scan each item on the PFD, confirm on the MFD

c)

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

54.

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

a)

compensate for an airman’s lack of skill or knowledge

b)

offer new capabilities and simplify the basic flying task

c)

improve flight awareness by allowing the pilot to simply watch for alerts

55.

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

a)

ADS-B in capability

b)

Airspeed indicator

c)

Altitude indicator