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#3248. Which instrument will become inoperative if the pitot tube becomes

clogged?

A- Altimeter.

B- Vertical speed.

C- Airspeed.

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#3273. What is the maximum

structural

cruising speed?

A- 100 MPH.

B- 165 MPH.

C- 208 MPH.

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#5157. While maintaining a constant angle of bank and altitude in a

coordinated turn, an increase in airspeed will

A- decrease the rate of turn resulting in a decreased load factor.

B- decrease the rate of turn resulting in no change in load factor.

C- increase the rate of turn resulting in no change in load factor.

Comm.

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#5604. Why should flight speeds above ‘Vne’ be

avoided?A- Excessive induced drag will result in structural failure.

B- Design limit load factors may be exceeded, if gusts are encountered.

C- Control effectiveness is so impaired that the aircraft becomes uncontrollable.

Comm.

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#3012. After takeoff, which airspeed would permit the pilot to gain the most altitude in a given period of

time?

A- Vy.

B- Vx.

C- Va.

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#3267. The maximum speed

at which the airplane can be

operated in smooth air is

A- 100 MPH.

B- 165 MPH.

C- 208 MPH.

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#3256. 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.

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#3252. Altimeter 3 indicates

A- 9,500 feet.

B- 10,950 feet.

C- 15, 940 feet.

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#5210. If airspeed is increased during a level turn, what action would

be necessary to maintain altitude?A- The angle of attack and angle of bank

must be decreased.B- The angle of attack must be increased

or angle of bank decreased.C- The angle of attack must be

decreased or angle of bank increased.

Comm.

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#3990. If a flight is made from an area of low pressure into an area of high pressure

without the altimeter setting being adjusted and a constant indicated altitude is maintained, the altimeter would 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.

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#3255. 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- High 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.

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#3279. Deviation in a magnetic compass is

caused by

A- presence of flaws in the permanent magnets of the compass.

B- the difference in the location between true north and magnetic north.

C- magnetic fields within the aircraft distorting the lines of magnetic force.

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#3280. In the Northern Hemisphere, a magnetic compass will normally indicate 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.

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#3283. 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.

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#3278. How should a pilot determine the

direction of bank from an attitude indicator

such as the one illustrated?

A- The direction of deflection of the banking scale (A).

B- The direction of deflection of the horizon bar (B).

C- The relationship of the miniature airplane (C) to the deflected horizon bar (B).

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#5268. What is an operational difference between the turn

coordinator and the turn-and-slip indicator?

A- The turn coordinator is always electric; the turn-and-slip indicator is always vacuum-driven.

B- The turn coordinator indicates bank angle only; the turn-and-slip indicator indicates rate of turn and coordination.

C- The turn coordinator indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination.

Comm.

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