Slow Flight and Stalls - FAA PPL(A) - Private Pilot Airplane

Question 1

Changes in the center of pressure of a wing affect the aircraft's

Accepted Answer

aerodynamic balance and controllability

Answer

lift/drag ratio

Answer

lifting capacity

Question 2

The use of flaps in slow flight:

Accepted Answer

May be used

Answer

Can only be deployed ten degrees

Answer

Are never allowed to be used in slow flight

Question 3

As the airplane slows down in flight, the angle of attack must be:

Accepted Answer

Increased to maintain altitude

Answer

Remain the same

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Decreased to maintain altitude

Question 4

During a spin to the left, which wing(s) is/are stalled?

Accepted Answer

Both wings are stalled

Answer

Only the left wing is stalled

Answer

Neither wing is stalled

Question 5

During an approach to a stall, an increased load factor will cause the airplane to

Accepted Answer

stall at a higher airspeed

Answer

have a tendency to spin

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be more difficult to control

Question 6

How is the stalling speed or minimum steady flight speed in the landing configuration symbolized?

Accepted Answer

VS0

Answer

VN0

Answer

Red radial line

Question 7

The angle between the chord line of an airfoil and the relative wind is known as the angle of

Accepted Answer

attack

Answer

incidence

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lift

Question 8

In what flight condition must an aircraft be placed in order to spin?

Accepted Answer

Stalled

Answer

Partially stalled with one wing low

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In a steep diving spiral

Question 9

As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will

Accepted Answer

remain the same regardless of altitude

Answer

decrease as the true airspeed increases

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decrease as the true airspeed decreases

Question 10

(Refer to figure 1.) The acute angle A is the angle of

Accepted Answer

attack

Answer

dihedral

Answer

incidence

Exam questions Slow Flight and Stalls - FAA PPL(A) - Private Pilot Airplane