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PRIVATE PILOT TEST GUIDE (CHAPTER 3) QUESTIONS, Exams of Aviation

PRIVATE PILOT TEST GUIDE (CHAPTER 3) QUESTIONS WITH EXPLANATIONS OF ANSWERS.

Typology: Exams

2024/2025

Available from 07/16/2025

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PRIVATE PILOT TEST GUIDE (CHAPTER 3) QUESTIONS
WITH EXPLANATIONS OF ANSWERS.
“In what flight condition are torque effects more pronounced in a single-engine airplane? -
CORRECT ANSWER Low airspeed, high power, high angle of attack."
"The term "angle of attack" is defined as the angle between the - CORRECT ANSWER Chord
line of the wing and the relative wind."
"(Refer to Figure 2.) If an airplane weighs 3,300 pounds, what approximate weight would the
airplane structure be required to support during a 30 degree banked turn while maintaining
altitude? - CORRECT ANSWER 3,800 pounds"
"Loading an airplane to the most aft CG will cause the airplane to be - CORRECT ANSWER
Less stable at ALL speeds."
"Ground effect is most likely to result in which problem? - CORRECT ANSWER Becoming
airborne before reaching recommended takeoff speed."
"Which statement relates to Bernoulli's principle? - CORRECT ANSWER Air traveling faster
over the curved upper surface of an airfoil causes lower pressure on the top surface."
"Changes in the center of pressure of a wing affect the aircraft's - CORRECT ANSWER
Aerodynamic balance and controllability."
"An airplane said to be inherently stable - CORRECT ANSWER Requires less effort to
control."
"The four forces acting on an airplane in flight - CORRECT ANSWER Lift, Weight, Thrust,
Drag."
"The left turning tendency of an airplane caused by P-factor is the result of the - CORRECT
ANSWER Propeller blade descending on the right, producing more thrust than the ascending
blade on the left."
"What determines the longitudinal stability of an airplane? - CORRECT ANSWER The
location of the Center of Gravity (CG) with respect to the center of lift."
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PRIVATE PILOT TEST GUIDE (CHAPTER 3) QUESTIONS

WITH EXPLANATIONS OF ANSWERS.

“In what flight condition are torque effects more pronounced in a single-engine airplane? -

CORRECT ANSWER Low airspeed, high power, high angle of attack."

"The term "angle of attack" is defined as the angle between the - CORRECT ANSWER Chord

line of the wing and the relative wind." "(Refer to Figure 2.) If an airplane weighs 3,300 pounds, what approximate weight would the airplane structure be required to support during a 30 degree banked turn while maintaining

altitude? - CORRECT ANSWER 3,800 pounds"

"Loading an airplane to the most aft CG will cause the airplane to be - CORRECT ANSWER

Less stable at ALL speeds."

"Ground effect is most likely to result in which problem? - CORRECT ANSWER Becoming

airborne before reaching recommended takeoff speed."

"Which statement relates to Bernoulli's principle? - CORRECT ANSWER Air traveling faster

over the curved upper surface of an airfoil causes lower pressure on the top surface."

"Changes in the center of pressure of a wing affect the aircraft's - CORRECT ANSWER

Aerodynamic balance and controllability."

"An airplane said to be inherently stable - CORRECT ANSWER Requires less effort to

control."

"The four forces acting on an airplane in flight - CORRECT ANSWER Lift, Weight, Thrust,

Drag."

"The left turning tendency of an airplane caused by P-factor is the result of the - CORRECT

ANSWER Propeller blade descending on the right, producing more thrust than the ascending

blade on the left."

"What determines the longitudinal stability of an airplane? - CORRECT ANSWER The

location of the Center of Gravity (CG) with respect to the center of lift."

"When are the four forces that act on an airplane in equilibrium? - CORRECT ANSWER

During unaccelerated flight."

"When does P-factor cause the airplane to yaw to the left? - CORRECT ANSWER When at high

angles of attack." "What causes an airplane (except a T-tail) to pitch nose down when power is reduced and

controls are not adjusted? - CORRECT ANSWER The downwash on the elevator from the

propeller slipstream is reduced and elevator effectiveness is reduced."

"(Refer to Figure 1.) The acute angle A is the angle of - CORRECT ANSWER Attack."

"(Refer to Figure 2.) If an airplane weighs 2,300 pounds, what approximate weight would the airplane structure be required to support during a 60 degree banked turn while maintaining

altitude? - CORRECT ANSWER 4,600 pounds"

"An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One

undesirable flight characteristic a pilot might experience with this airplane would be -

CORRECT ANSWER Difficulty in recovering from a stalled condition."

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

CORRECT ANSWER Attack."

"What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-

level flight? - CORRECT ANSWER Lift equals weight and thrust equals drag."

"In what flight condition must an aircraft be placed in order to spin? - CORRECT ANSWER

Stalled." "(Refer to Figure 2.) If an airplane weights 4,500 pounds, what approximate weight would the airplane structure be required to support during a 45 degree banked turn while maintaining

altitude? - CORRECT ANSWER 6,400 pounds"

"The amount of excess load that can be imposed on the wing of an airplane depends upon the -

CORRECT ANSWER Speed of the airplane."

"During a spin to the left, which wing(s) is/are stalled? - CORRECT ANSWER Both wings are

stalled."