Private Pilot: FAA Written Exam COMPLETE MULTIPLE QUESTIONS
WITH 100% RATED CORRECT ANSWERS | 2025 LATEST UPDATED |
GET IT CORRECT!!
What is one purpose of wing flaps? - (answers)To enable the pilot to make steeper approaches to
a landing without increasing the airspeed
One of the main functions of flaps during approach and landing is to... - (answers)Increase the
angle of descent without increasing the airspeed
What is the purpose of the rudder on an airplane? - (answers)To control yaw
Which is not a primary flight control surface?
A. Flaps
B. Stabilator
C Ailerons - (answers)A. Flaps
The elevator controls movement around which axis? - (answers)Lateral
Which statement is true concerning primary flight controls?
A. The effectiveness of each control surface increases with speed because there is more airflow
over them.
B. Only when all three primary flight controls move in sequence do the airflow and pressure
distribution change over and around the airfoil.
C. Primary flight controls include ailerons, rudder, elevator, and trim systems. - (answers)A. The
effectiveness of each control surface increases with speed because there is more airflow over
them
Which of the following is true concerning flaps?
A. Flaps are attached to the leading edge of the wing and are used to increase wing lift.
,B. Flaps allow an increase in the angle of descent without increasing airspeed.
C. Flaps are high drag devices deployed from the wings to reduce lift. - (answers)B. Flaps allow
an increase in the angle of descent without increasing airspeed
Which device is a secondary flight control?
A. Spoilers
B. Ailerons
C. Stabilators - (answers)A. Spoilers
Trim systems are designed to do what? - (answers)They relieve the pilot of the need to maintain
constant back pressure on the flight controls
The four forces acting on an airplane in flight are: - (answers)Lift, Weight, Thrust, and Drag
When are the four forces that act on an airplane in equilibrium? - (answers)During unaccelerated
flight
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level
flight? - (answers)Lift equals weight
Thrust equals drag
Which statement relates to Bernoulli's principle? - (answers)Air traveling faster over the curve
upper surface of an airfoil causes lower pressure on the top surface
The term "angle of attack" is defined as the angle... - (answers)Between the wing chord line and
the relative wind
Angle of attack is defined as the chord line of an airfoil and the... - (answers)Direction of the
relative wind
,The angle of attack at which an airplane wing stalls will... - (answers)Remain the same
regardless of gross weight
As altitude increases, the indicated airspeed at which a given airplane stalls in a particular
configuration will... - (answers)Remain the same regardless of altitude
In what flight condition must an aircraft be placed in order to spin? - (answers)Stalled
During a spin to the left, which wing(s) is/are stalled? - (answers)Both wings are stalled
How will frost on the wings of an airplane affect takeoff performance? - (answers)Frost will
disrupt the smooth flow of air over the wing, adversely affecting its lifting capability
Why is frost considered hazardous to flight? - (answers)Frost spoils the smooth flow of air over
the wings, thereby decreasing lifting capability
How does frost affect the lifting surfaces of an airplane on takeoff? - (answers)Frost my prevent
the airplane from becoming airborne at normal takeoff speed
What is ground effect? - (answers)The result of inference of the surface of the earth with the
airflow patterns about an airplane
Floating caused by the phenomenon of ground effect will be most realized during an approach to
land when at... - (answers)Less than the length of the wingspan above the surface
What must a pilot be aware of as a result of ground effect? - (answers)Induced drag decreases;
therefore, any excess speed at the point of flare may cause considerable floating
Ground effect is most likely to result in which problem? - (answers)Becoming airborne before
reaching recommended takeoff speed
, What force makes an airplane turn? - (answers)The horizontal component of lift
An airplane said to be inherently stable will... - (answers)Require less effort to control
What determines the longitudinal stability of an airplane? - (answers)The location of the CG with
respect to the center of lift
Changes in the center of pressure of a wing affect the aircraft's... - (answers)Aerodynamic
balance and controllability
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... -
(answers)Difficulty in recovering from a stalled condition
What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls
are not adjusted? - (answers)The downwash on the elevators from the propeller slipstream is
reduced and the elevator effectiveness is reduced
Loading an airplane to the most aft CG will cause the airplane to be... - (answers)Less stable at
all speeds
In what flight condition is torque effect the greatest in a single-engine airplane? - (answers)Low
airspeed, high power, high angle of attack
The left turning tendency of an airplane caused by P-factor is the result of the... -
(answers)Propeller blade descending on the right, producing more thrust than the ascending
blade on the left
When does P-factor cause the airplane to yaw to the left? - (answers)When at high angles of
attack
WITH 100% RATED CORRECT ANSWERS | 2025 LATEST UPDATED |
GET IT CORRECT!!
What is one purpose of wing flaps? - (answers)To enable the pilot to make steeper approaches to
a landing without increasing the airspeed
One of the main functions of flaps during approach and landing is to... - (answers)Increase the
angle of descent without increasing the airspeed
What is the purpose of the rudder on an airplane? - (answers)To control yaw
Which is not a primary flight control surface?
A. Flaps
B. Stabilator
C Ailerons - (answers)A. Flaps
The elevator controls movement around which axis? - (answers)Lateral
Which statement is true concerning primary flight controls?
A. The effectiveness of each control surface increases with speed because there is more airflow
over them.
B. Only when all three primary flight controls move in sequence do the airflow and pressure
distribution change over and around the airfoil.
C. Primary flight controls include ailerons, rudder, elevator, and trim systems. - (answers)A. The
effectiveness of each control surface increases with speed because there is more airflow over
them
Which of the following is true concerning flaps?
A. Flaps are attached to the leading edge of the wing and are used to increase wing lift.
,B. Flaps allow an increase in the angle of descent without increasing airspeed.
C. Flaps are high drag devices deployed from the wings to reduce lift. - (answers)B. Flaps allow
an increase in the angle of descent without increasing airspeed
Which device is a secondary flight control?
A. Spoilers
B. Ailerons
C. Stabilators - (answers)A. Spoilers
Trim systems are designed to do what? - (answers)They relieve the pilot of the need to maintain
constant back pressure on the flight controls
The four forces acting on an airplane in flight are: - (answers)Lift, Weight, Thrust, and Drag
When are the four forces that act on an airplane in equilibrium? - (answers)During unaccelerated
flight
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level
flight? - (answers)Lift equals weight
Thrust equals drag
Which statement relates to Bernoulli's principle? - (answers)Air traveling faster over the curve
upper surface of an airfoil causes lower pressure on the top surface
The term "angle of attack" is defined as the angle... - (answers)Between the wing chord line and
the relative wind
Angle of attack is defined as the chord line of an airfoil and the... - (answers)Direction of the
relative wind
,The angle of attack at which an airplane wing stalls will... - (answers)Remain the same
regardless of gross weight
As altitude increases, the indicated airspeed at which a given airplane stalls in a particular
configuration will... - (answers)Remain the same regardless of altitude
In what flight condition must an aircraft be placed in order to spin? - (answers)Stalled
During a spin to the left, which wing(s) is/are stalled? - (answers)Both wings are stalled
How will frost on the wings of an airplane affect takeoff performance? - (answers)Frost will
disrupt the smooth flow of air over the wing, adversely affecting its lifting capability
Why is frost considered hazardous to flight? - (answers)Frost spoils the smooth flow of air over
the wings, thereby decreasing lifting capability
How does frost affect the lifting surfaces of an airplane on takeoff? - (answers)Frost my prevent
the airplane from becoming airborne at normal takeoff speed
What is ground effect? - (answers)The result of inference of the surface of the earth with the
airflow patterns about an airplane
Floating caused by the phenomenon of ground effect will be most realized during an approach to
land when at... - (answers)Less than the length of the wingspan above the surface
What must a pilot be aware of as a result of ground effect? - (answers)Induced drag decreases;
therefore, any excess speed at the point of flare may cause considerable floating
Ground effect is most likely to result in which problem? - (answers)Becoming airborne before
reaching recommended takeoff speed
, What force makes an airplane turn? - (answers)The horizontal component of lift
An airplane said to be inherently stable will... - (answers)Require less effort to control
What determines the longitudinal stability of an airplane? - (answers)The location of the CG with
respect to the center of lift
Changes in the center of pressure of a wing affect the aircraft's... - (answers)Aerodynamic
balance and controllability
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... -
(answers)Difficulty in recovering from a stalled condition
What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls
are not adjusted? - (answers)The downwash on the elevators from the propeller slipstream is
reduced and the elevator effectiveness is reduced
Loading an airplane to the most aft CG will cause the airplane to be... - (answers)Less stable at
all speeds
In what flight condition is torque effect the greatest in a single-engine airplane? - (answers)Low
airspeed, high power, high angle of attack
The left turning tendency of an airplane caused by P-factor is the result of the... -
(answers)Propeller blade descending on the right, producing more thrust than the ascending
blade on the left
When does P-factor cause the airplane to yaw to the left? - (answers)When at high angles of
attack
