And Answers Rated A+
,Private Pilot FAA Written Exam Verified Questions
And Answers Rated A+
What is one purpose of wing flaps? - Answer - 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... - Answer -
Increase the angle of descent without increasing the airspeed
What is the purpose of the rudder on an airplane? - Answer - To control yaw
Which is not a primary flight control surface?
A. Flaps
B. Stabilator
C Ailerons - Answer - A. Flaps
The elevator controls movement around which axis? - Answer - 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. - Answer -
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. - Answer - 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 - Answer - A. Spoilers
Trim systems are designed to do what? - Answer - 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: - Answer - Lift, Weight, Thrust, and
Drag
,Private Pilot FAA Written Exam Verified Questions
And Answers Rated A+
When are the four forces that act on an airplane in equilibrium? - Answer - During
unaccelerated flight
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-
and-level flight? - Answer - Lift equals weight
Thrust equals drag
Which statement relates to Bernoulli's principle? - Answer - 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... - Answer - Between the wing chord
line and the relative wind
Angle of attack is defined as the chord line of an airfoil and the... - Answer - Direction of
the relative wind
The angle of attack at which an airplane wing stalls will... - Answer - Remain the same
regardless of gross weight
As altitude increases, the indicated airspeed at which a given airplane stalls in a
particular configuration will... - Answer - Remain the same regardless of altitude
In what flight condition must an aircraft be placed in order to spin? - Answer - Stalled
During a spin to the left, which wing(s) is/are stalled? - Answer - Both wings are stalled
How will frost on the wings of an airplane affect takeoff performance? - Answer - Frost
will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability
Why is frost considered hazardous to flight? - Answer - 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? - Answer - Frost my
prevent the airplane from becoming airborne at normal takeoff speed
What is ground effect? - Answer - 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... - Answer - Less than the length of the wingspan above the
surface
, Private Pilot FAA Written Exam Verified Questions
And Answers Rated A+
What must a pilot be aware of as a result of ground effect? - Answer - 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? - Answer - Becoming airborne
before reaching recommended takeoff speed
What force makes an airplane turn? - Answer - The horizontal component of lift
An airplane said to be inherently stable will... - Answer - Require less effort to control
What determines the longitudinal stability of an airplane? - Answer - 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... - Answer -
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... - Answer - 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? - Answer - 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... - Answer - Less
stable at all speeds
In what flight condition is torque effect the greatest in a single-engine airplane? -
Answer - Low airspeed, high power, high angle of attack
The left turning tendency of an airplane caused by P-factor is the result of the... -
Answer - 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? - Answer - When at high
angles of attack
The amount of excess load that can be imposed on the wing of an airplane depends
upon the... - Answer - Speed of the airplane
Which basic flight maneuver increases the load factor on an airplane as compared to
straight-and-level flight? - Answer - Turns