The four forces acting on an airplane in flight are
A – lift, weight, thrust, and drag.
B – lift, weight, gravity, and thrust.
C – lift, gravity, power, and friction.
2. Multiple Choice
1 minute
1 pt
When are the four forces that act on an airplane in equilibrium?
A – During unaccelerated flight.
B – When the aircraft is accelerating.
C – When the aircraft is at rest on the ground.
3. Multiple Choice
1 minute
1 pt
(Refer to Figure 1.) The acute angle A is the angle of
A – incidence.
B – attack.
C – dihedral.
4. Multiple Choice
1 minute
1 pt
The term “angle of attack” is defined as the angle between the
A – chord line of the wing and the relative wind.
B – airplane’s longitudinal axis and that of the air striking the airfoil.
C – airplane’s center line and the relative wind.
5. Multiple Choice
1 minute
1 pt
The angle between the chord line of an airfoil and the relative wind is known as the angle of
A – lift.
B – attack.
C – incidence.
6. Multiple Choice
1 minute
1 pt
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?
A – Lift, drag, and weight equal thrust.
B – Lift and weight equal thrust and drag.
C – Lift equals weight and thrust equals drag.
7. Multiple Choice
1 minute
1 pt
One of the main functions of flaps during approach and landing is to
A – decrease the angle of descent without increasing the airspeed.
B – enable a touchdown at a higher indicated airspeed.
C – increase the angle of descent without increasing the airspeed.
8. Multiple Choice
1 minute
1 pt
What is one purpose of wing flaps?
A – To decrease wing area to vary the lift.
B – To relieve the pilot of maintaining continuous pressure on the controls.
C – To enable the pilot to make steeper approaches to a landing without increasing the airspeed.
9. Multiple Choice
1 minute
1 pt
The angle of attack at which an airplane wing stalls
A – increases if the CG is moved forward.
B – changes with an increase in gross weight.
C – remains the same regardless of gross weight.
10. Multiple Choice
1 minute
1 pt
What is ground effect?
A – The result of the interference of the surface of the Earth with the airflow patterns about an airplane.
B – The result of an alteration in airflow patterns increasing induced drag about the wings of an airplane.
C – The result of the disruption of the airflow patterns about the wings of an airplane to the point where the wings can no longer support the airplane in flight.
11. Multiple Choice
1 minute
1 pt
Floating caused by the phenomenon of ground effect is most realized during an approach to land when at
A – a higher-than-normal angle of attack.
B – less than the length of the wingspan above the surface.
C – twice the length of the wingspan above the surface.
12. Multiple Choice
1 minute
1 pt
What must a pilot be aware of as a result of ground effect?
A – Wingtip vortices increase, creating wake turbulence problems for arriving and departing aircraft.
B – Induced drag decreases; therefore, any excess speed at the point of flare may cause considerable floating.
C – A full stall landing requires less up elevator deflection than a full stall that is done free of ground effect.
13. Multiple Choice
1 minute
1 pt
Ground effect is most likely to result in which problem?
A – Setting to the surface abruptly during landing.
B – Becoming airborne before reaching recommended takeoff speed.
C – Inability to get airborne even though airspeed is sufficient for normal takeoff needs.
14. Multiple Choice
1 minute
1 pt
Which statement relates to Bernoulli’s principle?
A – For every action there is an equal and opposite reaction.
B – An additional upward force is generated as the lower surface of the wing deflects air downward.
C – Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface.
15. Multiple Choice
1 minute
1 pt
Changes in the center of pressure of a wing affect the aircraft’s