1. Which of the following statements regarding energy is true?: d. Kinetic energy can
be traded for potential energy, and potential energy can be traded forkinetic energy
2. The objective in maneuvering the airplane is to manage energy so that:: d.All of the
above
3. What is the effect on total drag if airspeed slows below L/D Max?: c. Dragincreases
because of increased induced drag.
4. A jet pilot flying at L/D Max will obtain best:: b. Endurance
5. When a jet aircraft is flown at the appropriate airspeed for maximum range,which type
of drag predominates?: a. Parasite
6. While already at high speed,what happens if Mach is allowed to increase?-
: d. All of the above
7. What is the result of a shock-induced separation of airflow occurring sym-metrically
near the wing root of a swept wing aircraft?: c. A severe moment of"Mach tuck"
8. The speed of sound generally decreases with increasing altitude. This occurs
because:: a.The air temperature decreases.
9. Critical Mach number can be defined as:: c.The speed of an aircraft in whichairflow
over any part of the aircraft or structure first reaches, but doesn't exceed Mach 1.0.
10. Stability in the vertical axis tends to drive the sideslip angle toward zero.The most
dynamic stability about the vertical axis on modern jet transportsis from:: c. An active
stability augmentation system / yaw damper.
11. Swept wings cause a significant:: b. Reduction in effectiveness of flaps.
12. Why is convergence of Stall AOA and Mmo hazardous?: d. All of the above
13. To maintain altitude in a banked turn, the lift produced by the airplanemust be::
a. Greater than the airplane weight, and the amount is a function ofbank angle.
14. Excessive bank angles at high altitudes can be hazardous because:: d.Allof the
above
15. When operating at constant speed with constant thrust setting at high altitude
(typically above FL250) in slow flight below L/D Max airspeed, any disturbance
causing a decrease in airspeed will result in a further decreasein airspeed unless
thrust in increased. High altitude recovery from slow
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flight while turning is best accomplished by:: c. Increasing thrust to maximum
available thrust and reducing bank angle while accelerating to airspeed above L/D
Max speed. In a thrust limited situation, exiting slow flight will require an immediate
descend as an aerodynamic stall is imminent.
16. Maximum Altitude is the highest altitude at which an airplane can be
operated. Maximum Altitude for an airplane is:: e.The lowest of the above listed
altitudes.
17. Exceed the critical angle of attack and the surface will stall, and lift will
decrease instead of increasing.This is true:: d. Regardless of airplane speed
or attitude.
18. Which of the following statements is true?: d. Recovery from approach to
stall warning is the same as recovery from a stall.
19. The airplane angle of attack is the angle between the wing chord and the
oncoming air or relative wind.: True
20. Airplane stall speeds are published in the Approved Flight Manual for
each airplane model. These speeds are presented as a function of aircraft
weight.Therefor if the pilot maintains airspeed above the appropriate speed
listed for the aircraft weight, the aircraft will not stall.: False
21. The stall speed of an airplane:: b. Is affected by weight and bank angle.
22. Large downward aileron deflections:: a. Cloud induce air separation over
that portion of the wing at very high angles of attack.
23. Place the following steps from the stall recovery template in the correct
order:: d. Disconnect autopilot and autothrottle / autothurst.
b. Apply nose down pitch control until impeding stall indications are eliminated.
c. Adjust bank angle to wings level.
f. Apply thrust as needed.
a. Retract speed brakes and spoilers.
e. Return to the desire flight path.
24. The predominant number of airplane upsets are caused by:: a. Environmental factors.
25. Most of the multi-engine turbojet loss-of-control incidents that are
caused by environmental factors because of:: d.Wake turbulence
26. When initiating recommended airplane upset recovery techniques, the
first two techniques are:: c. Recognize and confirm the situation and disengage
the autopilot and auto-throtles.
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