- ATP QUIZ #3
- Instructor's
Name___________________________
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- Student's
Name_____________________________ Date__________________
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- Instructions: Answer the multiple-choice
question with the best possible answer. Write the answer
to the essay question in the space provided. If more
space is needed, use the reverse side.
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- 1. When are inboard ailerons normally
used?
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- 2. When are outboard ailerons normally
used?
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- 3. Which of the following is
considered an auxiliary flight control?
- a. Ruddervator.
- b. Upper rudder.
- c. Leading-edge flaps.
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- 4. What is the purpose of a control
tab?
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- 5. What is the purpose of an
anti-servo tab?
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- 6. What is the purpose of a servo tab?
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- 7. Which is a purpose of leading-edge
flaps?
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- 8. For which purpose may flight
spoilers be used?
- a. Reduce the wings' lift upon
landing.
- b. Increase the rate of descent
without increasing aerodynamic drag.
- c. Aid in longitudinal balance when
rolling an airplane into a turn.
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- 9. Which is a purpose of wing-mounted
vortex generators?
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- 10. Which of the following are
considered primary flight controls?
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- 11. How can turbulent air cause an
increase in stalling speed of an airfoil?
- 12. If an aircraft with a gross weight
of 2,000 pounds were subjected to a total load of
6,000 pounds in flight, the load factor would be how
many G’s?
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- 13. What is the safest and most
efficient takeoff and initial climb procedure in a
light, twin-engine airplane?
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- 14. What procedure is recommended for
an engine-out approach and landing?
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- 15. What performance should a pilot of
a light, twin-engine airplane be able to maintain at
VMC?
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- 16. What criteria determines which
engine is the ``critical'' engine of a twin-engine
airplane?
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- 17. What effect, if any, does altitude
have on VMC for an airplane with unsupercharged
engines?
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- 18. Under what condition should stalls
never be practiced in a twin-engine airplane?
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- 19. Describe dynamic longitudinal
stability.
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- 20. What is the reason for variations
in geometric pitch along a propeller or rotor blade?
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- 21. If an engine failure occurs at an
altitude above single-engine ceiling, what airspeed
should be maintained?
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- 22. What is the approximate resulting
climb performance loss in terms of percent, when one
engine on a twin-engine fails?
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- 23. Under what condition is VMC the
highest?
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- 24. What characteristic should exist
if an airplane is loaded to the rear of its CG range?
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- 25. What is the highest speed possible
without supersonic flow over the wing?