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ATP Commercial Single-Engine Checkride Questions and Answers 100% Solved $12.99   Add to cart

Exam (elaborations)

ATP Commercial Single-Engine Checkride Questions and Answers 100% Solved

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ATP Commercial Single-Engine Checkride Questions and Answers 100% Solved

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  • October 14, 2024
  • 10
  • 2024/2025
  • Exam (elaborations)
  • Questions & answers
  • ATP
  • ATP
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ATP Commercial Single-Engine Checkride Questions and
Answers 100% Solved

Spoilers Correct Ans-Secondary flight controls are intended to improve the aircraft

performance characteristics or to relieve excessive control loading, and consist of flaps as well

as _____ and trim systems.




Trim Correct Ans-Secondary flight controls are intended to improve the aircraft

performance characteristics or to relieve excessive control loading, and consist of flaps as well

as spoilers and _____ systems.




Magnetos Correct Ans-The purpose of _____ are to increase performance and redundancy.




Performance Correct Ans-The purpose of magnetos are to increase _____ and redundancy.




Redundancy Correct Ans-The purpose of magnetos are to increase performance and

_____.

, ATP Commercial Single-Engine Checkride Questions and
Answers 100% Solved
Detonation Correct Ans-An explosion of the fuel-air mixture inside the cylinder. It occurs

after the compression stroke near or after TDC. During detonation, the fuel/air charge

explodes rather than burning smoothly.




Slotted Correct Ans-The most commonly used flaps today are _____.




Slotted Correct Ans-The Piper Archer has _____ flaps.




Camber Correct Ans-Slotted flaps increase wing _____.




Energy Correct Ans-By opening a slot between the wing and the flap, high pressure air

from the bottom of the wing flows through the slot into the upper surface. This adds _____ to

the wing's boundary layer, delays airflow separation, and produces less drag. The result? Lots

of additional lift, without the excessive drag.




Boundary Layer Correct Ans-By opening a slot between the wing and the flap, high

pressure air from the bottom of the wing flows through the slot into the upper surface. This

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