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CAX Written - Aerodynamics & Aircraft exam with complete solutions 2024_2025 $11.49   Add to cart

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CAX Written - Aerodynamics & Aircraft exam with complete solutions 2024_2025

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CAX Written - Aerodynamics & Aircraft exam with complete solutions 2024_2025

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  • September 27, 2024
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  • 2024/2025
  • Exam (elaborations)
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CAX Written - Aerodynamics & Aircraft
exam with complete solutions 2024/2025




Which is the symbol for the stalling speed or the minimum steady flight speed in
a specified configuration? - ANSWER-VS1


Which is the correct symbol for the stalling speed or the minimum steady flight
speed at which the airplane is controllable? - ANSWER-VS


Vf - ANSWER-Design Flap Speed


Vle - ANSWER-Maximum Landing Gear Extended Speed


Vne - ANSWER-Never-Exceed Speed


Vy - ANSWER-Speed for best rate of Climb


If an airplane is listed as utility, it would mean that this airplane could be operated
in which of the following maneuvers? - ANSWER-Limited Acrobatics, including
spins (if approved)


Which is true with respect to operating limitations of a 'restricted' category
airplane? - ANSWER-No person may operate a 'restricted' category airplane
carrying passengers or property for compensation for hire.

, Which is true to operating limitations of a "primary" category airplane? -
ANSWER-No person may operate a "primary" category airplane carrying
passengers or property for compensation for hire.


The carriage of passengers for hire by a commercial pilot is - ANSWER-not
authorized in a "limited" category aircraft


No person may operate an aircraft that has an experimental airworthiness
certificate - ANSWER-when carrying persons or property for hire


The ratio between the total air load imposed on the wing and the gross weight of
an aircraft in flight is known as - ANSWER-load factor and directly affects stall
speed


Load factor is the lift generated by the wings of an aircraft at any given time -
ANSWER-divided by the total weight of the aircraft


For a given angle of bank, in any airplane, the load factor imposed in a
coordinated constant-attitude turn - ANSWER-is constant and the stall speed
increased


Airplane wing loading during a level coordinated turn in smooth air depends
upon the - ANSWER-angle of bank


in a rapid recovery from a dive, the effects of load factor would cause the stall
speed to - ANSWER-increase


If an aircraft with a gross weight of 2,000 pounds was subjected to a 60 deg
constant-attitude bank, the total load would be - ANSWER-4,000 pounds


While maintaining a constant angle of bank and altitude in a coordinated turn, an
increase in airspeed will - ANSWER-decrease the rate of turn resulting in no
change in load factor

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