UAV Campus | Remote Pilot FAA Exam Prep for Drones

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

As temperature decreases, aircraft performance will

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remain constant. decrease. increase.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

As speed increases, induced drag will

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remain constant. decrease. increase.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

As the angle of attack increases, induced drag will

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remain the same. increase. decrease.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

Which of the following increases load factor the most on fixed wing aircraft?

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Steady climb. Level turn. Unpowered stall.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

At which bank angle does the load factor increase dramatically

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30 degrees. 15 degrees. 45-50 degrees.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

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stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

During an approach to a stall, an increased load factor will cause the aircraft to

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have a tendency to spin. be more difficult to control. stall at a higher airspeed.

As temperature decreases, aircraft performance will

As speed increases, induced drag will

As the angle of attack increases, induced drag will

Which of the following increases load factor the most on fixed wing aircraft?

At which bank angle does the load factor increase dramatically

An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

During an approach to a stall, an increased load factor will cause the aircraft to

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As the angle of attack increases, induced drag will

In a fixed-wing aircraft, pitch is controlled by

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