UAV Loading and Performance – Page 2 – UAV Campus | Remote Pilot FAA Exam Prep for Drones

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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

If an unmanned airplane weighs 33 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?

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34 pounds. 38 pounds. 47 pounds.

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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

The term “angle of attack” is defined as the angle between the

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airplane’s center line and the relative wind. chord line of the wing and the relative wind. airplane’s longitudinal axis and that of the air striking the airfoil.

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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

The angle of attack at which an airplane wing stalls will

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increase if the CG is moved forward. remain the same regardless of gross weight. change with an increase in gross weight.

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UAV CampusAdministrator

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

The acute angle A is the angle of

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Attack. Dihedral. Incidence.

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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

In a fixed-wing aircraft, yaw is controlled by

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the rudder. the ailerons. the stabilizer.

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UAV CampusAdministrator

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

To ensure that the unmanned aircraft center of gravity (CG) limits are not exceeded, follow the aircraft loading instructions specified in the

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Aircraft Weight and Balance Handbook. Aeronautical Information Manual (AIM). Pilot’s Operating Handbook or UAS Flight Manual.