UAV Campus – Questions – Page 25 – 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

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.

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UAV CampusAdministrator

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

What effect does humidity have on flight performance?

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It increases performance. It has no effect over performance. It decreases performance.

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UAV CampusAdministrator

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

In a fixed-wing aircraft, pitch 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

In a fixed-wing aircraft, roll is controlled by

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the stabilizer. the ailerons. the rudder.

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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

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

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 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.