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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

According to 14 CFR part 107, who is responsible for determining the performance of a small unmanned aircraft?

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Remote Pilot in Command Manufacturer. Owner or operator

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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

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

When loading cameras or other equipment on an sUAS, mount the items in a manner that

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can be easily removed without the use of tools. is visible to the visual observer or other crew members. does not adversely affect the center of gravity.

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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.

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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

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

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

What could be a consequence of operating a small unmanned aircraft above its maximum allowable weight?

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Faster speed. Shorter endurance. Increased maneuverability.