UAV Loading and Performance

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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

When operating an unmanned airplane, the remote pilot should consider that the load factor on the wings may be increased anytime

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the CG is shifted rearward to the aft CG limit. the gross weight is reduced. the airplane is subjected to maneuvers other than straight and level flight.

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UAV CampusAdministrator

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

A stall occurs when the smooth airflow over the unmanned airplane’s wing is disrupted and the lift degenerates rapidly. This is caused when the wing

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exceeds its critical angle of attack. exceeds the maximum speed. exceeds maximum allowable operating weight.

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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

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

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

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.

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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

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, yaw is controlled by

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the rudder. the ailerons. the stabilizer.