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.
UAV Loading and Performance
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30 degrees. 15 degrees. 45-50 degrees.
Remote Pilot in Command Manufacturer. Owner or operator
remain constant. decrease. increase.
34 pounds. 38 pounds. 47 pounds.
Aircraft Weight and Balance Handbook. Aeronautical Information Manual (AIM). Pilot’s Operating Handbook or UAS Flight Manual.
It increases performance. It has no effect over performance. It decreases performance.
stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition.
Steady climb. Level turn. Unpowered stall.
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.