UAV Loading and Performance

30 degrees. 15 degrees. 45-50 degrees.

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

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.

  34 pounds. 38 pounds.  47 pounds.

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.

Remote Pilot in Command  Manufacturer. Owner or operator

the rudder. the ailerons. the stabilizer. 

Faster speed. Shorter endurance.  Increased maneuverability.

Steady climb. Level turn. Unpowered stall.

stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition.