stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition.
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remain constant. decrease. increase.
remain constant. decrease. increase.
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the rudder. the ailerons. the stabilizer.
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.
It increases performance. It has no effect over performance. It decreases performance.
exceeds its critical angle of attack. exceeds the maximum speed. exceeds maximum allowable operating weight.
have a tendency to spin. be more difficult to control. stall at a higher airspeed.
Faster speed. Shorter endurance. Increased maneuverability.