experience a reduction in ground friction and require a slight power reduction

require a lower angle of attack to maintain the same lift coefficient

experience an increase in induced drag and a decrease in performance

Settling to the surface abruptly during landing

Becoming airborne before reaching recommended takeoff speed

Inability to get airborne even though airspeed is sufficient for normal takeoff needs

The horizontal component of lift

Centrifugal force

The vertical component of lift

The relationship of thrust and lift to weight and drag

The effectiveness of the horizontal stabilizer, rudder, and rudder trim tab

The location of the center of gravity (CG) with respect to the center of lift

require less effort to control

not spin

be difficult to stall

lift/drag ratio

aerodynamic balance and controllability

lifting capacity

stalling at higher-than-normal airspeed

a longer takeoff run

difficulty in recovering from a stalled condition

The CG shifts forward when thrust and drag are reduced

When thrust is reduced to less than weight, lift is also reduced and the wings can no longer support the weight

The downwash on the elevators from the propeller slipstream is reduced and elevator effectiveness is reduced

less stable at slow speeds, but more stable at high speeds

less stable at all speeds

less stable at high speeds, but more stable at low speeds

Both aircraft groundspeed and angle of attack will increase

Airspeed will remain relatively constant but the aircraft will climb

The aircraft will accelerate, which will cause a turn to the right

Low airspeed, low power, low angle of attack

High airspeed, high power, high angle of attack

Low airspeed, high power, high angle of attack

porpeller blade descending on the right, producing more thrust than the ascending blade on the left

clockwise rotation of the engine and the propeller turning the airplane counterclockwise

gyroscopic forces applied to the rotating propeller blades acting 90 degrees in advance of the point the force was applied

When at high airspeed

When at high angles of attack

When at low angles of attack

Climbs

Stalls

Turns

1,200 pounds

3,100 pounds

3,960 pounds