Slow Flight
Power On-Stalls
Power Off Stalls
Spins
Cross control stalls
100

In this region during slow flight

Reverse command

100

A power on stall is performed in this configuration

Clean

100

The configuration of power off stalls

Dirty

100

The airplane must be in this category to practice spins

Utility

100

This stall occurs due to uncoordinated operation of these two flight controls

ailerons and rudder

200

The configuration for slow flight

Dirty or landing

200

This can be the result of an uncoordinated power on stall

Spin

200

This CG makes recovering from this stall more difficult

Aft

200

The more stalled wing in the spin

The wing that drops

200

The most common phase of flight a cross controlled stall will occur

Base to Final turn

300

A heavier aircraft stalls at a higher airspeed due to cruising closer to

The critical angle of attack

300

The most common phase of flight a power on stall will be encountered

Takeoff

300

The type of stall most commonly entered after improper recovery from this stall

Secondary stall

300

This is the FINAL step in the Spin recovery process

Elevator backpressure to recover to straight and level flight

300
should be performed no less than this altitude

3000' AGL

400

Upon recovering from slow flight, you can retract flaps to 0 degrees after this speed

Vx

400

The measurement of lift as it relates to the AOA

Cor Coefficient of Lift

400

The proper recovery technique for a power off stall (according to the supplement)

Reduce AOA, level wings, apply max power

400

This is established in 2-4 turns of a spin

Incipient phase

400

This stall can result in what condition if not corrected in a real world scenario

low-altitude spin

500

The region of reverse command begins at this speed

L/D Max

500

Any AOA beyond this area/point (not the critical angle of attack) will result in a power on stall

CLMAX or the Maximum Coefficient of lift

500

The ACS for a commercial pilot in a power off stall

+/- 5 degrees bank,+/- 10 degrees heading

500

The regulation for CFI's and the spin training they must undergo in the FAR/AIM

14 CFR 61.183 (i)1 

500

Due to the sideslip/abnormal airflow the stall may occur before this happens

Stall horn activation

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