In this region during slow flight
Reverse command
A power on stall is performed in this configuration
Clean
The configuration of power off stalls
Dirty
The airplane must be in this category to practice spins
Utility
This stall occurs due to uncoordinated operation of these two flight controls
ailerons and rudder
The configuration for slow flight
Dirty or landing
This can be the result of an uncoordinated power on stall
Spin
This CG makes recovering from this stall more difficult
Aft
The more stalled wing in the spin
The wing that drops
The most common phase of flight a cross controlled stall will occur
Base to Final turn
A heavier aircraft stalls at a higher airspeed due to cruising closer to
The critical angle of attack
The most common phase of flight a power on stall will be encountered
Takeoff
The type of stall most commonly entered after improper recovery from this stall
Secondary stall
This is the FINAL step in the Spin recovery process
Elevator backpressure to recover to straight and level flight
3000' AGL
Upon recovering from slow flight, you can retract flaps to 0 degrees after this speed
Vx
The measurement of lift as it relates to the AOA
CL or Coefficient of Lift
The proper recovery technique for a power off stall (according to the supplement)
Reduce AOA, level wings, apply max power
This is established in 2-4 turns of a spin
Incipient phase
This stall can result in what condition if not corrected in a real world scenario
low-altitude spin
The region of reverse command begins at this speed
L/D Max
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
The ACS for a commercial pilot in a power off stall
+/- 5 degrees bank,+/- 10 degrees heading
The regulation for CFI's and the spin training they must undergo in the FAR/AIM
14 CFR 61.183 (i)1
Due to the sideslip/abnormal airflow the stall may occur before this happens
Stall horn activation