Aerodynamics of power-on stalls 
Relationship of various factors such as landing gear and flap configuration, weight, center of gravity, load factor, and bank angle to stall speed 
Flight situations where unintentional power-on stalls may occur 
Entry technique and minimum entry altitude 
Performance of power-on stalls in climbing flight (straight or turning) 
Coordination of flight controls 
Recognition of the first indications of power-on stalls 
Recovery technique and minimum recovery altitude 
COMPLETION STANDARDS
Exhibits knowledge of the elements related to power-on stalls 
Selects an entry altitude that allows the task to be completed no lower than 1,500 feet AGL 
Establishes the takeoff or departure configuration 
Sets power to no less than 65 percent available power 
Transitions smoothly from the takeoff or departure attitude to the pitch attitude that will induce a stall.
Maintains a specified heading, &amp;plusmn;10&amp;deg;, in straight flight; maintains a specified angle of bank not to exceed 20&amp;deg;, &amp;plusmn;10&amp;deg;, in turning flight, while inducing the stall 
Recognizes and recovers promptly after the stall occurs by simultaneously reducing the angle of attack, increasing power as appropriate, and leveling the wings to return to a straight-and-level flight attitude with a minimum loss of altitude appropriate for the airplane 
Retracts the flaps to the recommended setting; retracts the landing gear if retractable, after a positive rate of climb is established 
Accelerates to Vx or Vy speed before the final flap retraction; returns to the altitude, heading, and airspeed