Chair flying / Power-Off Stall
Power-Off Stall
Recognize and recover from a stall in the landing configuration, simulating an approach: reduce the angle of attack, add power, and return to a climb with minimal altitude loss and no secondary stall.
Pre-Maneuver Checklist (CRAAC)
- Clearing turns — two 90° turns or one 180° turn; look for traffic
- Reference point — select a visual reference and set the heading bug
- Altitude — high enough to complete the maneuver at or above 1,500 ft AGLACS minimums: slow flight and stall recovery complete ≥1,500 ft AGL; ground reference maneuvers enter at 600–1,000 ft AGL.
- Airspeed — at or below Va (105 @ 2,325 lb / 90 @ 1,900 lb kt)
- Configuration — fuel pump ON, lights ON, mixture RICH, flaps as needed
Setup
- Landing configuration flowLanding configuration flow: electric fuel pump ON · fuel selector proper tank · mixture full rich · flaps 40.
- Establish a stabilized descent at 66 kt
Execution
- Throttle to idle
- Wings level or up to 20° of bank
- Smoothly raise the nose to the horizon and hold until the stallBring the pitch up to induce the stall; expect the buffet and stall horn as the wing reaches its critical angle of attack.
Recovery
- At the first indication / full stall: reduce AOA, level the wings, add max power“Stall — recover”
- Retract flaps to 25°, then establish Vx or Vy as appropriate
- Flaps to 0° accelerating through Vx (66 kt); return to altitude, heading, and airspeed
ACS tolerances
- Airspeed ±10 kt
- Heading ±10°
- Minimal altitude loss, no secondary stall
Common errors
- Recovering before the stall actually occurs
- Using too much back pressure and inducing a secondary stall
- Not adding power promptly, losing excess altitude