Chair flying / Accelerated Stall
Accelerated Stall
Demonstrate that a wing stalls at its critical angle of attack regardless of airspeed: load the wing in a banked turn until it stalls at a higher-than-normal speed, then recover at the first indication.
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
- Slow to about 80 kt during the clearing turns
- Clean configuration flowClean configuration flow: electric fuel pump ON · fuel selector proper tank · mixture full rich · flaps 0.
Execution
- Establish a coordinated 45° bank turn
- Slowly reduce power to idle
- Increase back pressure to hold altitude and load the wing until it stallsThe higher load factor in the turn raises the stall speed (Vs × √load factor), so the wing stalls well above the 1-G stall speed — the same critical angle of attack, a higher airspeed.
Recovery
- At the first indication (buffet or horn): reduce AOA, level the wings, add max power“Buffet — recover”
- Return to the specified altitude, heading, and airspeed
ACS tolerances
- Recover at the first indication of the stall
- No secondary stall
Common errors
- Uncoordinated entry — a wing drops toward a spin
- Waiting past the first indication before recovering
- Excessive altitude loss in the recovery