Definition
A wing stalls at a critical angle of attack, not at a particular airspeed, so any manoeuvre that increases load factor raises the airspeed at which that angle is reached. In a level turn at 45 degrees of bank the load factor is about 1.41G and the stall speed rises by roughly 19 percent; at 60 degrees it is 2G and the stall speed rises by about 41 percent. That is the whole of the accelerated stall: the same aerodynamic event as a straight-ahead stall, arriving sooner and usually with less warning.
FAA-S-ACS-7 requires the applicant to select an entry altitude that allows the Task to be completed no lower than 3,000 feet AGL — higher than the 1,500 feet used for power-off stalls in a single — to set power such that the airspeed does not exceed maneuvering speed or any other POH/AFM limitation, and to establish and maintain a coordinated turn at 45 degrees of bank while increasing elevator back pressure smoothly and firmly until an impending stall is reached. The applicant acknowledges the cues at the first indication, recovers in accordance with the POH, configures as the manufacturer recommends, accelerates to best angle or best rate of climb speed, and returns to the altitude, heading and airspeed specified by the evaluator.
The maneuvering-speed limit is the safety boundary that makes the demonstration acceptable: at or below that speed the wing will stall before the airframe reaches its structural load limit.
Why It Matters for Flight Schools
The accelerated stall matters far beyond the checkride because it is the stall that actually kills people. The classic base-to-final overshoot is an accelerated stall: a pilot steepens the turn, loads the wing, and reaches the critical angle of attack at an airspeed that looked comfortably safe on the indicator. Teaching it at altitude is how a school makes that connection before a student meets it in the pattern.
For instructors it is also a standardisation item. Because the entry involves deliberately loading the airplane, the briefing has to be explicit about the maneuvering-speed limit, the altitude floor, and what an acceptable recovery looks like, so that the demonstration is consistent across a fleet and across instructors.
How Aviatize Handles This
Aviatize lets a school hold stall training as separate graded objectives — power-off, power-on and accelerated — rather than one stall entry, so a training record shows which type a student has actually demonstrated and to what standard. Where a school attaches its own altitude floors and briefing notes to the objective, every instructor sees the same standard at the point of grading.
Frequently Asked Questions
- Why does a stall happen at a higher speed in a turn?
- Because the wing stalls at a critical angle of attack rather than a fixed airspeed. A banked turn increases load factor — about 1.41G at 45 degrees of bank — and the airspeed at which the critical angle is reached rises with the square root of the load factor, roughly 19 percent higher at 45 degrees and 41 percent at 60.
- What altitude is required for an accelerated stall demonstration?
- FAA-S-ACS-7 requires an entry altitude that allows the Task to be completed no lower than 3,000 feet above ground level. That is higher than the 1,500 feet AGL floor the same ACS sets for power-off stalls in a single-engine airplane.
- Why is maneuvering speed a limit for this maneuver?
- At or below maneuvering speed the wing reaches its critical angle of attack and stalls before the airframe reaches its structural load limit. The ACS therefore requires power set so airspeed does not exceed maneuvering speed or any other POH or AFM limitation during the entry.