Earlier quoted context omitted.
I am not a pilot, not even a little bit; But I was under the impression that pilot training has a lot of attention on recovery from a stall or spin, and unless at low altitude, those are generally recoverable (in a small aircraft). Would love for someone with actual knowledge to weigh in, thanks!
In docile trainer aircraft the spin can be recovered from, but that's usually only allowed to be tested in the utility category which has more restrictive weight & balance limits. In famously efficient airframes, it can take several thousand feet. In this article, the famously hard to insure pilot killer the Lancair IV took 4,000 feet: https://www.kitplanes.com/taming-the-lancair-iv/ Part of the Part 23 (certified ai…
> The Cirrus test pilot performing the spin program noted that while all spins entered were recoverable, they required a method of spin recovery that, while not unique in light general aviation airplanes, is different from that of a light trainer airplane in which a pilot is likely to receive spin training. Significant variability in spin recovery training techniques also exists – ranging from merely releasing the elevator control in some light trainers, to movement of the control to neutral, to brisk forward movement to neutral, to brisk foreward movement past neutral, etc.. In the case of the SR20, the proper spin recovery procedure is to briskly move the elevator control to the full down position. This is an unnatural control movement, when the nose of the aircraft may already appear to the pilot to be pointing down sharply. This is also a movement not typically advocated by spin training instructors due to associated discomfort.
https://www.peter2000.co.uk/aviation/misc/3-105960-Cirrussta...