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![]() "Jim Stewart" wrote in message .. . My instructor carefully pointed out the difference between a stall on final as opposed to a snap spin. I suspect a misuse in terminology, IMHO normal usage of the term 'snap' is to refer to a 'snap roll' (or as the Brits would say, 'flick roll') which is a roll performed with (loading and) rudder only and is really a spin in the logitudinal plane or direction of flight. A stall might be recoverable with no more damage than a looseness of the bowels whereas a spin could really fsk up your day. The gist of his advice was that if you keep the turn coordinated or even add a little extra aileron, the up wing will have to come all the way down through level before it will spin, giving you time get the nose down and level the wings before that spin can develop. IMHO, a combination of stall and yaw in a decending turn (arrival stall) is most likely to result in a spin under the bottom, where the aircraft will enter the spin by dropping the lower or inside wing. On the other hand, a stall combined with yaw in a climbing turn (departure stall) is most likely to result in a spin over the top where the aircraft will enter the spin by dropping the upper or outside wing. I suspect that you or your instructor may be confusing the two. Your instructor is correct that most consider a slip to be more spin resistant than a skid and some/most will maintain that a turning slip is even more spin resistant than cordinated flight. IMHO stall/spin awareness training should include lots of demonstrations (at safe altitude (where recover is made @2000')) of at least incipient (and preferably full spin) spin entry (and recovery) from both arrival and departure stall spins and demonstrations of the circumstances likely to lead to each. OTOH, a flat turn to final can quickly develop into a spin before you can get it under control. IMHO, A flat turn is most likely to be a skid, which most consider to be the uncoordinated condition most likely to result in a spin. Happy landings, |
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