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![]() "Ian Johnston" wrote in message news:dzZo7CxomoOm-pn2-QjvLCM11RPHz@localhost... On Thu, 23 Jun 2005 21:27:25 UTC, Don Johnstone wrote: The answer is again simple and goes to recognition. A stall with wing drop is just that and provided action is taken to solve that problem, unstall the wing, the a spin will be prevented. A spin is the result of failure at the first step for whatever reason. Everyone properly trained will know the difference. OK, so how would you described the difference. How far does the wing have to drop before /you/ use spin recovery rather than stall recovery? I'm genuinely interested: it's not supposed to be a trick question in any way. Ian What do we think about picking up the wing with rudder when in a stall with wing drop? It's not the BGA method and I'm troubled by someone who recommends it. Stephen |
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Stephen ] writes
What do we think about picking up the wing with rudder when in a stall with wing drop? It's not the BGA method and I'm troubled by someone who recommends it. I'm not sure I understand what you mean. Say, right wing drops in a stall so this "method" would advocate kicking in left rudder as you move the stick forwards to alleviate the stall? Personally, the last thing I'd do when the aircraft was in a stalled state, whether or not a wing drop was involved, would be to intentionally use the rudder in an uncoordinated fashion. That is, unless I actually wanted to spin. -- Bill Gribble http://www.scapegoatsanon.demon.co.uk - Learn from the mistakes of others. - You won't live long enough to make all of them yourself. |
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