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On May 29, 10:58*am, Bertie the Bunyip wrote:
He's obviously looking at getting an answer that it will be the same speed, but that's not correct. It probably wouldn;'t be far off it, but the thrust line and any up or down thrust will play a big part in what the airplane settles at after the engine dies. And in a propeller-driven plane with a conventional (as opposed to a T- tail) empennage, the design and location (relative to the prop blast) of the horizontal stab will probably swamp the effect of the thrust line. In most cases, the trim speed will actually be higher when the engine quits. This question is a good one - without more information it can't really be answered, but it's a great jumping-off point for a discussion of the way pitch, power, and speed interact. The airplane CFI PTS includes demonstrating and explaining trim stalls (I remember having to do one on my CFI-ASE ride). So at least the people who wrote the PTS expected the CFI to have that level of aerodynamic knowledge, as well they should. It would help him to explain to the student why certain things happen, and what he should expect. But that's probably way beyond what the average ops inspector is going for (and probably more than he knows) - and it's somewhat depressing that it's obvious to us that he's going for the wrong answer. You would think we would give the guy the benefit of the doubt - but having met several ops inspectors, I find that difficult to do. Michael |
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