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#1
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drake wrote:
Hi, there is a HAL HPT-32 (pistonengined 2 seater trainer light a/c) which, when attempting a stall, does not pitch down correctly. Instead one of the wings (either port or starboard (50/50)... no gyro problems due to engine) almost always drops, and this genreally results in the a/c entering a spin (which the rookie pilots are unable to handle, generally). There is no inherent imbalance in the c.g. location due to the fuel tanks ot fuel flow. What could be causing such a wing drop while stalling? Is it soem inherent instability in the roll axis? Sounds like a good rudder trainer. |
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#2
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On Sat, 10 Jan 2004 00:03:57 GMT, john smith
wrote: drake wrote: Hi, there is a HAL HPT-32 (pistonengined 2 seater trainer light a/c) which, when attempting a stall, does not pitch down correctly. Instead one of the wings (either port or starboard (50/50)... no gyro problems due to engine) almost always drops, and this genreally results in the a/c entering a spin (which the rookie pilots are unable to handle, generally). There is no inherent imbalance in the c.g. location due to the fuel tanks ot fuel flow. What could be causing such a wing drop while stalling? Is it soem inherent instability in the roll axis? Sounds like a good rudder trainer. Sounds like my Debonair. And...no it doesn't have wedges on the wing roots although it does have the little 1/4 inch stall strips about 6 inches long. I don't think the first 60 or so had any washout either, but I'd have to dig deeper on that. Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com |
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