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Normal G limits vs Rolling G limits ?
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26th May 2009, 22:53
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dh90pilot
Join Date: May 2009
Location: New Zealand
Age: 67
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When I think of this particular hazard to airframe integrity. I see the ailerons as imparting a twisting force through the wings and main spar which I imagine must then fail for a lower g loading than when the ailerons are neutral.
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