Originally Posted by
Centaurus
Either an aeroplane drops a wing at point of stall or it doesn't.
Quite a few configurations and flight states to consider, for example
Of course there was that error in the crew moment arms back then so the actual CG was further aft than determined by the POH.
Originally Posted by
Centaurus
Is this at idle power? if not, how much power has to be used to meet certification requirements? Seems to me a grey area when it comes to LSA certification as against non LSA types.
Not a grey area at all as it seems to me that the requirements are quite clear.
Originally Posted by
Centaurus
Feel free.