I can understand how the 31-deg pitch-up occured, but how did the following 76-deg nose-down pitch movement (to 45-deg aircraft nose down) occur? Surely a stall at 31-deg but with full power on a powerful aircraft would not need such a large nose-down movement, or for the aircraft to pitched down so far to accelerate back out of the stall.
Last edited by dangrey; 23rd Feb 2009 at 15:21.