2

Your wrote: a value which, according to the report, would not have been altered by the aircraft's rapidly-increasing AOA The report did not say that (but I can see how that confusion can arise). It said the 1) flap retraction and 2) increasing g load -- would not alter the AOA trip point of 13.5 -- no mention of rapidly-increasing AOA: the flaps had ...


Only top voted, non community-wiki answers of a minimum length are eligible