Quote:
Originally Posted by BEA Final Report (English) p.22-23
At 2 h 10 min 51, the stall warning triggered again, in a continuous manner. The thrust levers were positioned in the TO/GA detent and the PF made nose-up inputs. The recorded angle of attack, of around 6 degrees at the triggering of the stall warning, continued to increase. The trimmable horizontal stabilizer (THS) began a nose-up movement and moved from 3 to 13 degrees pitch-up in about 1 minute and remained in the latter position until the end of the flight.
That's a factual account of the THS behaviour - and the limit of what the BEA can say.
Indeed this is a factual account and the limit of what BEA want to say
Conf asked about a analyze ....
I find (like him certainly) that what you quoted from the report is not a analyze ..
But maybe (or likely certainly) the BEA think that a analyze about is not relevant ...