Dutch M The A330 is layed out nose heavy
and with stalled main wings the residual main wing lift vector has moved
aft.
up to AoA 45 deg the move is very low,
even with AoA 60 deg it has moved not to much aft.....
look at the curve of the pitching moment (Cm) against angle of incidence posted by machinbird
http://www.pprune.org/tech-log/39510...ml#post5569978