"Aural Stall warning is inhibited on ground (except in functional test mode) and above M 0.866."
What caused the STALLSTALL to attenuate at PF's inputs?
Why was it not available at <60 (but airborne?)
Was PF's (initial) reaction to 'overspeed' (as in from bad airdata)? Is there Inertial record of airspeed at >.866M?
Was CL a reaction to O/S? What else could have kept her "flying" to FL380, especially after STALL at "cruise" (a/p) managed parameters? If the STALL was true at a/p drop, how could she have held that much (aero derived) ENERGY?