Takata - Engines run on the ground or in testbeds without airspeed, wouldn't a modern FADEC with sensitive surge protection managing fuel flow maintain operation even where there is not enough air massflow/density to attempt re-light? And if engines not stalled at altitude why would they with increasing air density below 6000ft?
Previous posts suggest rate of fall fully stalled would be much greater than 6000ft/min, so a single event would have to have started later/higher, but could still end 2:14:30.
[edit: deleted ref to RAT, its the APU thats been seen]
Last edited by sensor_validation; 5th May 2011 at 17:37.