CNN Anderson Cooper 360 August 6, 2015 00:09:00
Aircraft did enter into a very steep stall, and exceeded its mach limits at which point a flutter would occur on the back of that which would explain that broken trailing edge. and then be ripped off by that. but theyll be able to tell that in the metalurgy tests to lack at that and see exactly what type of stress it was under when it cam offe off. one thing conclusive not on the aircraft when it hit the water. sure about that. if it crashed into the water there would be leading edge damage on i...
Source: archive.org