Can you elaborate for the non-rotorheads? You implying retreating blade stall or one of those other scary helicopter things?199 kts at about 1300' AGL...tailboom found 1500' from the main wreckage...I wonder if that film (should it ever see the light of day) will show the aircraft pitching up and roll...
I'm gonna go with "helicopter suddenly realized that there is no physical way that helicopters should work and gave up"Depends what phase of flight that last data point was taken from. Level? Post incident? Not enough info yet.
Can you elaborate for the non-rotorheads? You implying retreating blade stall or one of those other scary helicopter things?
Gotcha.Those are factors of retreating blade stall, yes. But without knowing when that data point was taken, it cannot be attributed to anything yet
Depends what phase of flight that last data point was taken from. Level? Post incident? Not enough info yet.
Update:
NTSB investigator John Lovell said the “data indicates that main rotor [rotations per minute] dropped significantly” and the main rotor blades “appeared to have dropped from their normal plane of rotation.” NTSB investigators have not released their preliminary findings of the July 6 crash in Ellis County that killed two pilots, it appears the main rotor struck the front and back of the helicopter, causing the helicopter to break up in mid-flight, said NTSB spokesman Peter Knudson.
Apparently the out of track blades (two opposing) dropped enough to cut through the cockpit and tailboom in flight. Bad deal............
Haven't picked up on anything else.....Any new word?
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