Originally Posted by
Magplug
It has been a few years since I flew heavy helicopters but fundamentally the loss of TR control 200-500 feet above the stadium was not survivable.
The AAIB will want to quickly establish the '4 corners' of the accident to confirm that all the components of the aircraft are present at the crash scene. One video shot seems to suggest that a component flew away from the aircraft with high energy immediately before control was lost, the only components posessing such energy would have been a MR pocket (or two) or a TR blade. The fact that the aircraft immediately lost yaw control indicates it may have been a TR blade.... Crash site pictures indicate 2 TR blades present but one is half missing, you could argue it had been consumed in the post crash fire but the edges appear jagged as if it had been torn apart rather than burnt. The AW 169 has an impeccable safety record with no history of TR blade mishaps or other TR drive or contol problems. So why in this case?
TR blades are stressed in construction so as to survive a minor impact from a birdstrike and still perform their role. In this day and age modern helicopters do not crash because birds fly through the tail rotors. In-service failure due to substandard manufacturing is a possibility but frankly unlikely. It is much more likely that a foreign object struck the tailrotor causing sufficient damage to cause blade failure and separation.... But caused by what? The surrounding area several hundred yards in every direction will be thoroughly searched for debris.... who knows what else might be found?
Might we be looking at the first fatal aviation accident due to an aircraft colliding with a drone?
The stadium is located next to the River Soar which has a fair quantity of resident Canada geese , they are are known to fly at night - would a TR survive a strike from a bird of this size?