Primary finding
Probable cause
THIS CASE WAS MODIFIED 6/26/2006. The failure of the tail rotor pitch change link due to a fatigue fracture, which resulted in a loss of tail rotor control and separation of the aft tailboom.
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NTSB investigation record
FTW97FA051
CompletedEurocopter As350B2· N6100U
- Date
- November 28, 1996
- Location
- High Island A20,
- Conditions
- VMC
- Record
- Completed
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