NTSB CAROL · Event
Event FTW82IA268
Aircraft involved
Factual narrative
WHILE THE AIRCRAFT WAS BEING HOVERED LOW AND SLOW AROUND A WATER TROUGH, DIRECTIONAL CONTROL WAS LOST. THE PILOT AUTOROTATED TO THE GROUND AND ON TOUCHDOWN THE RIGHT SKID BUCKLED AND THE TAILROTOR GEARBOX SEPARATED WHEN IT STRUCK AN ANT HILL. THE PILOT ORIGINALLY REPORTED THAT ONE OF THE TAILROTOR BLADES HAD SEPARATED IN WHAT APPEARED TO BE FATIGUE. HOWEVER METALLURGICAL EXAMINATION OF THE FAILED PARTS INDICATED THAT ALL OF THE FRACTURES HAD OCCURED IN OVERLOAD. THE REPORTED WINDS WOULD HAVE BEEN CONDUCIVE TO LOSS OF TAILROTOR EFFECTIVENESS AT LOWER AIRSPEEDS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_FTW82IA268.txt.
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