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Faribault, MN
THE PILOT SAID THAT HE WAS EXECUTING A 360 DEGREE TURN WHILE HOVER/TAXIING. THE AIRCRAFT ABRUPTLY WHIPPED AROUND ITS AXIS OF ROTATION, IN THE GUSTY CROSSWIND ENVIRONMENT. THE HELICOPTER BEGAN UNCONTROLLED OSCILLATIONS AND STRUCK THE GROUND WITH A REARWARD MOMENTUM. THE TAIL CONE HIT THE GROUND AND COLLAPSED, CAUSING THE MAIN ROTOR BLADES TO HIT THE GROUND REPEATEDLY BEFORE COMING TO A STOP.
COMPENSATION FOR WIND CONDITIONS WAS NOT ATTAINED BY THE PILOT RESULTING IN LOSS OF DIRECTIONAL CONTROL. A FACTOR RELATED TO THE ACCIDENT WAS A GUSTY CROSSWIND LANDING ENVIRONMENT.
THE PILOT SAID THAT HE WAS EXECUTING A 360 DEGREE TURN WHILE HOVER/TAXIING. THE AIRCRAFT ABRUPTLY WHIPPED AROUND ITS AXIS OF ROTATION, IN THE GUSTY CROSSWIND ENVIRONMENT. THE HELICOPTER BEGAN UNCONTROLLED OSCILLATIONS AND STRUCK THE GROUND WITH A REARWARD MOMENTUM. THE TAIL CONE HIT THE GROUND AND COLLAPSED, CAUSING THE MAIN ROTOR BLADES TO HIT THE GROUND REPEATEDLY BEFORE COMING TO A STOP.