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Beech Grove, IN
THE ACCIDENT HELICOPTER EXPERIENCED A LOSS OF CYCLIC PITCH CONTROL DURING LIFTOFF TO A HOVER AT THE START OF A BUSINESS FLIGHT. THE HELICOPTER PITCHED UP, STRIKING THE TAIL ROTOR INTO THE GROUND AND THEN ROLLED ONTO ITS RIGHT SIDE. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE. THE COMMERCIAL PILOT AND TWO PASSENGERS WERE NOT INJURED. ON SCENE INSPECTION OF THE WRECKAGE SHOWED A FLIGHT CONTROL LINKAGE DISCONNECT. THE MISSING BOLT WAS FOUND ON THE GROUND NEXT TO THE HELICOPTER. THE OTHER CONNECTING HARDWARE WAS NOT FOUND. THE PILOT STATED THAT HE DID NOT NOTICE THE MISSING NUT DURING HIS PREFLIGHT INSPECTION.
IMPROPER INSTALLATION OF THE FLIGHT CONTROL LINKAGE DURING MAINTENANCE. COMPLACENCY AND INADEQUATE INSPECTION OF THE HELICOPTER BY MAINTENANCE PERSONNEL AND THE PILOT ARE FACTORS IN THE ACCIDENT.
THE ACCIDENT HELICOPTER EXPERIENCED A LOSS OF CYCLIC PITCH CONTROL DURING LIFTOFF TO A HOVER AT THE START OF A BUSINESS FLIGHT. THE HELICOPTER PITCHED UP, STRIKING THE TAIL ROTOR INTO THE GROUND AND THEN ROLLED ONTO ITS RIGHT SIDE. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE. THE COMMERCIAL PILOT AND TWO PASSENGERS WERE NOT INJURED. ON SCENE INSPECTION OF THE WRECKAGE SHOWED A FLIGHT CONTROL LINKAGE DISCONNECT. THE MISSING BOLT WAS FOUND ON THE GROUND NEXT TO THE HELICOPTER. THE OTHER CONNECTING HARDWARE WAS NOT FOUND. THE PILOT STATED THAT HE DID NOT NOTICE THE MISSING NUT DURING HIS PREFLIGHT INSPECTION.