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Lapeer, MI
THE HELICOPTER WAS IN CRUISE FLT WHEN THE RGT SIDE HORIZONTAL STABILIZER ATTACH TUBE FAILED & SEPARATED FROM THE TAIL BOOM, THEN CONTACTED THE TAIL ROTOR. THIS RESULTED IN FAILURE OF THE TAIL ROTOR DRIVE SHAFT FLEX COUPLING AT THE TAIL ROTOR GEAR BOX. IN TURN, THERE WAS A LOSS OF TAIL ROTOR THRUST. THE PLT MADE A SUCCESSFUL AUTOROTATION IN AN OPEN FIELD. AN EXAM OF THE RGT HORIZONTAL STABILIZER ATTACH TUBE REVEALED IT HAD FAILED FROM FATIGUE AT THE RGT INBOARD ATTACH HOLE. THE FATIGUE ORIGINATED AT A SURFACE DEFECT ON THE OUTER DIAMETER OF THE TUBE WHICH WAS CAUSED BY MISALIGNED DRILLING.
THE HELICOPTER WAS IN CRUISE FLT WHEN THE RGT SIDE HORIZONTAL STABILIZER ATTACH TUBE FAILED & SEPARATED FROM THE TAIL BOOM, THEN CONTACTED THE TAIL ROTOR. THIS RESULTED IN FAILURE OF THE TAIL ROTOR DRIVE SHAFT FLEX COUPLING AT THE TAIL ROTOR GEAR BOX. IN TURN, THERE WAS A LOSS OF TAIL ROTOR THRUST. THE PLT MADE A SUCCESSFUL AUTOROTATION IN AN OPEN FIELD. AN EXAM OF THE RGT HORIZONTAL STABILIZER ATTACH TUBE REVEALED IT HAD FAILED FROM FATIGUE AT THE RGT INBOARD ATTACH HOLE. THE FATIGUE ORIGINATED AT A SURFACE DEFECT ON THE OUTER DIAMETER OF THE TUBE WHICH WAS CAUSED BY MISALIGNED DRILLING.