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Cape Girardeau, MO
THE PLT REPORTED THAT DURING FLT, HE HEARD A GRINDING NOISE, THEN THE HELICOPTER PITCHED UP & TO THE LEFT. HE REDUCED POWER & NOTICED THAT THE TAIL ROTOR WAS INOPERATIVE. DURING A RUN-ON LANDING APPROACH, THE HELICOPTER BEGUN TO YAW, THEN BEFORE TOUCHDOWN, IT BEGAN TO SPIN. DURING GROUND IMPACT, THE LANDING GEAR SKIDS WERE TWISTED, THE VERTICAL FIN WAS KNOCKED OFF, ALL MAIN ROTOR BLADES STRUCT THE GROUND & THE RIGHT FRONT & RIGHT REAR DOORS WERE DAMAGED. AN INVESTIGATION REVEALED THE TAIL ROTOR DRIVE SHAFT, PN 350A34-0110-02, HAD FAILED.
THE PLT REPORTED THAT DURING FLT, HE HEARD A GRINDING NOISE, THEN THE HELICOPTER PITCHED UP & TO THE LEFT. HE REDUCED POWER & NOTICED THAT THE TAIL ROTOR WAS INOPERATIVE. DURING A RUN-ON LANDING APPROACH, THE HELICOPTER BEGUN TO YAW, THEN BEFORE TOUCHDOWN, IT BEGAN TO SPIN. DURING GROUND IMPACT, THE LANDING GEAR SKIDS WERE TWISTED, THE VERTICAL FIN WAS KNOCKED OFF, ALL MAIN ROTOR BLADES STRUCT THE GROUND & THE RIGHT FRONT & RIGHT REAR DOORS WERE DAMAGED. AN INVESTIGATION REVEALED THE TAIL ROTOR DRIVE SHAFT, PN 350A34-0110-02, HAD FAILED.