What was found
(CAN)TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DEBONDING TO A POINT 50 MM ALONG LEADING EDGE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN)TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DEBONDING TO A POINT 50 MM ALONG LEADING EDGE.