What was found
(AUS) MAIN ROTOR SPLIT CONE HALF INSTALLED UPSIDE DOWN. MAIN ROTOR TRUNNION CHAMFER DAMAGED BY SHARP EDGE OF CONE. MAST SPLIT CONE SEAT FRETTING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) MAIN ROTOR SPLIT CONE HALF INSTALLED UPSIDE DOWN. MAIN ROTOR TRUNNION CHAMFER DAMAGED BY SHARP EDGE OF CONE. MAST SPLIT CONE SEAT FRETTING.