As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CUSTOMER HAS REPORTED DAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40” WIDE AND THE GOUGE DAMAGE IS APPROXIMATELY 0.10” IN LENGTH, 0.05” IN WIDTH AND 0.020” IN DEPTH