As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BRACKET REMOVED FOR COMPLIANCE WITH AD 78-08-03 (HINGE BRACKET ASSY). CRACKS FOUND IN BRACKET OFF OF ANCHOR NUT RIVET HOLES. UPON FURTHER INSP, CRACKS FOUND ALSO IN SIMILAR LOCATION ON REAR VERTICAL FIN SPA (PN 17067-02). SERVICEABLE VERTICAL FIN ASSY INSTALLED ON ACFT, AD COMPLIED WITH ON INSTALLED ASSY. TO BE REVISTED IN 1000 HRS (TIS).