What was found
INSPECTION TYPE:SI, VERTICAL FIN STA 180.6, STR 7, ANGLE IS CRACKED AT FASTENER HOLE. REMOVED FASTENERS COMMON TO REPAIR, FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED REPAIR PARTS IAW SRM 55-30-02, 55-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:SI, VERTICAL FIN STA 180.6, STR 7, ANGLE IS CRACKED AT FASTENER HOLE. REMOVED FASTENERS COMMON TO REPAIR, FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED REPAIR PARTS IAW SRM 55-30-02, 55-30-05.