As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C1 VERTICAL FIN, RT SIDE AFT OF ISOLATION STRIP HAS SKIN BULGING AND FASTENERS PULLING. REMOVED FASTENERS FOR ACCESS IAW SRM 51-01-21. NO CORROSION NOTED ON A REA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00, AND 51-01-21.