What was found
INSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.