What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 294.5, STRINGER 14. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 294.5, STRINGER 14. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.