As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON FUSELAGE FRAME LOWER FLANGE AT X547.0, BETWEEN STR 31S AND STR 32S. CORROSION ON FUSELAGE FRAME LOWER FLANGE AT X54.70 BETWEEN STR 31S AND STR 32S WAS FOUND TO BE BEYOND LIMITS AS PER SRM 53-00-00 REPAIR 9 REV 16. PERFORMED A PERMANENT REPAIR IAW SRM 53-00-00 REPAIR 18 REV 16. SEE AWS AND NDT REPORTS TWO21960-10 AND TWO22097-3 FOR DETAILS. NO CRACKS FOUND.