As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT CARGO SYSTEM FWD FLOOR ANCHOR HAS GOUGES, PITTING AND SURFACE CORRODED AROUND 3 ATTACH POINTS AND NUT PLATES HAVE CORROSION. REMOVED CORROSION AND GOUGES IAW CPM ORIGINAL MATERIAL THICKNESS IS .063 AND .040 MATL LOSS AT AREA OF .063 IS .005 WITHIN LIMITS IAW SRM MAT LOSS AREA .040 IS .014 FOUND OUT OF LIMITS. FABED REPAIR PART IAW SRM.