As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK 0.045". OUT OF LIMITS. FABRICATED ANGLE ON T19/1450803. INSTALLED ANGLE IAW SRM 51-31-01 VOL I. REPAIRED BEAM IAW SRM 53-00-01 VOL II FIG 9. MAJOR REPAIR.