As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT CARGO FLOOR PANEL 1535X HAS CORROSION ON EDGES OF THE UPPER SURFACE AS MARKED. REMOVED CORROSION ON FLOOR PANEL 1535X IAW SRM 53-30-53 FIG 101. ORIGINAL THICKNESS IS 080 ENDING THICKNESS IS 076 MATERIAL LOSS IS 004 AND FOUND TO BE WITHIN LIMITS. (K)