As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT CARGO FLOOR PANEL 1534X HAS CORROSION AROUND FASTENER HOLES ON FORWARD F/S 727 TO 732, LBL 20 TO RBL 20 ON ITS UPPER SURFACE. BLENDED AREA AT AFT CARGO FLOOR PANEL 1534X AROUND FASTENER HOLES ON FORWARD END UPPER SURFACE. ORIGINAL THICKNESS IS 080, BLENDED AREA IS L=42 BY W=2 MAX MATERIAL LOSS IS 003 AND IS WITHIN LIMITS IAW SRM 53-30-53, FIG 101. (K)