As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT FLOOR PANEL 120AF HAS CORROSION / EVALUATED CORROSION ON FWD PIT FLOOR PNL 120AF FOUND TO BE OUT OF LIMITS AS ACCUMULATED DAMAGE IS OVER 20' IAW SRM 53-00-53-1A-1 FIG 103; VERIFIED MAT IAW AIPC 25-52-10-17; SRM 53-30-53-01-1; AND BOEING DWG 452A1610 REV F; FABRICATED PNL 120AF IAW BOEING DWG 453A1610 REV F; TREATED AND PRIMED PNL IAW AMM 51-21-41-370-803; AND AMM 51-21-72-370-804 PN 453A 1610-14 ATAG A3941