As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD CARGO COMPARTMENT FLOOR PANEL 120AF HAS CORROSION AROND THE OUTSIDE EDGES / REMOVED AND EVALUATED CORROSION ON PANEL 120AF ORIGINAL MATERIAL THICKNESS .071' LOSS OF .004' WITH .067' REMAINING. BLEND FOUND TO BE OUT OF LIMITS DUE TO LENGTH OF BLEND OVER 20' PER SRM 53-00-53-1A-1. FABRICATED REPLACEMENT PANEL 120AF PART #453A1610-14 PER DWG 453A1610 REV C