As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD CARGO LOWER BAFFLE CORRODED ON LOWER SURFACE OF UPPER FLANGE. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL THICKNESS: 0.020" MATERIAL LOSS 0.004" REMAINING THICKNESS 0.016", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD CARGO BAFFLE IAW SRM 51-40-02 AND BAC DWG # 143A7505 REV-.