As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF ROLLER TRAY AT FRAME 32, FOUND HEAVY CORROSION ON TOP OF FLANGE. CHECKED DIMENSIONS L 5.0", W 1.5" NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REPAIRED UPPER FLANGE BY CUTTING & SPLICING IAW SRM 53-10-15 FIG 207. FABRICATED FLANGE ON T16 1198513 & SPLICE ON T16 1198512. CLASSIFIED AS MAJOR CAT A REPAIR.