As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT CABIN L/H I/B CREASEBEAM UPPER SURFACE HAS CORROSION STA 988 LBL 46-48 WL 208. MRKD<[01] REMOVED CORROSION STA 988 LBL 46-48; ORIGINAL MATERIAL THICKNESS IS 0.080?; MATERIAL LOSS IS 0.010?; MAX ALLOWED IS 0.008?. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1;[02] ALL WORK AND PART REPLACEMENT WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00TPQGP;[03] VERIFIED ALL WORK ACCOMPLISHED ON TASK CARD TTG8Q00TPQGP.