As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME BS 1661 STRINGER 25L TO 25R CORRODED ON AFT LOWER FLANGE. R & R FRAME IAW DWG 146N1032 & SRM 51-40-02 DUE TO CORROSION FOUND WITH MATERIAL LOSS CLEANUP OF .047 OF ORIGINAL .063 OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. MAJOR REPAIR.