As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C5 CHECK - STRINGER 31R IS CORRODED AT CROSSRACE ATTACH POINT AND AT STRINGER SPLICE AFT SIDE OF FRAME AT STA 18.250. REMOVED CORROSION IAW SRM 51-21-00-00-02, FOUND TO BE IN LIMITS IAW SRM 53-20-03. MIN MATERIAL THICKNESS .080 SRM NOMINAL .080 NO MATERIAL LOSS NOTED. APPLIED ALODINE, PRIMER AND PAINT TO AREA IAW SRM 51-21-10, 51-25-10 AND 51-25-25.