As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT FILLET FORMER AT STA 851 HAS CORROSION AROUND SCREW HOLES AT LOWER END. REPLACED LT FILLET FORMER "ITEM-10 ANGLE" AT STA 851 THAT WAS CORRODED BEYOND LIMITS NOMINAL .050" LOSS=.023 REMAINING .027" IAW SRM 51-41-02 0G, 53-20-71 0I-1 AND DWG 5971058.