As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT OVERWING FILL PORT HAS EVIDENCE OF CORROSION CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01-1A FIG 102 DETAIL 1. REV 125 ALLOWABLE MINIMUM REMAINING THICKNESS = 0.240" ACTUAL REMAINING THICKNESS = 0.145" REPAIR CARRIED OUT IAW EA F-5730-T0343997 P1 AND SRM 57-20-01-2R REPAIR 7 REV 125.