As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** ON FORWARD ENTRY DOOR MOP SILL AT B.S. 312-355; L.B.L. 62; W.L. 208.1. / REMOVED CORROSION FROM FED MOPSILL BS312-355 LBL62 WL208.1; ORIGINAL THICKNESS IS 0.090' MAX MAT REMOVED 10' X 2' X .015' REMAINING THICKNESS .075' FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED FED MOPSILL IAW SRM 53-10-15-01-1; SRM 53-10-15-1A-1; SRM 51-40-02 AND DWG# 141A8110