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 SCUFF PLATE INBOARD SUPPORT AT B.S. 312-344; L.B.L. 64; W.L. 208.1. / REMOVED CORROSION FROM FED I/B SCUFF PLATE SUPPORT BS312-344 LBL64 WL208.1; ORIGINAL THICKNESS .080' MAX MAT REMOVED 5' X 1' X .010' REMAINING THICKNESS IS .070' FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 53-10-15-01-1; SRM 53-10-15-1A-1 AND DWG# 141A8112. 84632U; 12MAR20.