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 OUTBOARD SUPPORT AT B.S. 312-344; L.B.L. 66; W.L. 208.1. / REMOVED CORROSION FROM FED O/B SCUFF PLATE SUPPORT BS312-344; LBL66 WL208.1; ORIGINAL THICKNESS IS .050'; MAX MAT REMOVED IS MORE THAN 30% IN AN AREA OF 7' X 1'; FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 53-10-15-0I-1; SRM 53-10-15-1A-1 SRM 51-40-02-0G-0 AND DWG# 141A8110. 84632U;12MAR20.