As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FSD; SCUFF PLATE AFT SIDE IS CRACKED 3 INCHES.<[01] FUSION WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM53-10-15-2R-2. PT INSPECTED WELDED AREA PER SOPM 20-20-02. NO CRACKS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF SCUFF PLATE AS NECESSARY TO GET A SURFACE ROUGHNESS OF 125RA OR SMOOTHER. REFERRED TO 51-20-13;[02] VERIFIED TASK CARD COMPLETE.