As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT AFT PASSENGER DOOR SILL BEAM AT FR 66 UPPER FLANGE AND AROUND NUT PLATE HOLES. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-41-14 FIG 201 (REF NON ROUTINE 21/260). FOLLOW UP INSPECTION REQUIRED PER SRI 53-41-14-2-001-00. FIRST INSPECTION REQUIRED AFTER REPAIR EMBODIMENT AT 92731FC/208644FH, SUBSEQUENT INSPECTION AT INTERVAL-TBD AND INPECTION METHOD-TBD.