As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FAULT - FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE). 1.I.A.W AMM 53-13-01-424-005 REV.141 INSTALLED THE SCUFF PLATE. 2.ACCOMPLISHED THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST I.A.W AMM 05-51-24-782-001 REV.141, NO LEAKAGE WAS FOUND. 3.JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEWED