As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - MAJOR REPAIR - Q1 CHECK - CRACK ON FORWARD ENTRY DOOR INNER SKIN AFT EDGE BETWEEN NR 5 AND NR 7 STOP FITTING ACCESS HOLES. REPAIRED FORWARD ENTRY DOOR INNER SKIN AFT EDGE BETWEEN NR 5 AND NR 7 STOP FITTING ACCESS HOLES IAW ENGINEERING AUTHORIZATION 102584.