As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE. (SM). UPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE WAS REPAIRED PER SRM 52-11-04-201-009-A01.