As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT EXTERNAL POWER DOOR LOWER HINGE AREA, STA 235.8 - 243.7, S20R. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03672. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR PER ECRA 5330-03672, PART 3 WITHIN 12 MONTHS.