As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE CARGO DOOR AFT FUSELAGE FRAME OF FS 509 AT THE GAS STRUT MOUNT BETWEEN STRINGERS 4L & 5L, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-061. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR.