As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 500 AND STRINGERS 4L & 5L CRACKED AT THE STRUT MOUNT UPPER IB NUTPLATE AREA, .65" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-027. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.