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 A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 456 AND STRINGER 3L & 4L AT THE GAS STRUCT MOUNT UPPER IB NUTPLATE AREA, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-028. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.