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 AFT FUSELAGE FRAME CRACKED 1.5" IN LENGTH AT THE GAS STRUT MOUNT UPPER IB NUT PLATE, FS 509 BETWEEN STRINGERS 4L & 5L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-011. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.