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 ROUTINE INSPECTION, MX FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 509.5 BETWEEN STRINGERS 3L AND 4L INNER FACE OF FRAME AT 2 FASTNER HOLES, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-041 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.