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 A/S DOOR FUSELAGE FRAME ANGLE AT FS 150.60 & STRINGER 9AL AT THE AS DOOR LWR MOUNTS, UPPER AFT ATTACH POINT, 2 CRACKS 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW. EO 11-1900-53-039 MATERIALS UTILIZED ARE INCLUDED IN THE EO.