As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE AT FS 150 AND STRINGER 9AL AT THE AS DOOR STRUT LWR MOUNT UPPER AFT INNER NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-063. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR