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 MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 456 & STRINGER 10R IS CRACKED AT THE LOWER RADIUS OF THE CUTOUT, .2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-045 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.