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 FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED AT STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-030. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.