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 ROUNTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CUTOUT IS CRACKED AT THE IB LWR CORNER OF THE COUTOUT, CRACK IS .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-020. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.