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 INSPECTION MAINTENANCE FOUND A CRACK IN THE FUSELAGE FRAME CHANNEL AT FS 177.35 & STRINGER 13L IN THE FRAME FLANGE BEND RADIUS, .7 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-036. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.