As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FLANGE RADIUS ON THE FRAME AT FS 451 & STRINGER 10R .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-029. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.