As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A "C-CHECK, MX FOUND A HALF CRADLE FROM THE RT OTBD WING FRONT SPAR TO FUSELAGE ATTACHMENT POINT. THE HALF OF CRADLE HAD FALLEN OUT OF THE ASSY. ON REMOVAL OF HARDWARE IT WAS NOTED THAT THE BARREL NUT WAS ALSO CRACKED. ALL HARDWARE REPLACED IN THE RT OTBD SPAR ATTACHMENT FITTING. REMOVED HARDWARE, RETURNED TO MFG FOR ANALYSIS.