As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLAP ACTUATOR ROD END SEPARATED FROM ACTUATOR ASSEMBLY RESULTING IN LOSS OF FLAP OPERATION DURING FLIGHT. IT IS LIKELY THE JAMB NUT RETAINING THE ROD END WAS NOT PROPERLY TORQUED AND THE THE ROD END UNSCREWED FROM THE ACTUATOR MOTOR. IT IS UNKNOWN IF ANY FIELD SERVICE TO THE SYSTEM AFTER AIRCRAFT DELIVERY. THE DISCREPANCY WAS REPORTED TO CIRRUS FIELD SERVICE PER CASE NUMBER 465147.