As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON CLIMB-OUT 12-15 DEGREES NOSE UP AND 220 KNOTS, GOT A HARD KICK TO THE RIGHT (ABOUT SIX DEGREE HEADING CHANGE). RUDDER POSITION INDICATORS SPLIT, CREW REPORTED LOWER RUDDER TO THE RIGHT. AIRCRAFT HAD PREVIOUS REPORTS OF YAW DAMPER PROBLEMS. FOUND W323-006-22 OPEN AT SM 1. REPAIRED OPEN WIRE AND ACCOMPLISHED YAW DAMPER COUPLER TEST.