As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CENTRAL/AILERON CONTROL: SLIGHT TWITCH OR LOOSE IN YOKE POSITION TO THE RIGHT. SLIGHT LAG IN CONTROL RESPONSE ON INITIAL ROLL INPUT. PILOT CONTROL YOKE FASTENERS AT THE CONTROL COLUMN TUBE FOUND LOOSE. BOLTS SECURED WITH LOCKTITE. AILERON CABLE TENSIONS WERE FOUND WITHIN LIMITS.