As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HAD A "CATCH" IN THE ROLL CONTROL TURNING TO THE RIGHT, CONTROLS HEAVIER AFTER OR BEYOND THE CATCH. INSPECTED AILERON ROLL SPOILER SYSTEM BETWEEN CONTROL YOKES AND PCU'S. NO DEFECT NOTED. PERFORMED AILERON AND AILERON/SPOILER DISCONNECT CHECK IAW 750 MM, 27-10-00. ALL CHECKS WERE GOOD.