As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ROLLING AILERON BEYOND 3 UNITS ON CONTROL COLUMN BINDING FELT. WHEEL VERY SLOW TO RETURN TO NORMAL. NOT AS STIFF WITH INPUT TO THE LEFT. WHEEL WOULD NOT RETURN TO NEUTRAL ON ITS OWN. FOUND INBOARD DROOP QUADRANT SIEZED. (CROSS SHAFT) ON INSPECTION OF REMOVED UNIT , FOUND BEARING SIEZED AND BUSHING MIGRATED. UNIT P/N 251T1602-6 UNIT REPLACED AND AILERON SYSTEM NORMAL.