What was found
ARM C581-1 WAS BINDING AND WEARING INTO SHAFT. THIS CAUSED THE LATERAL SPRING ASSEMBLY TO LOCK MOMENTARILY. EXCESSIVE WEAR ON THE SPRING SHAFT COULD AFFECT THE FLIGHT CONTROLS AND AIRCRAFT CONTROL ABILITY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ARM C581-1 WAS BINDING AND WEARING INTO SHAFT. THIS CAUSED THE LATERAL SPRING ASSEMBLY TO LOCK MOMENTARILY. EXCESSIVE WEAR ON THE SPRING SHAFT COULD AFFECT THE FLIGHT CONTROLS AND AIRCRAFT CONTROL ABILITY.