What was found
NO CONTROL INPUT EVEN WHEN CONTROL COLUMN WAS MOVED AFT. REMOVED SCREW THAT WAS WEDGED BETWEEN ELEVATOR CONTROL TAB STOP AND INBOARD ATTACHED FITTING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NO CONTROL INPUT EVEN WHEN CONTROL COLUMN WAS MOVED AFT. REMOVED SCREW THAT WAS WEDGED BETWEEN ELEVATOR CONTROL TAB STOP AND INBOARD ATTACHED FITTING.