As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TAB (S/N S0328) WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER.