What was found
RUD LIMIT FAULT CAME ON DURING DESCENT. REPLACED NR 1 RUDDER LIMITER LINEAR ACTUATOR AND SPRING FOR NR 1 ACTUATOR ROD ENDS IAW MM 27-25-03. OPERATIONAL CHECK OK IAW MM 27-21-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RUD LIMIT FAULT CAME ON DURING DESCENT. REPLACED NR 1 RUDDER LIMITER LINEAR ACTUATOR AND SPRING FOR NR 1 ACTUATOR ROD ENDS IAW MM 27-25-03. OPERATIONAL CHECK OK IAW MM 27-21-00.