What was found
AFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAMPER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER TAKEOFF BOTH STABILIZER TRIM FAULTED, BOTH YAW DAMPER AND NR 2 RUDDER SYSTEM FAULTED. STABILIZER TRIM AND YAW DAMPER WERE RESET. LANDED WITHOUT INCIDENT. REPLACED RUDDER LIMITER MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION.