As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON ROLLOUT F/O RT RUDDER PEDAL WENT FULL FORWARD. CAPT SIDE NORMAL, THEN ON TAXI IN CAPT SIDE WENT FULL FORWARD BUT OPPOSITE OF F/O'S. F/O'S LT SIDE FULL FWD/CAPT RT SIDE FWD. ACCESSED AVIONICS COMPT & INSPECTED RUDDER PEDAL TORQUE TUBE. FOUND BROKEN IN HALF ON PILOTS SIDE. ACCOMPLISHED WC EO 9-2720-7-5000, PART 4.