As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER RATIO EICAS ON TAKEOFF ROLL AFTER V1..FOLLOWED FIM, L HYD PSI NORMAL. PERFORMED RUDDER RATIO CHANGER MODULE BITE PROCEDURE. REF FIM 27-21-00-815-804 AND FIM 27-09-00-815-814. OPS CHECK NORMAL. NO FAULTS NOTED. ALSO PERFORMED GENERAL VISION INSPECTION OF RUDDER RATIO ACTUATOR CONECTORS AND HYDRAULIC LINES. NO DEFECTS NOTED.