As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT REJECTED TAKEOFF AT 60 KNOTS, DURING TAKEOFF RUN THE STEERING CONTROL WAS INOPERATIVE. AT PLATFORM MAINTENANCE PERSONNEL PERFORMED OPERATIONAL TEST OF THE STEERING CONTROL AND RUDDER MOVEMENT RESULTED CORRECT, SO AIRPLANE WAS SENT TO THE HANGAR AND DURING THE OVERNIGHT CHECK THE CENTERING SPRING OF PEDAL STEERING OVERRIDE MECHANISM WAS FOUND BROKEN, SO IT WAS REPLACED IAW MM 32-51-00 AND TESTED IAW MM 32-52-00, ALL CORRECT.