As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING APPLICATION OF THRUST POWER, TAKEOFF WAS ABORTED TO THE HEAVY STICK PRESSURES. TAKEOFF WAS ABORTED AT 140 KNOTS AND PERFORMED WITH NO INCIDENTS. REPLACED STABILIZER TRIM BRAKE MECHANISM, MAIN STABILIZER TRIM ACTUATOR, AND R27 NOSE UP STABILIZER TRIM RELAY. PERFORMED OPERATIONAL CHECK OF STABILIZER SYSTEM. CHECKED OK.