As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF ROLL, THE FIRST OFFICER'S AIRSPEED INDICATION NEVER EXCEEDED 45 KNOTS. ABORTED TAKEOFF AT 105 KNOTS. REPLACED THE LEFT NR 1 AIR DATA MODULE AND NR 2 AIR DATA INERTIAL REFERENCE UNIT. LEAK AND FUNCTIONAL CHECK OF ALTITUDE, AIRSPEED AND AIR DATA SYSTEM OK. AFS AND LAND III TEST OK. AIRCRAFT RETURNED TO SERVICE.