As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF ROLL, AT APPROXIMATELY 1.73 EPR, THE RT ENGINE N2 REACHED 103.1 FOR FIVE SECONDS. TAKEOFF ABORTED AT APPROX 90 TO 95 KNOTS. R & R HP 3 & HP 3 BLEED VALVES IAW AMM 75-32-04. R & R HP 3 & HP 2 SOLENOIDS IAW AMM 75-32-05. ACCOMPLISHED HIGH POWER ASSURANCE TEST & TEST NR 3 IAW AMM 71-00-00. SYS CHECKED NORMAL.