As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE ON T/O LOST POWER FROM 111.5 PERCENT TO 92.1 PERCENT ENGINE FAIL LIGHT CAME ON ABORTED T/O DUE TO LOSS OF N1 POWER. INSPECTED NR 2 ENGINE FOUND 14TH STAGE HIGH PRESSURE DUCT RUPTURED. REMOVED AND REPLACED PER MM 75-20 PERFORMED HIGH POWER RUN PER JRH, OPS CHECKED NORMAL.