As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 3 ENGINE FAILURE LIGHT ON DURING TAKEOFF ROLL. SEVERE VIBRATION AT IDLE N1 19 PERCENT, N2 50 PERCENT. REPLACED ENGINE. THE T-2 BLADE FAILURE WAS DUE TO IMPACT DAMAGE, LEADING TO HIGH CYCLE FATIGUE CRACK AND RESULTANT FAILURE. SEVERE DOWNSTREAM DAMAGE IN THE N1 TURBINE AND EXHAUST CASE.