As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 3 ENGINE FAILED AT 800 FEET ON TAKEOFF. EGT PEGGED, RPM DECAY, OIL QUANTITY DROPPED TO ONE GALLON AND OIL PRESSURE DROPPED TO ZERO. RETURNED TO DEN. T-2 BLADE FAILURE DUE TO NOTCH BREAK-OUT AND RESULTANT CYCLE FATIGUE. THE BLADE FAILURE WAS THE CAUSE OF THE DISC BLADE FIR TREE POST-FAILURE. EXTENSIVE DOWN STREAM DAMAGE IN THE N1 TURBINE AND EXHAUST CASE. UNDER INVESTIGATION.