As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
APPROX 110 KTS LEFT ENG FAILURE WITH SEVERE DAMAGE. EGT 565, FF0, OIL PRESS 1. ENGINE SHUTDOWN, ABORTED T-O, BRAKE TEMP NORMAL, NORMAL STOP, NO OTHER INDICATIONS. RETURN TO BLOCKS. ENGINE WAS REMOVED DUE TO METAL IN TAILPIPE. FAILURE ORIGINATED AT HIGH PRESSURE TURBINE STAGE 1 BLADE FRACTURED JUST ABOVE THE PLATFORM. THERE WAS EVIDENCE OF STRESS CORROSION CRACKING. SB PW4G-112-72-240 AND -245 HAD NOT BEEN INCORPORATED.