As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE EXPERIENCED AN INTERNAL HOT SECTION FAILURE RESULTING IN COMPLETE LOSS OF POWER AND FLAMEOUT. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO THE FAILURE. A ROUTINE HOT SECTION BORESCOPE INSPECTION HAD BEEN PERFORMED. 10.2 HOURS PRIOR TO FAILURE. THIS ENGINE IS 340.6 HOURS FROM SCHEDULED 4000 HOUR OVERHAUL. PRELIMIARY INSPECTION REVEALED COMPRESSOR TURBINES BLADES FAILURE IS PROBABLE GAUGE. (K)