As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE SECOND STAGE EXHAUST STATOR HAD A BLADE BURNED THROUGH, CAUSE WAS TRACED TO BAD FUEL FLOW FROM FUEL NOZZLES THAT WERE POSSIBLY MAGNITIZED BY STARTER MAGNETIC FIELD. TESTING AND REPAIRS TO PARTS WERE CONDUCTED BY NORTH TEXAS TURBINES.