As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) NR 1 ENGINE EXPERIENCED CONTINUOUS HIGH TEMPERATURES. INVESTIGATION FOUND THE FOLLOWING DEFECTS: HOLE BURNED IN INLET GUIDE VANE. FIRST STAGE NOZZLE BURNED WITH A PIECE MISSING. T5 HARNESS THERMOCOUPLE END BURNED OFF. POWER TURBINE VANE RING CRACKED BETWEEN ADJACENT BLADES.