As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) PILOT REPORTED TOT OF 813C FOR 6 SECONDS. INSPECTION FOUND THE TURBINE FIRST STAGE NOZZLE CRACKED AND ERODED ON 19 VANES. THE COMBUSTION LINER 980916051 WAS ALSO CRACKED. THE OVERTEMP IS NOT CONSIDERED THE SOURCE OF EITHER THE TURBINE OR COMBUSTION LINER DAMAGE. PART TC: 932.