As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) NR 1 ENGINE IFSD AND ATB OUT OH HI LO. METAL IN TAIL PIPE AND BULGED HP T CASE, INDICATIVE OF A 1ST STAGE HPT BLADE FAILURE. THE ENGINE HAD 3480 CYCLES SINCE REPAIR. ENGINE INDUCTED AT MFG FOR REPAIR. FURTHER DETAIL WILL BE SUBMITTED UPON DISSASSEMBLY OF ENGINE.