As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AFTER T/O, THE PILOT NOTICED A LOSS OF POWER ON NR 2 ENGINE. SECURED THE ENGINE AND RETURNED TO THE POINT ORIGIN WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. PRELIMINARY INSPECTION REVEALED A POSSIBLE TURBINE BLADE FRACTURE WITH PROPELLER SEIZED AND HEAVY OIL LEAK.