As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER CHANGE WITH NO SUBSEQUENT RESPONSE TO THROTTLE LEVEL INPUT. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT-OF-DEPATURE. SUBSEQUENT INSPECTION REVEALED A DAMAGED HYDROMECHANICAL FUEL CONTROL/FUEL PUMP ASSEMBLY.