As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AT CRUISE, AN UNUSUAL NOISE AND VIBRATION WAS HEARD AND FELT FOLLOWED BY #2 HYDRAULIC PUMP FAIL LIGHT. #1 SYSTEM PRESSURE WAS NORMAL. ALTHOUGH NOT REQUIRED, #2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. POST FLIGHT INSPECTION DETERMINED THAT #2 HYDRAULIC PUMP HAD FAILED.