As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 RADIAL ENGINE HYDRAULIC PUMP PRESSURE LINE INTERNAL TO THE FUSELAGE BEGAN LEAKING IN FLIGHT. UPON IDENTIFICATION OF THE LEAK, THE NR 2 ENGINE WAS SHUTDOWN AND AN IFE WAS DECLARED. LANDING WAS UNEVENTFUL. UPON INVESTIGATION OF THE LEAK, IT WAS DISCOVERED THAT THE LINE B-NUT FERRULE HAD CRACKED. THE LINE ASSEMBLY WAS R&R'D AND LEAK TESTED GOOD.