As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE PREPARING TO REFUEL THE AIRCRAFT, PILOT NOTED A LARGE QUANTITY OF HYDRAULIC FLUID ON THE RT ENGINE/THRUST REVERSER AREA. THE AFT HYDRAULIC HOSE CONNECTING THE TAIL ROTOR TO THE PYLON HAD BURST AT APPROXIMATELY MID LENGTH. (THIS IS THE AREA WHERE THE HOSE MAKES A 90 DEGREES TURN.) THE CREW HAD NO INDICATION OF THE PROBLEM DURING LANDING AND TAXI.