As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING CLIMB AS THE GEAR WAS SELECTED UP, HYDRAULIC PRESSURE BEGAN TO FLUCTUATE AND THE QUANTITY IN THE NR 2 SYSTEM BEGAN TO DROP. AFTER THE AIRCRAFT LANDED, MAINTENANCE FOUND THE NOSE GEAR DRAG STRUT ACTUATOR HYDRAULIC SUPPLY HOSE RUPTURED.