As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AFTER TAKEOFF DURING CLIMB AND FLAPS RETRACTED, ENGINE DRIVEN HYDRUALIC FAIL LIGHT ILLUMINATED. HYDRAULIC FLUID LEVEL INDICATED EMPTY. FLAPS EXTENDED USING D.C. PUMP AND LANDING GEAR EXTENDED USING EMERGENCY FREE FALL PROCEDURES. MAINTENANCE INVESTIGATION REVEALED THAT AN ELBOW FITTING HAD BROKEN ON THE RH MAIN LANDING GEAR UPLINE. FITTING REPLACED.