As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON FINAL APPROACH, NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED AND FLIGHT CREW CONFIRMED HYD NR 2 SYS QTY INDICATOR DOWN TO ZERO. ACFT LANDED WITHOUT FURTHER INCIDENT. INITIAL INSPECTION REVEALED THAT THE HYD FLUID LEAK ORIGINATED FROM THE LT MLG DOOR SEQUENCE SOLENOID VALVE. THE VALVE CASING WAS FOUND PARTIALLY SPLIT. THE LT MLG DOOR SEQUENCE SOLENOID VALVE WAS REPLACED, LEAK CHECKED AND TESTED SERVICEABLE. THE ACFT RETURNED IN SERVICE.