What was found
(CAN) IN FLIGHT AFTER THE LANDING GEAR WAS SELECTED DOWN THE NR 2 ENGINE HYD PUMP CAUTION LIGHT, CAME ON. WITH LOSS OF HYD PRESSURE AND QTY OF THE HYD SYSTEM NR 2. DURING POST FLIGHT INSPECTION WE FOUND SEQUENCE SOLENOID VALVE WAS BROKEN, 3 OF 4 THE COUPLING BOLTS WERE SHEARED. ALL ASSOCIATED FILTERS CHECKED NO CONTAMINATION. THE EDP WORKED FOR MORE THAN 34 MINUTES WITHOUT FLUID, NO EDP CASE DISCOLORATION FOUND BUT REPLACED. THE VALVE REPLACED. THE ACFT HAS BEEN RETURNED TO SERVICE.