What was found
HYDRAULIC SYSTEM FAILURE DURING CRUISE, ALT LANDING GEAR EXTENSION REQUIRED, DIVERTED TO (SVMI/CCS). FOUND DEFECTED HYD HOSE NR 3 ENGINE DRIVEN PUMP, LOWER HOSE ASSY. REPLACED HOSE WITH SERVICEABLE HOSE IAW MD-11 MM 20-40-01, PERFORMED LEAK CHECK IAW MM 71-00-06, NO LEAKS, SERVICED NR 3 HYD SYSTEM IAW MM 12-13-02, AIRCRAFT RETURNED TO SERVICE.