What was found
ENGINE #2 HYD PUMP FAILURE IN FLIGHT. DIVERTED. LANDING UNEVENTFUL. REPAIRED HYDRAULIC LEAK IN RIGHT WHEEL WELL. EDP PRESSURE LINE. NOTICED PITTING IN BULKHEAD FITTING IN WHERE LINE SEATS APPROX 20% OF THE WAY AROUND LOWER SIDE. REPLACED #2 ENGINE EDP PRESSURE RIGID LINE FORM NACELLE MID FRAME FLEX LINE CONNECTION TO AFT FIREWALL CONNECTION. REF MM TASK 29-00-00-400-802. PRESSURIZED LINE FROM EDP TO FILTER MANIFOLD WITH 3000 PSU FROM GHPU NO LEAKS NOTED. RETURNED TO SERVICE.