What was found
(CAN) AIRCRAFT WAS CLIMBING THROUGH 8000 FEET WHEN NR 1 A SYSTEM HYDRAULIC PUMP FAILED, FOLLOWED SHORTLY BY THE NR 2 PUMP FAILURE. QUANTITY WAS DECREASING RAPIDLY. AIRCRAFT RETURNED. INSPECTION FOUND A SYSTEM FLEX LINE, LOCATED FORWARD OF L/H GEAR LEAKING. REPLACED LINE, TOPPED UP HYDRAULIC FLUID, RUN UP ENGINES SYSTEMS CHECKED SERVICEABLE.