As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) HYDRAULIC LEAK FROM #1 NACELLE. LINE BETWEEN #2 HYDRAULIC SYSTEMS SPOILER LIFT DUMP VALVES FOUND LEAKING AT 3000 PSI. BENCH CHECK FOUND LINE START TO WEEP AT 400 PSI AND JUST STARTS TO DIP AT 1000 PSI. STEADY STREAM AT 3000 PSI. LINE REPLACED.