As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOSS OF NR 2 HYDRAULIC QUANTITY AND PRESSURE AFTER TAKEOFF (LEAK FROM NOSE GEAR AREA). REPLACED NOSE GEAR DRAG STRUT ACTUATOR HOSE ASSEMBLY. INSPECTED ENGINE DRIVEN PUMP PER MM PROCEDURE 05-50-33. NO CONTAMINATION FOUND IN CASE DRAIN FILTER. GROUND RAN AIRCRAFT IAW PROCEDURE. RUNUP AND LEAK CHECK GOOD.