As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#1 AND #2 HYDRAULIC SYSTEMS FLUID LOSS. #2 RUDDER ISO VALVE CAUTION LIGHT ILLUMINATED. HYD PRESSURES NORMAL. ON LANDING NORMAL BRAKES FAILED. FOUND LEAK AT #3 BRAKE. #3 SHUTTLE VALVE FAILURE ALLOWED FLUID LOSS FROM BOTH HYD SYSTEMS. REPLACED #3 SHUTTLE VALVE.