As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) INTERMITTENT HYDRAULIC LEAK AROUND LINES AND FITTINGS IN THE NOSEWHEEL AREA WAS TRACED TO A LOOSE NUT THAT SECURES THE TEE FITTING TO THE HYDRAULIC SELECTOR VALVE. THE HYDRAULIC FLUID HAD SATURATED ALL THE INSULATION IN THE PEDESTAL AREA AND SOME OF THE CARPET. PART TC: 122.