Fluidic valve

A fluid valve for a hydraulic circuit in an item of aircraft equipment, comprising:

• a hollow valve body comprising one inlet, two outlets and a communication channel with an external pressure source;
• an electric solenoid actuator located in the hollow of the hollow valve body and including a movable ferromagnetic pilot;
• a valve member movable inside the valve body to at least partially block a passage between said inlet and one of the two outlets, said valve member at least partially defining a first and a second cavity located on either side of said valve member in the hollow of valve body, and
• a fixed limiter in said communication channel such that a displacement of said movable pilot causes a variation in pressure in one of said first and second cavities to produce a force for moving said valve member to vary a flow rate of a fluid between the inlet and the two outlets,
• wherein at least a section of said member contains a ferromagnetic material, and that said electric solenoid actuator is configured to exert a magnetic displacement force on said ferromagnetic section of the valve member.