An aircraft refuelling equipment for an aircraft, the equipment comprising: - a pipework comprising a fuel supply line connected to a plurality of tank supply lines; - fuel tanks (14, 15, 16) connected to tank supply lines of the pipework and adapted to be refuelled through the fuel supply line; - first valves (24, 25, 26) arranged in said pipework and adapted to allow each fuel tank (14, 15, 16) to be disconnected from the fuel supply line; - at least one captor allowing, for each of said first valves (24, 25, 26), a first valve flow parameter to be estimated, said at least one captor being arranged within the pipework for providing at least one signal indicative of a pressure or a flow rate, said at least one captor comprising at least one pressure captor for sensing a pressure within the pipework and for providing at least one signal indicative of a pressure; and characterized in that each first valve (24, 25, 26) comprise a valve body with a plurality of adjustable positions between a full open position and a closed position, and in that it further comprises:- at least one actuator associated with each of said first valves (24, 25, 26) in a respective actuator-first valve assembly and allowing adjustment of an opening of the associated first valve at a defined position of the valve body chosen among the full open position, the closed position and the plurality of adjustable positions therebetween; - an electronic control unit connected to the respective actuator-first valve assemblies, the electronic control unit comprising: a receiving module for receiving position data from said first valves (24, 25, 26) and for estimating the respective first valve flow parameters, using the pressure data and the position data, and a control module adapted to regulate the opening of the first valves, using respective first valve flow parameter data. - a pipework comprising a fuel supply line connected to a plurality of tank supply lines; - fuel tanks (14, 15, 16) connected to tank supply lines of the pipework and adapted to be refuelled through the fuel supply line; - first valves (24, 25, 26) arranged in said pipework and adapted to allow each fuel tank (14, 15, 16) to be disconnected from the fuel supply line; - at least one captor allowing, for each of said first valves (24, 25, 26), a first valve flow parameter to be estimated, said at least one captor being arranged within the pipework for providing at least one signal indicative of a pressure or a flow rate, said at least one captor comprising at least one pressure captor for sensing a pressure within the pipework and for providing at least one signal indicative of a pressure; and - an electronic control unit connected to the respective actuator-first valve assemblies, the electronic control unit comprising: a receiving module for receiving position data from said first valves (24, 25, 26) and for estimating the respective first valve flow parameters, using the pressure data and the position data, and a control module adapted to regulate the opening of the first valves, using respective first valve flow parameter data. a receiving module for receiving position data from said first valves (24, 25, 26) and for estimating the respective first valve flow parameters, using the pressure data and the position data, and a control module adapted to regulate the opening of the first valves, using respective first valve flow parameter data.