The invention relates to a
braking system (1, 1', 1'') for an aircraft, comprising an electrically actuated device (2, 2', 2E, 2I) having a bi-stable operating mode and a progressive operating mode, and at least one control device (OCF n 1, OCF n2) capable of generating a park command (Co / f), which activates the bi-stable operating mode of the electrically actuated device (2, 2', 2E, 2I), and a progressive braking command (Cp1, Cp1', Cp2, Cp2'), characterised in that the
system comprises at least one inhibition
system configured to inhibit an operation of the electrically actuated device (2, 2', 2E, 2I) according to at least one operating state of a normal
braking system, the at least one progressive braking command (Cp1, Cp2) being configured to activate the progressive operating mode of the electrically actuated device (2, 2', 2E, 2I) according to the at least one inhibition
system.