A landing gear for an aircraft, having mounting means fitted to the fuselage of the aircraft; at least one wheel; and at least one supporting arm having a first end portion connected to the mounting means, and a second end portion opposite the first end portion, and to which the wheel is suspended. The first end portion of the supporting arm has a seating portion fitted in rotary manner to a pin connected to the mounting means and extending crosswise to the supporting arm; and an electrically controlled actuator is fitted to the seating portion, and is activated selectively to rotate the supporting arm, about the pin, between a first and second operating position defining a stowed in-flight configuration and a lowered landing configuration of the landing gear respectively.
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