Abstract: The present invention relates to an aircraft having at least one landing flap arranged at the wing of the aircraft and having at least one drive unit for actuating the landing flap, wherein the aircraft furthermore has at least one control unit which controls the aileron function of the aircraft, wherein the control unit is connected to the named drive unit or units for adjusting the landing flap(s) and is configured such that it carries out the aileron function of the aircraft in at least one flight mode only or also by the operation of the named drive unit(s) and thus by the adjustment of the landing flap(s).

Abstract: The invention relates to a servo valve, in particular a two-stage or multistage electrohydraulic servo valve, having a first stage which works as a pilot stage, and a second stage which works as a power stage, wherein the second stage has a valve block and a control slide valve sleeve arranged therein and having a jacket surface (18), wherein the jacket surface and/or another region of the control slide valve sleeve is preferably provided with at least one flow passage for transferring control flow and/or volume flow, and wherein a control slide valve is movably arranged in the control slide valve sleeve, wherein at least one of the flow passages is formed by a groove which is arranged in the surface of the control slide valve sleeve and which does not extend sectionally or overall in the peripheral direction of the control slide valve sleeve.