Metallic, integral structural component

connected Metal structural member, in particular for aircraft, wherein the structural component (1) comprises a skin panel (2) and at least one of the skin panel (2) arranged stiffening element (3) and the stiffening element (3) into an integral structure to the skin panel (2) is characterized in that the skin panel (2) and / or aufgedickte portions (4) of the skin panel (2) with at least one recess (5; 50) are provided, so that the thickness of the skin panel (2) and / or the thickened is reduced; portion (4) in the region of the recess (50 5).