▎ 摘　　要

NOVELTY - The component (2) has a heatable component section (4) that includes a layer structure comprising an inner base structure. A heating layer (26) has a carbon allotropes embedded in a matrix material. A first group (12) of consecutive layers comprising an anode layer (16), a first insulating layer (18), and an cathode layer (20) having an electroactive coating. The first group of layers are arranged between the inner base structure (10) and the heating layer. A protective layer (28) is arranged outside the heating layer. The first group of layers constitute a structural battery, and the anode layer and the cathode layer are electrically connected with the heating layer. USE - Structural component for aircraft (claimed) e.g. commercial aircraft. ADVANTAGE - The structural component is simple to manufacture and does not significantly add weight to the structural component, into which it is integrated. The current collector layers may comprise graphene, which comprises advantageous mechanical properties as well as high thermal conductivity, which offers the use of graphene at least for one of the collector layers that is opposite to the inner base structure. DETAILED DESCRIPTION - INDEPENDENT CLAIMS are included for the following: 1. a method for producing a structural component; and 2. an aircraft. DESCRIPTION OF DRAWING(S) - The drawing shows a sectional view of the structural component. Structural component (2) Heatable component section (4) Inner base structure (10) First group (12) Anode layer (16) First insulating layer (18) Cathdde layer (20) Heating layer (26) Protective layer (28)