A pressure bulkhead for an aircraft fuselage comprising a sandwich structure, which defines a central axis and which extends between a circumferential edge area, which edge area is configured to be secured to the fuselage structure of an aircraft fuselage, wherein the sandwich structure comprises: an inner cover layer, for facing towards the pressure side and which extends transversely to the central axis, an outer cover layer, which extends opposite the inner cover layer and transversely to the central axis, and a core layer, which extends between the inner and outer cover layers (13, 17) and connects them, characterized in that between the inner and the outer cover layer (13, 17), in addition to the core layer, a support structure is provided, which is connected to the cover layers (13, 17) and which extends from the inner cover layer to the outer cover layer, the support structure comprises at least one layer which, viewed in a cross section parallel to the central axis, extends from a first section of the edge area to an opposite second section of the edge area, the layer is configured as an anchor layer, which extends transversely to the central axis, and the support structure comprises a plurality of pins, which extend between the anchor layer and the outer cover layer and between the anchor layer and the inner cover layer, and which are secured with a first end in the anchor layer and with an opposite second end in the outer cover layer, respectively in the inner cover layer. comprising a sandwich structure, which defines a central axis and which extends between a circumferential edge area, which edge area is configured to be secured to the fuselage structure of an aircraft fuselage, wherein the sandwich structure comprises: an inner cover layer, for facing towards the pressure side and which extends transversely to the central axis, an outer cover layer, which extends opposite the inner cover layer and transversely to the central axis, and a core layer, which extends between the inner and outer cover layers (13, 17) and connects them, an inner cover layer, for facing towards the pressure side and which extends transversely to the central axis, an outer cover layer, which extends opposite the inner cover layer and transversely to the central axis, and a core layer, which extends between the inner and outer cover layers (13, 17) and connects them, characterized in that between the inner and the outer cover layer (13, 17), in addition to the core layer, a support structure is provided, which is connected to the cover layers (13, 17) and which extends from the inner cover layer to the outer cover layer, the support structure comprises at least one layer which, viewed in a cross section parallel to the central axis, extends from a first section of the edge area to an opposite second section of the edge area, the layer is configured as an anchor layer, which extends transversely to the central axis, and the support structure comprises a plurality of pins, which extend between the anchor layer and the outer cover layer and between the anchor layer and the inner cover layer, and which are secured with a first end in the anchor layer and with an opposite second end in the outer cover layer, respectively in the inner cover layer.