An aircraft structural component, comprising: - a panel element made of a fibre reinforced composite material and being provided with an opening extending through the panel element from a first surface to a second surface of the panel element, - a reinforcing element made of a fibre reinforced composite material and being provided with an opening extending through the reinforcing element from a first surface to a second surface of the reinforcing element, the opening extending through the reinforcing element being aligned with the opening extending through the panel element, - a bushing extending through the opening provided in the panel element and adapted to receive an attachment device for attaching a load to the aircraft structural component, characterised in that the bushing extends through the opening provided in the reinforcing element, and by - a connecting element which connects the reinforcing element to the panel element in a region of the panel element adjacent to the opening extending through the panel element, the connecting element having a first section disposed on the second surface of the panel element which faces the first surface of the reinforcing element and comprising a first plurality of hook and loop elements and a second section disposed on the first surface of the reinforcing element which faces the second surface of the panel element and comprising a second plurality of hook and loop elements, wherein the first and the second plurality of hook and loop elements (50a, 50b) of the first and the second section (48a, 48b) of the connecting element are adapted to interact with each other so as to produce a hook and loop connection between the panel element and the reinforcing element. - a panel element made of a fibre reinforced composite material and being provided with an opening extending through the panel element from a first surface to a second surface of the panel element, - a reinforcing element made of a fibre reinforced composite material and being provided with an opening extending through the reinforcing element from a first surface to a second surface of the reinforcing element, the opening extending through the reinforcing element being aligned with the opening extending through the panel element, - a bushing extending through the opening provided in the panel element and adapted to receive an attachment device for attaching a load to the aircraft structural component, characterised in that the bushing extends through the opening provided in the reinforcing element, and by - a connecting element which connects the reinforcing element to the panel element in a region of the panel element adjacent to the opening extending through the panel element, the connecting element having a first section disposed on the second surface of the panel element which faces the first surface of the reinforcing element and comprising a first plurality of hook and loop elements and a second section disposed on the first surface of the reinforcing element which faces the second surface of the panel element and comprising a second plurality of hook and loop elements, wherein the first and the second plurality of hook and loop elements (50a, 50b) of the first and the second section (48a, 48b) of the connecting element are adapted to interact with each other so as to produce a hook and loop connection between the panel element and the reinforcing element.