Patent ID: 8413929

Claim:
An aircraft assembly comprising: a skin having an inside, an outer surface side and fiber reinforced resin as a main structure; a structural member supporting the skin from the inside; a fastener coupling the skin and the structural member; a conductive foil disposed on the outer surface side of the skin; a conductive resin layer containing conductive powder disposed above the conductive foil; an insulating washer having a surface coated with an insulating material; an insulating spacer interposed between the structural member and the insulating washer; and a first glass-fiber reinforced plastic between the conductive foil and the conductive resin layer and a second glass-fiber reinforced plastic between the fiber reinforced resin and the structural member, wherein the fastener has a tip portion protruding inside from the structural member, the tip portion is disposed, via the insulating washer, in a fixture so as to secure the skin and the structural member.