A method for forming an aircraft component, the method comprising: forming an inner portion of the aircraft component; forming a combined outer layer of the aircraft component using extrusion of an elastomeric material; and wherein forming the combined outer layer of the aircraft component further comprises: extruding a single sheet of elastomeric material; cutting the single sheet of elastomeric material into multiple outer layers (358,360,362); stacking the multiple outer layers (358,360,362) together; forming a desired thickness of the combined outer layer by repeating the extruding, cutting, and stacking steps; and coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component by a fastener, wherein the fastener extends through each of the multiple outer layers (358,360,362) and a portion of the inner portion, wherein coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component includes applying an adhesive between each of the multiple outer layers (358,360,362) to form the combined outer layer, and includes applying the adhesive between the combined outer layer and the inner portion. forming an inner portion of the aircraft component; forming a combined outer layer of the aircraft component using extrusion of an elastomeric material; and wherein forming the combined outer layer of the aircraft component further comprises: extruding a single sheet of elastomeric material; cutting the single sheet of elastomeric material into multiple outer layers (358,360,362); stacking the multiple outer layers (358,360,362) together; forming a desired thickness of the combined outer layer by repeating the extruding, cutting, and stacking steps; and coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component by a fastener, wherein the fastener extends through each of the multiple outer layers (358,360,362) and a portion of the inner portion, wherein coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component includes applying an adhesive between each of the multiple outer layers (358,360,362) to form the combined outer layer, and includes applying the adhesive between the combined outer layer and the inner portion. extruding a single sheet of elastomeric material; cutting the single sheet of elastomeric material into multiple outer layers (358,360,362); stacking the multiple outer layers (358,360,362) together; forming a desired thickness of the combined outer layer by repeating the extruding, cutting, and stacking steps; and coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component by a fastener, wherein the fastener extends through each of the multiple outer layers (358,360,362) and a portion of the inner portion, wherein coupling the multiple outer layers (358,360,362) of the aircraft component to the inner portion of the aircraft component includes applying an adhesive between each of the multiple outer layers (358,360,362) to form the combined outer layer, and includes applying the adhesive between the combined outer layer and the inner portion.