Abstract: It is an object of the present disclosure to provide an interior member for an aircraft, a manufacturing method of the member and a replacement method of the member in which replacement cost can be reduced. An interior member for an aircraft according to the present disclosure includes a substrate, a decorative layer that covers the surface of the substrate, and an adhesive layer that adheres to the decorative layer to the substrate, and the decorative layer is peelably pasted to the surface of the substrate via the adhesive layer in a range that meets a required adhesive strength and that does not affect the substrate.

Abstract: An aircraft design apparatus calculates aircraft specifications, which are aircraft specifications, based on a plurality of design parameters required to design an aircraft; judges whether or not the calculated aircraft specifications meet constraints that indicate the aircraft feasibility and that are set in advance and given optimizing conditions for optimizing the aircraft; changes the design parameters so that the calculated aircraft specifications meet the constraints and also meet the optimizing conditions; and executes iterative processing in which the aircraft specifications are repeatedly calculated based on the changed design parameters. By doing so, with the aircraft design apparatus, it is possible to achieve a more optimal aircraft design and it is also possible to reduce the time and effort required to design an aircraft.