Tun Lwin, JaeWoo Lee, Sangho Kim and Hyojin Lee
International Journal of Aeronautical and Space Sicences, vol. 13, no. 4, pp.435-445, 2012

Abstract : In this paper, a design process is established by integrating aviation safety requirements for the development of general aviation aircraft. An Airworthiness–Design Integration System, which integrates certification requirements with the entire design/analysis process, is developed and presented. For the proposed system, KAS 23/FAR 23/AC 23/CS 23 certification regulations are analyzed to determine design constraints and system compliance checks and to construct an ER&G (Engineering Requirement and Guide) and a Design-Certification Related Table (DCRT). Furthermore, through building a DB (Data Base), the management of design and certification related resources for developing a FAR 23 class aircraft are made. Certification tools and resources are also efficiently managed by the DB. The connection between the certification requirements and the detailed design process is proposed in this system. Tracking of this proposed method is validated by configuring a USE CASE and a system. The Airworthiness–Design Integration system will be constructed based on the system’s design plan, certification system, and usage scenarios.

Keyword : Airworthiness, Database, Integrated System, Design Process