• 한국항공우주학회지
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• 제42권12호
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• pp.1073-1079
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• 2014

항공기 부품은 새로 개발되는 항공기의 설계를 구성하는 일부일 뿐만 아니라, 형식증명을 받은 항공기의 감항성을 유지하는데 중요한 역할을 한다. 미국은 1965년부터 부품제작자승인 제도를 수립 시행하여 운용 중인 항공기의 감항성 유지는 물론 전 세계의 항공기 부품 시장의 확대에 기여해 왔다. 본 논문에서는 미국의 부품제작자승인, 유럽의 유럽부품승인, 그리고 우리나라의 부품등제작자증명 제도를 상호 비교 분석함으로써 국제적 안전성 기준에 부합하고 부품산업 발전에 기여할 수 있도록 개선사항을 제시하였다.

• 항공우주시스템공학회지
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• 제2권4호
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• pp.13-18
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• 2008

Airworthiness is a term used to dictate whether an aircraft is worthy of safe flight. It is illegal in most countries to fly an aircraft without first obtaining an airworthiness certificate from the responsible government agency. For developing an aircraft, the design modifications and upgrades are considered a high financial risk proposal for most Program Managers(PMs). However Design-to-Certification Integrated System can be a great help in achieving a good design solution in an acceptable amount of time and flight test. In this paper, we present a method to construct database for the Development of Design-to-Certification Integrated System. By using this database, the human designer could manage and find the regulation and requirements related with his concern effectively.

• 항공우주시스템공학회지
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• 제6권2호
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• pp.7-12
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• 2012

De-icing system is essential for any aircraft to fly in icing conditions. So there are two kinds of aircraft-those that are certificated for flight in icing conditions and those that are not. Icing certification involves a rigorous testing program, and relatively few light aircraft carry this approval. From a legal perspective, aircraft that do not have all required ice protection equipment installed and functional are prohibited from venturing into an area where icing conditions are known. There are a few kinds of de-icing system. It is necessary to review the systems in point of aircraft certification considering the operational and safety issues.

• 항공우주시스템공학회지
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• 제3권1호
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• pp.30-35
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• 2009

This study is on the establishment process of Certification Plan of KPP small aircraft development, domestic BASA(Bilateral Aviation Safety Agreement) shadow certification project. For the development of certification plan incorporations process understanding applicable regulations, selection of certification basis, definition of means of compliance and establishment of compliance checklist. On the basis of this process, we develop type certification procedure suitable for domestic small aircraft.

• 항공우주시스템공학회지
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• 제9권3호
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• pp.47-58
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• 2015

An aircraft, its engine and propeller are certified in processes of design, production, and operation respectively. Type Certificate is issued if the aviation authority finds that the design of aircraft, engine, or propeller complies with applicable airworthiness standards and environmental standards. The ICAO (International Civil Aviation Organization) prescribes the international standards and recommended practices of type certification for the contracting states. The FAA (Federal Aviation Administration) and the EASA (European Aviation Safety Agency) established their regulations and procedures applicable to type certification. In this paper, we compared the differences among the ICAO, the FAA, and the EASA regulations, and on this comparison, we proposed the rulemaking items to improve type certification regulations in Korea.

• 항공우주시스템공학회지
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• 제1권3호
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• pp.21-25
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• 2007

This is a study on the establishment of airworthiness certification system fitted for korean military aircraft acquisition and export. Based on the investigation of US civil & military airworthiness system and analysis of the real state of domestic military aircraft acquisition, this paper offers some ideas that can be helpful to establish laws and organizations to certify airworthiness. Particularly this paper suggests that the best way to build airworthiness certification laws/guidelines and technical criteria, the optimal organizational structure which is decentralized by dividing administrative certification authority and technical research center.

• 한국항공운항학회지
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• 제21권1호
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• pp.57-61
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• 2013

In the present study, which is currently operating domestically and internationally, from the Technical Standards for Flight Safety of Light Sport Aircraft and certification system through a comparative analysis of the LSA Category Airworthiness Certifications documents. In particular, an aircraft type analysis of FAA certified S-LSA that the speed greater than 120 knots LSA manufactured without United States of America. Through the analysis, we presented a revised plan to activation of the domestic aviation leisure sports and the development of the Light Sport Aircraft industry in reality.

• 품질경영학회지
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• 제41권3호
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• pp.423-432
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• 2013

Purpose: A Study on the application of quality management system specification to production validation and audit in military airworthiness certification. Methods: Aircraft quality management system specification for quality assurance and production validation and audit requirements were examined to verify. Also, the system for domestic and foreign production certification were investigated. Results: Production validation and audit criteria for military aircraft by applying methods suggested Aircraft Certifications Systems Evaluation Program(ACSEP). ACSEP evaluation of the items, some items were complementary and not applied. Conclusion: As a way to ensure the safety of aircraft, confirm the correction of Production validation & audit criteria and rulemaking is necessary and how to manage for Critical Safety Item(CSI) is a need to improve.

• 항공우주시스템공학회지
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• 제3권1호
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• pp.17-22
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• 2009

For establishing new certification requirements for aircraft engines, Technical background of FAR Part33 amendments has reviewed and studied in this paper. The FAA is amending type certification standards for aircraft engines. These changes reflect current industry practices and harmonize FAA standards with those recently adopted by the European Aviation Safety Agency (EASA). These changes establish uniform standards for all engine control systems for aircraft engines certificated by both U.S. and European countries and will simplify airworthiness approvals for import and export.

• 항공우주시스템공학회지
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• 제1권2호
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• pp.1-5
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• 2007

This is a study on the effective and efficient way of airworthiness certification for Korean indigenously developed military aircrafts. Investigating the policy, process, and capability for military aircraft airworthiness certification in USA end Europe, the approach for Korean military aircraft airworthiness certification is recommended. Using FAR as basis for military airworthiness criteria is much more beneficial in initial stage of establishing airworthiness certification system. And all the available resources regardless of civil or military institutes need to be cooperated to accomplish required level of indigenous airworthiness certification capability.