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항공기 시스템 설계와 안전성평가에 운영경험 반영 사례 연구

A Study on the Application of Operational Experience in the Stage of Aircraft System Design and Safety Assessment

  • 구민성 (주) 대한항공 정비품질부)
  • 투고 : 2014.05.20
  • 심사 : 2014.06.18
  • 발행 : 2014.06.30

초록

Airworthiness authorities specify the technical standards of airworthiness that propose minimum requirement of the commercial transport category and apply the rules in the certification process to ensure the safety of the aircraft. The Federal Aviation Administration and other national airworthiness authorities define the fatal accident risk levels for the safety assessment of the aircraft system and establish standard procedures to apply both qualitative and quantitative analysis techniques. However, an accident or incident may occur by the combination of various factors, although the aircraft is designed in accordance with the strict standards and approval by the Airworthiness Authorities. There are some key factors, such as human error, unpredictable complex system failures, degradation of the components reliability, improper maintenance task and intervals. Risk can be reduced by reflecting aircraft operational experience with similar types of aircraft in the process of aircraft development and safety assessment. Result of the root cause analysis for the Airbus A300-600 incident in which the aircraft engine reverser was deployed in the air have been introduced to reflect the design of system and related components. Also, this paper suggests to create a big-database in order to provide a feed-back to the FAR Part 25 transport category design and safety assessment of the operational experience.

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참고문헌

  1. 국토교통부 훈령 제 40호, 항공기 형식 증명 지침, 2013.
  2. FAR AC 23-130-1E, "System Safety Analysis and Assessment for Part 23 Airplanes", 2011.
  3. FAR AC 25-1309-1A, "System Design Analysis", 1988.
  4. SAE ARP4761, "Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment " 1996.
  5. 구민성, "지속 감항성 유지프로그램 운영 경험의 항공기 설계와 인증 단계 적용", 한국항공운항학회지, 제 21권 제3호, 2013, pp. 9-14.
  6. A300-600 Maintenance Manual ATA 78-31 Revision 59, 2013.
  7. FAA System Safety Handbook, Chapter 7: Integrated System Hazard Analysis, 2000.