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Comparative Study on Airworthiness Standards for Aircraft Engines

항공기 엔진 감항기준에 대한 비교분석

  • Lee, Kang-Yi (Aviation Certification Division, Korea Institute of Aviation Safety Technology) ;
  • Kim, Kitae (Power Systems R&D Center, Samsung Techwin Co. Ltd.) ;
  • Chung, Ha-Girl (Airworthiness Division, Ministry of Land, Infrastructure and Transport) ;
  • Roh, Tae Seong (Dept. of Aerospace Engineering, Inha University)
  • 이강이 (항공안전기술원 항공인증본부 인증기획실) ;
  • 김기태 (삼성테크윈(주) 파워시스템연구소) ;
  • 정하걸 (국토교통부 항공정책실 항공기술과) ;
  • 노태성 (인하대학교 항공우주공학과)
  • Received : 2015.03.07
  • Accepted : 2015.06.10
  • Published : 2015.06.30

Abstract

An aircraft engine is considered as the most important element among aircraft systems. Thus type certificate is required for an aircraft engine to ensure its safety under appropriate airworthiness standard. U.S. FAR Part 33 or European CS-E is widely adopted as an airworthiness standard for aircraft engines, and other representative countries of the world established own airworthiness standards under their regulations. In this paper, we compared differences of the requirements between FAR Part 33 and CS-E, and proposed the rulemaking items to harmonize Korean Airworthiness Standard for Aircraft Engines with worldwide standards and to contribute to growth of aviation industry.

Keywords

References

  1. Federal Aviation Administration, "FAR Part 33: Airworthiness Standard; Aircraft Engines", Amendment 33-33, Sep. 2012.
  2. European Aviation Safety Agency, "CS-E: "Certification Specification for Engines, Amendment 3, Dec. 2010.
  3. Ministry of Land, Infrastructure and Transport, "KAS Part 33: Airworthiness Standard for Aircraft Engines", Notice 2013-629, Oct. 2013.
  4. Deok-Kon Hong, Kwanjung Yee, "Comparison of Airworthiness Certification System between Korea and U.S.", Journal of KSAS, Vol. 36, No. 3, pp. 298-305, Mar. 2008.
  5. Yongwun Jung, Jaehwan Kim, "Study on the Qualification Criteria for Aircraft Turbine Engine", KSAS Fall Conference, pp. 2367-2373, Nov. 2012.
  6. Federal Aviation Administration, "Order 8110.4C: Type Certification", Change 5, Dec. 2011.
  7. Federal Aviation Administration, "AC 33-2C: General Type Certification Guideline for Turbine Engines", Jun. 2013.
  8. FAA and EASA, "Technical Implementation Procedures for Airworthiness and Environmental Certification", Revision 3, Apr. 2013.
  9. Cosimo J. Bosco, "Certification Issues for Electrical and/or Electronic Engine Controls", SAE Conference, pp. 15-24, Oct. 1987.
  10. Kang-Yi Lee, Sang-Ho Han, Sang-Joon Lee, Kui-Soon Kim, "A Study on Certification of Electrical Engine Controls", Journal of KSAS, Vol. 33, No. 1, pp. 104-109, Jan. 2005.
  11. Yongmin Jun, "Introduction to the Software Planning Phase for an Aero Engine according to RTCA DO-178C", KSAS Fall Conference, pp. 248-251, Nov. 2013.
  12. Baisong Chen, Ailian Wang, "Reliability Analysis Method of an Aircraft Engine FADEC System", International Conference on RMS, pp. 289-292, Jul. 2009.
  13. Kang-Yi Lee, "Safety Analysis for Turbine Case Cooling System of Turbofan Engine", Ph.D. thesis, Pusan National University, Aug. 2012.