항공기 엔진 감항기준에 대한 비교분석 = Comparative Study on Airworthiness Standards for Aircraft Engines

다국어 초록 (Multilingual 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.

참고문헌 (Reference)

1 이강이, "항공기 엔진제어시스템 인증기술 개발" 한국항공우주학회 33 (33): 104-109, 2005

2 홍덕곤, "국내 항공인증과 미국 인증체계의 비교" 한국항공우주학회 36 (36): 298-305, 2008

3 FAA, "Technical Implementation Procedures for Airworthiness and Environmental Certification"

4 Yongwun Jung, "Study on the Qualification Criteria for Aircraft Turbine Engine" 2367-2373, 2012

5 Kang-Yi Lee, "Safety Analysis for Turbine Case Cooling System of Turbofan Engine" Pusan National University 2012

6 Baisong Chen, "Reliability Analysis Method of an Aircraft Engine FADEC System" 289-292, 2009

7 Federal Aviation Administration, "Order 8110. 4C : Type Certification" 5 : 2011

8 Ministry of Land, Infrastructure and Transport, "KAS Part 33 : Airworthiness Standard for Aircraft Engines" 2013

9 Yongmin Jun, "Introduction to the Software Planning Phase for an Aero Engine according to RTCA DO-178C" 248-251, 2013

10 Federal Aviation Administration, "FAR Part 33 : Airworthiness Standard; Aircraft Engines" 33-33, 2012

11 European Aviation Safety Agency, "Certification Specification for Engines" 2010

12 Cosimo J, "Certification Issues for Electrical and/or Electronic Engine Controls" 15-24, 1987

13 Federal Aviation Administration, "AC 33-2C : General Type Certification Guideline for Turbine Engines" 2013