• Title/Summary/Keyword: 감항당국

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Study on Foreign Military Authority Recognition Questionsets (MARQs) (해외 군당국의 감항인정의제 고찰)

  • Roh, Jin Chul;Goo, Bon Wook;Ko, Joon Soo
    • Journal of Aerospace System Engineering
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    • v.10 no.4
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    • pp.105-114
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    • 2016
  • The world is currently confronted with regional conflicts among nations that seek to protect their territory. The associated counter-terrorism activities and international business flows can be increased through airworthiness-recognition tasks that are related to aircraft exports, dispatch troops, and overseas bases. It is important to establish airworthiness-recognition processes between foreign military authorities to minimize the potential for sovereign national positions and responsibilities. For this study, the military airworthiness recognition between recognition partners was surveyed to secure flight safety for the development and operation of aircrafts. The analysis of the U.S. and European Military Authority Recognition Questionsets (MARQs) in this paper introduces the rules, inspection capabilities, production process, and certification of the airworthiness authority. The regulatory activities, which are required by the Korea Military Airworthiness Authority (MAA) with respect to foreign MAAs, can be reduced by the implementation of the MARQ.

항공기 안전성 시험평가에 대한 고찰(상)

  • Ryu, Jeong-Ju
    • Aerospace Industry
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    • v.47
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    • pp.14-21
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    • 1997
  • 국내에서 생산된 항공기 및 관련 부품을 운용하기 위해서는 항공기 및 그것을 구성하고 있는 모든 부품의 제반 특성이 감항기준을 만족시킨다는 것이 입증되어 감함당국에 의해 승인되어야 한다. 항공기와 관련 부품의 승인은 법에 의한 감항 적합성 평가 절차를 따라야 하며, 이러한 평가 절차를 거쳐서 승인된 항공기는 비로소 감항성을 인정받아 운항이 허락되고, 또한 승인된 관련 부품은 항공기에 사용되어 최종적으로 고부가가치의 경쟁력을 얻을 수 있다.

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Study on Introduction of Partial Delegation System for Aircraft Certification (항공기인증의 일부 위임제도 도입방안에 대한 연구)

  • Sanghyuk Park;Gyeongchul Kang;Minkyu Kang;Sunmi Jin;Yunseo Lee;Yonghee Kim;Seunghyeon Lee;Sungjin Kim
    • Journal of Aerospace System Engineering
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    • v.17 no.1
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    • pp.1-9
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    • 2023
  • Recently, aerospace industries in South Korea are expected to continue to grow due to UAM. Accordingly, certification services for aircraft are expected to increase. As a way to cope with the increase of certification work, one could consider a delegation system that can limitedly delegate the unique role of airworthiness authorities. In this paper, we reviewed regulations of FAA's individual delegation (DER, DAR, DMIR, etc.), the organizational delegation system (ODA), and the EASA's organizational delegation system (DOA, POA). We also reviewed regulations and actual status of delegation system in South Korea. On the basis of these, considering circumstances of aerospace industries in South Korea, we presented a method to introduce certification delegation system gradually and to improve domestic certification regulation.

Japanese Aircraft Certification System and Status of Bilateral Aviation Safety Agreement (일본의 항공기인증제도 및 항공안전협정(BASA) 체결 동향)

  • Park, Guen-Young;Jin, Young-Kwon;Lee, Jong-Hee
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.2
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    • pp.124-135
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    • 2010
  • The Japanese and U.S. governments has signed a Bilateral Aviation Safety Agrement and associated implementation procedures for airworthiness on April 27, 2009 to mutually accept the airworthiness approvals for aircraft and parts that the other country issue. This bilateral agreements do not relieve the Civil Aviation Authority(CAA) of its statutory responsibilities for certification. However, they provide an alternative means for the CAA to make its findings, recognizing the competency of another authority to conduct certification functions in a manner comparable to, and on behalf of, the CAA. In this way, the bilateral agreements contribute to ensuring aviation safety as well as reducing the burden imposed on the aviation industries without compromising safety. This paper is to discuss recent status of Bilateral Aviation Safety Agreement and associated Japanese Aircraft Certification System.

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A Study on Restricted Category Type Certification Procedure of Surion Derivatives Rotorcraft (수리온파생형 회전익항공기 민간 제한형식증명 획득 절차에 관한 연구)

  • Kim, Yonghee;Park, Sanghyuk;Lee, Seunghyun;Kim, Sungjin;Kang, Youngho
    • Journal of Aerospace System Engineering
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    • v.14 no.1
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    • pp.54-61
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    • 2020
  • For operating military aircraft, military certificate of airworthiness (MCA) must be obtained from military authority. Among procedures of general airworthiness certification, there is a military type certification process that aircraft design complies with military airworthiness certification criteria. The Surion is the first military rotorcraft which has obtained military type certificate, production validation and airworthiness certificate in Korea, and the Surion derivatives for special mission are being operated for government services. Based on Aviation Safety Act, in order to operate the Surion derivatives (military aircraft) for special purpose (such as emergency patient transportation and firefighting), the issuance of special airworthiness certificates was needed from civil airworthiness authority, and the restricted category type certification (RTC) is one of design approvals for special airworthiness certification to be streamlined. This study discussed the procedures for acquiring RTC for special purpose operation of the Surion derivatives classified as military derived aircraft, and suggested procedural ideas to improve Korean RTC system.

Current trends of Military Air'craft Airworthiness certification using Civil Aircraft Certification Basis (민간 항공기 인증기술을 이용한 군용항공기 감항인증 효율화 기술동향)

  • Choi, Seok;Kim, Sung-Chan
    • Current Industrial and Technological Trends in Aerospace
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    • v.6 no.2
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    • pp.154-160
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    • 2008
  • There are typically two categories of Flight Test Programs- commercial and military. Commercial flight testing is conducted to certify that aircraft meets all applicable safety and performance requirements of government certifying agency. Military programs differs from commercial in that the government contract with the aircraft manufacturer to design and build an aircraft to meet specific mission capabilities. The final phase of military aircraft flight test is the Operational Test(OT). OT is conducted by a government-only test team with the dictate to certify that the aircraft is suitable and effective to carry out the intended mission. This paper presents the current trends of military aircraft airworthiness certification using civil aircraft certification practices.

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Comparison of Airworthiness Certification System between Korea and U.S. (국내 항공인증과 미국 인증체계의 비교)

  • Hong, Deok-Kon;Yee, Kwan-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.3
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    • pp.298-305
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    • 2008
  • From design to serial production, aircraft should go thorough complicated certification procedure from airworthiness authority such as Type Certificate, Production Certificate and Certificate of Airworthiness. On the other hand, aircraft components are mandated to receive Technical Standard Order Approval and Production Manufacture Approval before commercial use. As domestic aircraft and LRUs are currently under development, Bilateral Aviation Safety Agreement is promoted for the purpose of increasing aviation safety as well as foreign export. This paper describes the basic aircraft certification procedure and compares the difference in the certification system of US and Korea. Thorough this, it is attempted to suggest a requirements for establishing international certification system.

A Study on the Application of Operational Experience in the Stage of Aircraft System Design and Safety Assessment (항공기 시스템 설계와 안전성평가에 운영경험 반영 사례 연구)

  • Koo, Min-Sung
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.22 no.2
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    • pp.34-39
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    • 2014
  • 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.

A Study on the Risk-based Model for Validation of Civil Aircraft (민간항공기 형식증명승인을 위한 위험기반 모델 개발 동향)

  • Baek, Unryul;Lee, Eunhee;Kim, Jinhee;Lee, Kyungchul
    • Journal of Aerospace System Engineering
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    • v.12 no.4
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    • pp.1-8
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    • 2018
  • The state of registry issues a type certificate validation (TCV) based on the satisfactory evidence that the product (aircraft, engine, and propeller) is in compliance with the appropriate airworthiness requirements. The Korean government performs an evaluation to determine whether the product complies with Korean airworthiness standards for issuing TCV according to the Korean aviation safety law. Recently, the Validation Principles Working Group (VPWG) has developed a risk-based model for validation of civil aeronautical products. Also, VPWG proposed to incorporate this validation model into the corresponding ICAO Standards and Recommended Practices and guidance material. In this paper, we have reviewed the validation model and discussed improvements in the validation process.

Analyses of Hover Lift Efficiency, Disc Loading and Required Battery Specific Energy for Various eVTOL Types (다양한 eVTOL 유형별 호버 효율, 회전판 하중 및 필요 배터리 비에너지 분석)

  • Kim, Dong-Hee;Jang, Han-Yong;Hwang, Ho-Yon
    • Journal of Advanced Navigation Technology
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    • v.25 no.3
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    • pp.203-210
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    • 2021
  • In many metropolitan cities around the world, ground and underground transportation networks are saturated due to urbanization. In addition, regulations on carbon emissions to prevent global warming are becoming stricter, and eVTOL, which will be operating in complex cities, is gaining popularity as the next generation of eco-friendly transportation. In this study, the hover lift efficiency and disc loading of eVTOLs for each type were calculated by classifying eVTOLs into following types: multicopter, lift+cruise, and vectored thrust. In addition, using the aerodynamic analysis programs OpenVSP, Fluent and Javaprop, the specific battery energy required for the smooth operation of eVTOL, which will be realized in the near future, was calculated and analyzed base on reports published by Uber and airworthiness authorities of each country.