• Title/Summary/Keyword: 감항

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A Study to the Technical Criteria of Propulsion System for the Military Airworthiness Certification (군용항공기 감항인증을 위한 추진체 기술기준에 대한 고찰)

  • Jeon, Jingark;Kim, Sunglae
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.205-206
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    • 2017
  • This is a study on the propulsion criteria for airworthiness certification of the military aircraft. This treatise described the introduction of the airworthiness certification system, the features and difference between the military and commercial aircraft, the introduction of the standard airworthiness certification, the important technical criteria, and the several application instances of the criteria.

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Utilization Aircraft Airworthiness Information for Aviation Safety Oversight (항공기 감항성 유지 기술정보의 항공안전감독 활용방안)

  • An, Ju-Hyeon;Choe, Byeong-Cheol;Choe, Yeong-Jae
    • 한국항공운항학회:학술대회논문집
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    • 2016.05a
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    • pp.125-130
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    • 2016
  • 최근 국내에서 개발한 KC-100 항공기의 형식증명 및 제작증명이 완료됨에 따라 우리나라도 항공기 제작/설계국 반열에 오르게 되었고, KC-100 개발을 계기로 국내 개발 항공기의 해외 수출을 대비한 제작/설계국으로서의 감항성 유지 체계 및 시스템 구축이 필요로 하게 되었다. 본 연구에서는 ICAO에서 제시하는 국가 유형 별 감항성 유지 업무의 책임 및 해외 항공선진국의 감항성 유지체계와 우리나라의 지속감항업무 수행현황을 비교분석하여 국내 감항성 유지 체계 및 항공기 고장보고 항목에 대한 개선 방안을 제시하였고 항공안전정보 네트워크를 구축하여 지속감항체계에서 획득한 항공 안전기술정보를 안전감독에 활용하기위한 방안을 연구하였다.

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Target Level of Safety Analysis in Airworthiness Certification for Military UAV (군용무인기의 감항인증 목표안전수준 분석)

  • Lee, Narae;Jeon, Byung-Il;Chang, Young-Keun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.10
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    • pp.840-848
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    • 2013
  • Airworthiness certification of military aircraft is a government's certification that it must have airworthiness and ability to demonstrate its requested function and performance. NATO released STANAG-4671 to establish the minimum airworthiness requirements for UAVs between 150kg and 20,000kg MTOW in 2009. Up to now, there are no clear airworthiness certification criteria and guideline for small UAV which is less than 150kg. STANAG-4671 is used for military UAV airworthiness certification in Korea as Other Airworthiness Certification Criteria. However, since STANAG-4671 requires the same Target Level of Safety without regard to MTOW, excessive Target Level of Safety or design requirements could be applied to relatively small-medium UAV. In this paper, classification and criteria of airworthiness certification for military UAV were investigated and a Target Level of Safety was analyzed based on MTOW using ground victim criteria.

A Study for the Airworthiness Certification Criteria and Compliance Related to the Flight Control Law (비행제어법칙 감항인증 기준 설정 및 입증 연구)

  • Koh, Gi Ok;Ko, Joon Soo;An, Young Gab
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.7
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    • pp.569-576
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    • 2013
  • The Airworthiness Certification from the government has an increasingly important role due to the dramatic growth of military aircraft development industry. It is a mandatory process of qualifying the flight safety within the aircraft's operational boundaries throughout its life cycle. The introduction of airworthiness certification has resulted in development paradigm shift from one requirement for one consumer need to the common requirement for many needs. This research paper provide the refinement of airworthiness certification criteria related to the flight control law and the verification methods which comply with its criteria.

A Study on the Improvement of Airworthiness Certification (항공기 감항증명제도에 대한 고찰)

  • Hwang, Ho-Won;Hong, Seung-Taek
    • The Korean Journal of Air & Space Law and Policy
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    • v.26 no.1
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    • pp.31-63
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    • 2011
  • Since Korea has invested only on developing an aircraft, it is true that Korea has neglected detailed standards and procedures about certification activities including essential safety procedures. Most developed countries have implemented mandatory airworthiness system by legislating it for operational safety of aircraft based on ICAO Annex 8, and the U.S. Department of Defense and the FAA's Airworthiness system have been adapted it to the realities of their circumstance. Therefore, Airworthiness system that can guarantee the safety of the aircraft at international level is necessary to enhance flight safety and to create export opportunities of an aircraft as a country which can develop an aircraft by itself To achieve this, a study on the improvement of aircraft airworthiness was carried out by analyzing the problem of domestic airworthiness system and by reflecting international best practices on the establishment of a system for improved Airworthiness.

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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 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.

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.

Study on Effective Airworthiness Certification Methods and Airworthiness Certification Standards for Aerial Launch Platform using Large Civil Aircraft (대형 민간항공기를 활용한 공중발사 플랫폼의 효율적 감항인증방안 및 감항인증기준 연구)

  • Oh, Yeon-Kyeong;Kim, Suho;Yoo, Min Young;Choi, Seong Hwan;Seo, Hyun Woo
    • Journal of Aerospace System Engineering
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    • v.16 no.4
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    • pp.28-34
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    • 2022
  • In 2021, Virgin Orbit converted a 747-400 aircraft into an air launch platform, and successfully launched it twice in February and July. Compared to the existing ground launch, interest in the air launch is increasing due to its great utility, such as its independence from the launch location or weather, cost reducing factor, shorter launch preparation time, and its benefit pursuant to altitude and speed. Additionally, as small satellites have similar performance to mid/large satellites in the past due to the miniaturization and precision of electronic equipment, small satellite launches are expected to dominate in the future. In this paper, institutional certification methods such as domestic, overseas, civilian and military airworthiness certification regulations/procedures are reviewed to ensure flight safety of aerial projectiles using large domestic civil aircraft, and applicable civil and military airworthiness certification technology standards are reviewed and analyzed. Additionally, we will review and suggest effective airworthiness certification application plans that reflect the reality, and present airworthiness certification standards (draft) for aerial launch vehicles, by analyzing applicable airworthiness certification technical standards when remodeling aerial launch vehicles.

Study on New Airworthiness Requirements of Powerplant System for the Small Airplane (소형 비행기 동력장치에 관한 신규 인증요건 분석)

  • Lee, Eunsuk;Lee, Seung geun;Lee, Kang-Yi
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.207-212
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    • 2017
  • Korean civil airworthiness requirements of powerplant system are regulated on KAS Part 23 and Part 33. These are equivalent to FAR Part 23, Part 33 of FAA and CS-23, CS-E of EASA. FAA and EASA rewrites entire airworthiness requirements for the small airplane. It changed current 'prescriptive regulation' into 'performance-based regulation' which makes the object of safety performance. Powerplant requirements are also changed extensively by these concept revolution. In accordance with reorganization, we studied new powerplant system requirements of FAR Part 23 and proposed ideal direction to rewrite of Korean Airworthiness Standard rewrite.

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