UÇAK PARÇA İMALAT SERTİFİKASYON YÖNETİMİ Bölüm 1 Sivil Havacılık Otoriteleri ve Kuruluşları TURKISH AIRLINES INC. AVIATION ACADEMY EASA APPROVAL: EASA.147.0015 JAA & TURKISH DGCA APPROVAL: TR.147.001
PROGRAM Bölüm 1 Sivil Havacılık Otoriteleri ve Kuruluşları Bölüm 2 Avrupa Sivil Havacılık Parça İmalat Yönetimi
Bölüm 1 Sivil Havacılık Otoriteleri ve Kuruluşları
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Definitions: Aircraft Large Aircraft Commercial Operation Maintenance Product Parts and Appliances Component Page 5 of 34
Sivil Havacılık Kuruluşları TCH STCH --------- Airbus Part 21 DOA DOE/DH -------- Airbus & Suppliers Part 21 POA POE ------------- Airbus & Suppliers JAR OPS EU OPS OM FOM & GOM ------------- THY Part M CAMO CAME MME ------------- THY Tech. Dir. Part 145 MO MOE ------------- THY Turkish Tech. Part 66/147 MTO MTOE ----------- THY Training Dir. FCL/OPS FTO / TRTO --------------- THY Flight Training Dir. FCL/OPS Medical Centers ------------------- GOP Hospital Page 6 of 34
International Civil Aviation Organisation (ICAO) Specialized agency of the United Nations Assembly with 190 contracting states A council with 36 delegates. Standard and Recommended Practices (SARP) Annexes to ICAO See web site http://www.icao.int/ Page 7 of 34
ICAO Chicago Convention: The Convention (Doc 7300) on 7 Dec. 1944 by 52 States. The latest revision: 9 (Doc7300/9) on 27 November 2007. Go to web site: http://www.icao.int/icaonet/dcs/7300.html 18 Annexes Annex 6 - Operation of Aircraft ICAO Annexes Page 8 of 34
Civil aviation authority of United States of America under DOT. FARs based on Title 14 (Aeronautics and Space) and Title 49 (Transportation) of USA CFR. List of Title 14 rules. No. 1-59 FAA / DOT Rules, Volume 1, Chapter 1 No. 60-139 FAA / DOT Rules, Volume 2, Chapter 1 No. 140-199 FAA / DOT Rules, Volume 3, Chapter 1 No. 200-399 Office of the Secretary, DOT(Aviation Proceedings), Volume 4, Chapter 2 No. 400-1199 Commercial Space Transportation, FAA Administration, DOT, Volume 4, Chapter 3, No. 1200-1299 National Aeronautics and Space Administration (NASA), Volume 5, Chapter 5, No. 1300-1399 Air Transportation System Stabilization, Volume 5, Chapter 6 CHAPTER I - FAA, DOT SUBCHAPTER C-- AIRCRAFT 25.1 to 25.1733 AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES... Similar numbering system to other NAA For more information see web site http://www.faa.gov Page 9 of 34
ECAC the widest grouping of Member States of any European organization dealing with civil aviation. 44 Member States including Albania, Armenia, Austria, Azerbaijan, Turkey, Ukraine, United Kingdom. Plenary Session triennially and more frequently, if required. Directors General of Civil Aviation at regular intervals to discuss and resolve policy issues. Some at Ministerial level JAA Board is currently an Associated Body of ECAC. ECAC based in Paris and its working languages are English and French. With 27 of its 42 Member States being also members of the European Union. Working relationship with ICAO Develop instruments enabling co-operation between EASA States and other non-easa ECAC States. Co-operate with European Commission, EASA, EUROCONTROL. Accident investigation group. ECAC SAFA program, but now it was transferred to EC. Page 10 of 34
Joint Aviation Authority (JAA) History: An associated body of ECAC Civil aviation regulatory authorities of some European and non-european States Developing and implementing common safety regulatory standards and procedures. Beginning in 1970 Originally its objectives to produce common certification codes for large aeroplanes and for engines. Needs of European Industry and particularly for products manufactured by international consortia (e.g. Airbus). Since 1987 its work has been extended. On 16th July 2008, EU-OPS1 requirements become applicable in the states of the EU and in the JAA member states which have concluded an association agreement with the European Community covering aviation safety regulation. Current Objectives and Funtions: Aviation Safety Co-operation with EASA International Co-operation (ECAC, ICAO & other regional bodies) Ensuring a forum to express the views of the non EASA JAA Member States to EASA; Assist the non EASA JAA Member States in their efforts to become EASA members or equivalent status; Further ensuring the role of JAA as a technically specialised body; Standardisation; For more information see web site: http://www.jaa.nl/introduction/introduction.html Page 11 of 34
European Aviation Safety Agency (EASA): The centrepiece of the EU s strategy for aviation safety. Developing common safety and environmental rules at the European level. Monitoring the implementation of standards through inspections in the States. Providing the necessary technical expertise, training and research. Working hand in hand with the national authorities which continue to carry out many operational tasks. Executive responsibilities in the area of type-certification Benefiting from common specifications, cost-efficient services and a single point of contact. Drafting aviation safety legislation and providing technical advice to the European Commission Inspections, training and standardisation programmes to ensure uniform implementation of European aviation safety legislation in all States; Approval of aircraft design organisations world-wide as and of production and maintenance organisations outside the EU; Authorization of third-country (non EU) operators; Coordination of the European Community programme SAFA (Safety Assessment of Foreign Aircraft) regarding the safety of foreign aircraft using Community airports; Data collection, analysis and research to improve aviation safety. In a few years, safety regulations regarding airports and air traffic management systems. Developing close working relationships with counterpart organisations across the world including the ICAO, the FAA and other civil aviation authorities of Canada, Brazil, Israel, China and Russia. Working arrangements between the Agency and these organisations are aimed at harmonising standards and promoting best practice in aviation safety world-wide. Page 12 of 34
Relationship between Authorities and Organisations Page 13 of 34
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Basic Regulations (European Commission (EC) Regulation 216 / 2008) Initial Regulation (EC) No 1592/2002 of 15 July 2002 Applicable to: Design, production, maintenance and operation of aeronautical products, parts and appliances, as well as personnel and organisations involved in the design, production, maintenance and operation Not applicable to: military, customs, police, or similar services. But Objective: the Member States shall undertake to ensure that such services have due regard as far as practicable to the objectives of this Regulation. to establish and maintain a high uniform level of civil aviation safety in Europe; and to assist EU Member States in fulfilling their obligations under the Chicago Convention, by providing a basis for a common interpretation and uniform implementation of its provisions, and by ensuring that its provisions are duly taken into account in this Regulation. Page 17 of 34
Implementing Rules on Design and Production (European Commission (EC) Regulation 1702 / 2003) Latest Revision EC No. 287/2008 regulation dated 28 March 2008 9 general rules, 5 Articles and 1 Annex (Part 21 and its appendices) Some amendments after the first issue, included in this document. Article 1 Scope and definitions : type-certificates, restricted type-certificates, supplemental type-certificates, changes to certificates; certificates of airworthiness, restricted certificates of airworthiness, permits to fly, authorised release certificates; repair design approvals; the showing of compliance with environmental protection requirements; noise certificates; airworthiness directives. the identification of products, parts and appliances; the certification of certain parts and appliances; the certification of design and production organisations; Article 2 Article 3 Article 4 Article 5 Products, parts and appliances certification Design Organisations Production Organisations Entry into force Annex PART 21 Appendices EASA Forms Page 18 of 34
Part 21 AMC & GM (EASA Director (ED) Decision 2003/1/RM) Acceptable Means of Compliance (AMC) : a means, but not the only means, by which a specification contained in an airworthiness code or a requirement in an implementing rule can be met. Guidance Material (GM): helps to illustrate the meaning of a specification or requirement. Example (for understanding coverage of BR, IR & AMC) Basic Regulation the essential requirements for airworthiness laid down in Annex I Implementing Rule 21A.3(b)(2) Failures, malfunctions and defects: Reporting to the Agency. Occurrence reports not later than 72 hours AMC 21A.3(b)(2) Reporting to the Agency by the fastest possible means (telephone, fax, email, telex, etc.) of whatever details are available initial report followed up by a full written report within 72 hours. Page 19 of 34
Certification Specifications (CS) Used in the text to the airworthiness codes and associated acceptable means of compliance developed by the Agency in accordance with Articles 13(b) and 14.2(a) of the Basic Regulation. Currently consulting phase on the contents of CSs with respect to IR Certification in co-operation with the JAA. Some completed CSs:: CS-22 CS-23 CS-25 CS-27 CS-29 CS-34 CS-36 CS-APU CS-AWO CS-E CSE-ETSO CS-Definitions CS-P CS-VLA CS-VLR AMC-20 Sailplanes and Powered Sailplane Normal, Utility, Aerobatic and Commuter Aeroplanes Large Aeroplanes Small Rotorcraft Large Rotorcraft Aircraft Engine Emissions and Fuel Venting Aircraft Noise Auxiliary Power Units All Weather Operations Engines European Technical Standard Orders Definitions and Abbreviations Propellers Very Light Aeroplanes Very Light Rotorcraft General Acceptable Means of Compliance for Airworthiness of Products, Parts and Appliances Page 20 of 34
Implementing Rules on Continuing Airworthiness (European Commission (EC) Regulation 2042 / 2003) The latest revision EC No 127/2010 of 05 February 2010 This Regulation has 8 general rules, 7 Articles and 4 Annexes (Part-M, Part-145, Part-66, Part-147 and their appendices) Article 1 Objective and scope Article 2 Definitions (given above) Article 3 Continuing airworthiness requirements with Annex I PART M Article 4 Maintenance organisation approvals with Annex II PART 145 Article 5 Certifying staff with Annex II PART 66 Article 6 Training organisation requirements with Annex II PART 147 Article 7 Entry into force Page 21 of 34
AMC & GM of Continuing Airworthiness (Part M, 145, 66 & 147) (EASA Director (ED) Decision 2003/19/RM) Annex I Acceptable Means of Compliance to Part-M Annex II Acceptable Means of Compliance to Part-145 Annex III Guidance Material to Part-145 Annex IV Acceptable Means of Compliance to Part-66 Annex V Guidance Material to Part-66 Annex VI Acceptable Means of Compliance to Part-147 Annex VII Guidance Material to Part-147 Page 22 of 34
Türk Sivil Havacılığı Temel Kanunları Türk Sivil Havacılık Kanunu 2920 / 1983 Ulaştırma Bakanlığını Kanunu 3348 / 1987 Sivil Havacılık Genel Müdürlüğü Kanunu 5431 / 2005 Page 23 of 34
Turkish Civil Aviation Law 2920 14/10/1983 first issued 05/02/2008 last revised BİRİNCİ KISIM Amaç, Kapsam ve Tanımlar Amaç Madde 1 Bu Kanunun amacı; devamlı ve hızlı bir gelişme gösteren,ileri teknolojinin uygulandığı,sürat ve emniyet faktörlerinin büyük önem taşıdığı sivil havacılık sahasındaki faaliyetlerin ulusal çıkarlarımız ve uluslararası ilişkilerimize uygun bir şekilde düzenlenmesini sağlamaktır. Kapsam Madde 2 Bu Kanun,kamu kurum ve kuruluşları ile gerçek ve özel hukuk tüzelkişilerinin havacılık sahasındaki faaliyetlerini kapsar. Devlet hava araçları, açık hüküm bulunmayan hallerde bu Kanunun kapsamı dışındadır. İKİNCİ KISIM - Hava Seyrüseferinin Genel Hükümleri BİRİNCİ BÖLÜM - İKİNCİ BÖLÜM - ÜÇÜNCÜ BÖLÜM - DÖRDÜNCÜ BÖLÜM - BEŞİNCİ BÖLÜM - ALTINCI BÖLÜM - YEDİNCİ BÖLÜM - Türk Hava Egemenliği Hükümleri Sivil Hava Aracı Kazaları Ticari Hava İşletmeleri Havaalanları ve Tesisleri Hava Araçları ve Sicillerin Tutulması Hava Araçlarına İlişkin Uçuş Kuralları Sivil Havacılık Personeli Page 24 of 34
ÜÇÜNCÜ KISIM - Havayolu ile Taşımalar BİRİNCİ BÖLÜM - İç Hat Taşıma Sözleşmesi İKİNCİ BÖLÜM - Hava Araçları Kullanma Sözleşmeleri DÖRDÜNCÜ KISIM - Taşıma Sözleşmesinden Doğan Sorumluluk BİRİNCİ BÖLÜM - Sorumluluk Halleri İKİNCİ BÖLÜM - Üçüncü Kişilere Karşı Sorumluluk BEŞİNCİ KISIM - Ceza Hükümleri ALTINCI KISIM - Çeşitli Hükümler YEDİNCİ KISIM - Son Hükümler Page 25 of 34
ULAŞTIRMA BAKANLIĞININ TEŞKİLAT VE GÖREVLERİ HAKKINDA KANUN 3348 09/04/1987 ilk yayın 04/07/2000 son rev. BİRİNCİ KISIM - Amaç, Görev, Teşkilat Amaç Madde 1 - Bu Kanunun amacı, ülkenin ulaştırma ve haberleşme sistem ve hizmetlerinin ülkenin ihtiyaçlarına uygun olarak tesisi ve geliştirilmesi için Ulaştırma Bakanlığının kurulmasına, teşkilat ve görevlerine ilişkin esasları düzenlemektir. İKİNCİ KISIM - Bakanlık Merkez Teşkilatı ÜÇÜNCÜ KISIM - Taşra Teşkilatı DÖRDÜNCÜ KISIM - Sorumluluk ve Yetkiler BEŞİNCİ KISIM - Çeşitli Hükümler Page 26 of 34
SİVİL HAVACILIK GENEL MÜDÜRLÜĞÜ KANUNU 5431 10/11/2005 ilk yayın BİRİNCİ BÖLÜM - Amaç ve Tanımlar MADDE 1.- Bu Kanunun amacı; Ulaştırma Bakanlığına bağlı, kamu tüzel kişiliğini haiz, özel bütçeli Sivil Havacılık Genel Müdürlüğünün teşkilat, görev, yetki ve sorumlulukları ile ilgili esasları düzenlemektir. İKİNCİ BÖLÜM - Teşkilat, Görevler ve Yetkiler ÜÇÜNCÜ BÖLÜM - Ana Hizmet Birimleri MADDE 7.- Genel Müdürlüğün ana hizmet birimleri şunlardır: a) Uçuş Standartları Daire Başkanlığı. b) Hava Ulaşım Daire Başkanlığı. c) Hava Seyrüsefer Daire Başkanlığı. d) Hava Alanları Daire Başkanlığı. e) Havacılık Güvenliği Daire Başkanlığı. DÖRDÜNCÜ BÖLÜM - Danışma Birimleri BEŞİNCİ BÖLÜM - Yardımcı Hizmet Birimleri ALTINCI BÖLÜM - Sorumluluk, Yetki Devri, Atama ve Düzenleme Yapma YEDİNCİ BÖLÜM - Teknik Denetçiliğe Görevlendirme, Havacılık Uzmanlığı, Personelin Statüsü SEKİZİNCİ BÖLÜM Gelirler, Anlaşmalarla Hizmet Yapma ve Anlaşmazlıkların Halli DOKUZUNCU BÖLÜM - Değiştirilen ve Yürürlükten Kaldırılan Hükümler ONUNCU BÖLÜM - Geçici ve Son Hükümler Page 27 of 34
SHGM TEŞKİLAT Genel Müdür Genel Müdür Genel Müdür Yardımcısı 1. Genel Müdür Yardımcısı Ana Hizmet Birimi Danışma Birimi Yardımcı Hizmet Birimi 1. Uçuş Standartları Daire Başkanlığı 1. Strateji Geliştirme Daire Başkanlığı 1. İnsan Kaynakları Müdürlüğü 2. Genel Müdür Yardımcısı 2. Hava Ulaşım Daire Başkanlığı 2. Hukuk Müşavirliği 2. Destek Hizmetleri Müdürlüğü 3. Hava Seyrüsefer Daire Başkanlığı 4. Hava Alanları Daire Başkanlığı 5. Havacılık Güvenliği Daire Başkanlığı Page 28 of 34
Havayolu veya Bakım Kuruluşunun Kullandığı Parçalardaki Gereklilikler M.A.501 Installation (a) No component may be fitted unless it is in a satisfactory condition, has been appropriately released to service on an EASA Form 1 or equivalent and is marked in accordance with Part 21 Subpart Q, unless otherwise specified in Part-145 and Subpart F. (b) Prior to installation of a component on an aircraft the person or approved maintenance organisation shall ensure that the particular component is eligible to be fitted when different modification and/or airworthiness directive configurations may be applicable. (c) Standard parts shall only be fitted to an aircraft or a component when the maintenance data specifies the particular standard part. Standard parts shall only be fitted when accompanied by evidence of conformity traceable to the applicable standard. (d) Material being either raw material or consumable material shall only be used on an aircraft or a component when the aircraft or component manufacturer states so in relevant maintenance data or as specified in Part-145. Such material shall only be used when the material meets the required specification and has appropriate traceability. All material must be accompanied by documentation clearly relating to the particular material and containing a conformity to specification statement plus both the manufacturing and supplier source. Page 29 of 34
Havayolu veya Bakım Kuruluşunun Kullandığı Parçalardaki Gereklilikler (devamı) M.A.502 Component maintenance (a) The maintenance of components shall be performed by appropriately approved Subpart F or Part-145 maintenance organisations. (b) Maintenance on any component may be performed by M.A.801(b)2 certifying staff only whilst such components are fitted to the aircraft. Such components, nevertheless, can be temporarily removed for maintenance when such removal is expressly permitted by the aircraft maintenance manual to improve access. M.A.503 Service life limited components Installed service life limited components shall not exceed the approved service life limit as specified in the approved maintenance programme and airworthiness directives. M.A.504 Control of unserviceable components (a) A component shall be considered unserviceable in any one of the following circumstances: 1. expiry of the service life limit as defined in the maintenance program; 2. non-compliance with the applicable airworthiness directives and other continued airworthiness requirement mandated by the Agency; 3. absence of the necessary information to determine the airworthiness status or eligibility for installation; 4. evidence of defects or malfunctions; 5. involvement in an incident or accident likely to affect its serviceability. Page 30 of 34
Havayolu veya Bakım Kuruluşunun Kullandığı Parçalardaki Gereklilikler (devamı) M.A.504 Control of unserviceable components (cont.) (b) Unserviceable components shall be identified and stored in a secure location under the control of the M.A.502 approved organisation until a decision is made on the future status of such component. (c) Components which have reached their certified life limit or contain a non-repairable defect shall be classified as unsalvageable and shall not be permitted to re-enter the component supply system, unless certified life limits have been extended or a repair solution has been approved according to M.A.304. (d) Any person or organisation accountable under Part-M shall, in the case of a paragraph (c) unsalvageable components: 1. retain such component in the paragraph (b) location, or; 2. arrange for the component to be mutilated in a manner that ensures that it is beyond economic salvage or repair before relinquishing responsibility for such component. (e) Notwithstanding paragraph (d) a person or organisation accountable under Part-M may transfer responsibility of components classified as unsalvageable to an organisation for training or research without mutilation. Page 31 of 34
Havayolu veya Bakım Kuruluşunun Kullandığı Parçalardaki Gereklilikler (devamı) 145.A.42 Acceptance of components (a) All components shall be classified and appropriately segregated into the following categories: 1. Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Part-21 Subpart Q. 2. Unserviceable components which shall be maintained in accordance with this section. 3. Unsalvageable components which are classified in accordance with 145.A.42(d). 4. Standard parts used on an aircraft, engine, propeller or other aircraft component when specified in the manufacturer's illustrated parts catalogue and/or the maintenance data. 5. Material both raw and consumable used in the course of maintenance when the organisation is satisfied that the material meets the required specification and has appropriate traceability. All material must be accompanied by documentation clearly relating to the particular material and containing a conformity to specification statement plus both the manufacturing and supplier source. (b) Prior to installation of a component, the organisation shall ensure that the particular component is eligible to be fitted when different modification and/or airworthiness directive standards may be applicable. Page 32 of 34
Havayolu veya Bakım Kuruluşunun Kullandığı Parçalardaki Gereklilikler (devamı) (c) The organisation may fabricate a restricted range of parts to be used in the course of undergoing work within its own facilities provided procedures are identified in the exposition. (d) Components which have reached their certified life limit or contain a non-repairable defect shall be classified as unsalvageable and shall not be permitted to re-enter the component supply system unless certified life limits have been extended or a repair solution has been approved according to Part-21. Page 33 of 34
Teşekkürler! Page 34 of 34