Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2779

c) the temperature gradients are: Note 1.— The standard geopotential metre has the value 9.80665 m2 s–2. Note 2.— See Doc 7488 for the relationship between the variables and for tables giving the corresponding values of temperature, pressure, density and geopotential. Note 3.— Doc 7488 also gives the specific weight, dynamic viscosity, kinematic viscosity and speed of sound at various altitudes. State of Design. The State having jurisdiction over the organization responsible for the type design. State of Manufacture. The State having jurisdiction over the organization responsible for the final assembly of the aircraft. State of Registry. The State on whose register the aircraft is entered. Note.— In the case of the registration of aircraft of an international operating agency on other than a national basis, the States constituting the agency are jointly and severally bound to assume the obligations which, under the Chicago Convention, attach to a State of Registry. See, in this regard, the Council Resolution of 14 December 1967 on Nationality and Registration of Aircraft Operated by International Operating Agencies which can be found in Policy and Guidance Material on the Economic Regulation of International Air Transport (Doc 9587). Take-off surface. That part of the surface of an aerodrome which the aerodrome authority has declared available for the normal ground or water run of aircraft taking off in a particular direction. Geopotential altitude (km) Temperature gradient From To (Kelvin per standard geopotential kilometre) –5.0 11.0 –6.5 11.0 20.0 0.0 20.0 32.0 +1.0 32.0 47.0 +2.8 47.0 51.0 0.0 51.0 71.0 –2.8 71.0 80.0 –2.0 2007/70/II. szám Part I Annex 8 — Airworthiness of Aircraft I-3 2/3/04 Type Certificate. A document issued by a Contracting State to define the design of an aircraft type and to certify that this design meets the appropriate airworthiness requirements of that State. Ultimate load. The limit load multiplied by the appropriate factor of safety. 2007/70/II. szám ANNEX 8 II-1-1 2/3/04 PART II. PROCEDURES FOR CERTIFICATION AND CONTINUING AIRWORTHINESS Note.— Although the Convention on International Civil Aviation allocates to the State of Registry certain functions which that State is entitled to discharge, or obligated to discharge, as the case may be, the Assembly recognized, in Resolution A23-13, that the State of Registry may be unable to fulfil its responsibilities adequately in instances where aircraft are leased, chartered or interchanged — in particular without crew — by an operator of another State and that the Convention may not adequately specify the rights and obligations of the State of an Operator in such instances until such time as Article 83 bis of the Convention enters into force. Accordingly, the Council urged that if, in the abovementioned instances, the State of Registry finds itself unable to discharge adequately the functions allocated to it by the Convention, it delegate to the State of the Operator, subject to acceptance by the latter State, those functions of the State of Registry that can more adequately be discharged by the State of the Operator. It was understood that pending entry into force of Article 83 bis of the Convention, the foregoing action would only be a matter of practical convenience and would not affect either the provisions of the Chicago Convention prescribing the duties of the State of Registry or any third State. However, as Article 83 bis entered into force on 20 June 1997, such transfer agreements will have effect in respect of those Contracting States which have ratified the related Protocol (Doc 9318) upon fulfilment of the conditions established in Article 83 bis. CHAPTER 1. TYPE CERTIFICATION 1.1 Applicability The Standards of this chapter shall be applicable to all aircraft of types for which the application for certification was submitted to a Contracting State on or after 13 June 1960, except that the provisions of 1.4 of this part shall only be applicable to an aircraft type for which an application for a Type Certificate is submitted to the State of Design on or after 2 March 2004. Note.— Normally, a request for a type certificate is submitted by the aircraft manufacturer when the aircraft is intended for serial production. 1.2 Design aspects of the appropriate airworthiness requirements 1.2.1 The design aspects of the appropriate airworthiness requirements, used by a Contracting State for type certification in respect of a class of aircraft or for any change to such type certification, shall be such that compliance with them will ensure compliance with the Standards of Part II of this Annex and, where applicable, with the Standards of Parts IIIA, IIIB and IV of this Annex. 1.2.2 The design shall not have any features or characteristics that render it unsafe under the anticipated operating conditions. 1.2.3 Where the design features of a particular aircraft render any of the design aspects of the appropriate airworthiness requirements or the Standards in Parts IIIA, IIIB or IV inappropriate, the Contracting State shall apply appropriate requirements that will give at least an equivalent level of safety. 1.2.4 Where the design features of a particular aircraft render any of the design aspects of the appropriate airworthiness requirements or the Standards in Parts IIIA, IIIB or IV inadequate, additional technical requirements that are considered by the Contracting State to give at least an equivalent level of safety shall be applied. Note.— An Airworthiness Manual (Doc 9760) containing guidance material has been published by ICAO. 1.3 Proof of compliance with the design aspects of the appropriate airworthiness requirements 1.3.1 There shall be an approved design consisting of such drawings, specifications, reports and documentary evidence as are necessary to define the design of the aircraft and to show compliance with the design aspects of the appropriate airworthiness requirements. Note.— The approval of the design is facilitated, in some States, by approving the design organization. 2007/70/II. szám Annex 8 — Airworthiness of Aircraft Part II 2/3/04 II-1-2 1.3.2 The aircraft shall be subjected to such inspections and ground and flight tests as are deemed necessary by the State to show compliance with the design aspects of the appropriate airworthiness requirements. 1.3.3 In addition to determining compliance with the design aspects of the appropriate airworthiness requirements for an aircraft, Contracting States shall take whatever other steps they deem necessary to ensure that the design approval is withheld if the aircraft is known or suspected to have dangerous features not specifically guarded against by those requirements. 1.3.4 A Contracting State issuing an approval for the design of a modification, of a repair or of a replacement part shall do so on the basis of satisfactory evidence that the aircraft continues to comply with the design aspects of the appropriate airworthiness requirements used for the type certification of that aircraft type or amended Type Certificate. Note.— The approval of the design of a modification to an aircraft is signified, in some States, by the issuance of a supplemental Type Certificate or amended Type Certificate. 1.4 Type Certificate 1.4.1 The State of Design, upon receipt of satisfactory evidence that the aircraft type is in compliance with the design aspects of the appropriate airworthiness requirements, shall issue a Type Certificate to define the design and to signify approval of the design of the aircraft type. 1.4.2 When a Contracting State, other than the State of Design, issues a Type Certificate for an aircraft type, it shall do so on the basis of satisfactory evidence that the aircraft type is in compliance with the design aspects of the appropriate airworthiness requirements. 2007/70/II. szám ANNEX 8 II-2-1 2/3/04 CHAPTER 2. PRODUCTION 2.1 Applicability The Standards of this chapter are applicable to all aircraft. 2.2 Production 2.2.1 Aircraft production The State of Manufacture shall ensure that each aircraft, including parts manufactured by sub-contractors, conforms to the approved design. 2.2.2 Parts production The Contracting State taking responsibility for the production of parts manufactured under the design approval referred to in 1.3.4 of Part II shall ensure that the parts conform to the approved design. 2.2.3 Production control When approving production of aircraft or aircraft parts, a Contracting State shall ensure that it is performed in a controlled manner including the use of a quality system so that construction and assembly are satisfactory. Note.— The oversight of production is facilitated, in some States, by approving the production organization. 2.2.4 Traceability Records shall be maintained such that the identification of the aircraft and of the parts with their approved design and production can be established. 2007/70/II. szám ANNEX 8 II-3-1 2/3/04 CHAPTER 3. CERTIFICATE OF AIRWORTHINESS Note.— The Certificate of Airworthiness as used in these Standards is the Certificate of Airworthiness referred to in Article 31 of the Convention. 3.1 Applicability The Standards of this chapter are applicable in respect of all aircraft, except 3.3 and 3.4 which are not applicable in respect of all aircraft that are of a type of which the prototype was submitted to appropriate national authorities for certification before 13 June 1960. 3.2 Issuance and renewal of a Certificate of Airworthiness 3.2.1 A Certificate of Airworthiness shall be issued by a Contracting State on the basis of satisfactory evidence that the aircraft complies with the design aspects of the appropriate airworthiness requirements. 3.2.2 A Contracting State shall not issue or render valid a Certificate of Airworthiness for which it intends to claim recognition pursuant to Article 33 of the Convention on International Civil Aviation unless it has satisfactory evidence that the aircraft complies with the applicable Standards of this Annex through compliance with appropriate airworthiness requirements. 3.2.3 A Certificate of Airworthiness shall be renewed or shall remain valid, subject to the laws of the State of Registry, provided that the State of Registry shall require that the continuing airworthiness of the aircraft shall be determined by a periodical inspection at appropriate intervals having regard to lapse of time and type of service or, alternatively, by means of a system of inspection, approved by the State, that will produce at least an equivalent result. 3.2.4 When an aircraft possessing a valid Certificate of Airworthiness issued by a Contracting State is entered on the register of another Contracting State, the new State of Registry, when issuing another Certificate of Airworthiness or rendering the original certificate valid, may consider prior issuance of the Certificate of Airworthiness by a Contracting State as satisfactory evidence, in whole or in part, that the aircraft is airworthy and in compliance with the appropriate airworthiness requirements. The validity of the authorization shall not extend beyond the period of validity of the Certificate of Airworthiness. Note.— This applies both when the aircraft is registered for the first time and when the aircraft changes its nationality. 3.3 Standard form of Certificate of Airworthiness 3.3.1 The Certificate of Airworthiness shall contain the information shown in Figure 1 and shall be generally similar to it. 3.3.2 When Certificates of Airworthiness are issued in a language other than English, they shall include an English translation. Note.— Article 29 of the Convention on International Civil Aviation requires that the Certificate of Airworthiness be carried on board every aircraft engaged in international air navigation. 3.4 Aircraft limitations and information Each aircraft shall be provided with a flight manual, placards, or other documents stating the approved limitations within which the aircraft is considered airworthy as defined by the appropriate airworthiness requirements, and additional instructions and information necessary for the safe operation of the aircraft. 3.5 Temporary loss of airworthiness Any failure to maintain an aircraft in an airworthy condition as defined by the appropriate airworthiness requirements shall render the aircraft ineligible for operation until the aircraft is restored to an airworthy condition. 3.6 Damage to aircraft 3.6.1 When an aircraft has sustained damage, the State of Registry shall judge whether the damage is of a nature such that the aircraft is no longer airworthy as defined by the appropriate airworthiness requirements. 2007/70/II. szám Annex 8 — Airworthiness of Aircraft Part II 2/3/04 II-3-2 3.6.2 If the damage is sustained or ascertained when the aircraft is in the territory of another Contracting State, the authorities of the other Contracting State shall be entitled to prevent the aircraft from resuming its flight on the condition that they shall advise the State of Registry immediately, communicating to it all details necessary to formulate the judgement referred to in 3.6.1. 3.6.3 When the State of Registry considers that the damage sustained is of a nature such that the aircraft is no longer airworthy, it shall prohibit the aircraft from resuming flight until it is restored to an airworthy condition; the State of Registry may, however, in exceptional circumstances, prescribe particular limiting conditions to permit the aircraft to fly without fare-paying passengers to an aerodrome at which it will be restored to an airworthy condition, and the Contracting State that had originally, in accordance with 3.6.2, prevented the aircraft from resuming flights shall permit such flight. 3.6.4 When the State of Registry considers that the damage sustained is of a nature such that the aircraft is still airworthy, the aircraft shall be allowed to resume its flight. * For use of the State of Registry. ** Manufacturer’s designation of aircraft should contain the aircraft type and model. *** This space shall be used either for periodic endorsement (giving date of expiry) or for a statement that the aircraft is being maintained under a system of continuous inspection. Figure 1 * State of Registry Issuing Authority CERTIFICATE OF AIRWORTHINESS *

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