Nařízení Komise (EU) č. 748/2012 ze dne 3. srpna 2012, kterým se stanoví prováděcí pravidla pro certifikaci letové způsobilosti letadel a souvisejících výrobků, letadlových částí a zařízení a certifikaci ochrany životního prostředí, jakož i pro certifikaci projekčních a výrobních organizací (přepracované znění) (Text s významem pro EHP)

THE EUROPEAN COMMISSION,

Having regard to the Treaty on the Functioning of the European Union,

Having regard to Regulation (EC) No 216/2008 of the European Parliament and of the Council of 20 February 2008 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency, and repealing Council Directive 91/670/EEC, Regulation (EC) No 1592/2002 and Directive 2004/36/ECOJ L 79, 19.3.2008, p. 1 . , and in particular Articles 5(5) and 6(3) thereof,

This Regulation lays down, in accordance with Article 5(5) and Article 6(3) of Regulation (EC) No 216/2008, common technical requirements and administrative procedures for the airworthiness and environmental certification of products, parts and appliances specifying:

(a) the issue of type-certificates, restricted type-certificates, supplemental type-certificates and changes to those certificates;

(b) the issue of certificates of airworthiness, restricted certificates of airworthiness, permits to fly and authorised release certificates;

(c) the issue of repair design approvals;

(d) the showing of compliance with environmental protection requirements;

(e) the issue of noise certificates;

(f) the identification of products, parts and appliances;

(g) the certification of certain parts and appliances;

(h) the certification of design and production organisations;

(i) the issue of airworthiness directives.

For the purpose of this Regulation, the following definitions shall apply:

(a) JAA means the Joint Aviation Authorities;

(b) JAR means Joint Aviation Requirements;

(c) Part 21 means the requirements and procedures for the certification of aircraft and related products, parts and appliances, and of design and production organisations laid down in Annex I to this Regulation;

(d) Part M means the applicable continuing airworthiness requirements adopted in pursuance of Regulation (EC) No 216/2008;

(e) principal place of business means the head office or registered office of the undertaking within which the principal financial functions and operational control of the activities referred to in this Regulation are exercised;

(f) article means any part and appliance to be used on civil aircraft;

(g) ETSO means European Technical Standard Order. The European Technical Standard Order is a detailed airworthiness specification issued by the European Aviation Safety Agency (the Agency) to ensure compliance with the requirements of this Regulation as a minimum performance standard for specified articles;

(h) EPA means European Part Approval. European Part Approval of an article means the article has been produced in accordance with approved design data not belonging to the type-certificate holder of the related product, except for ETSO articles;

(i) ELA1 aircraft means the following manned European Light Aircraft:(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 1200 kg or less that is not classified as complex motor-powered aircraft;(ii) a sailplane or powered sailplane of 1200 kg MTOM or less;(iii) a balloon with a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air balloons, 1050 m3 for gas balloons, 300 m3 for tethered gas balloons;(iv) an airship designed for not more than 4 occupants and a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air airships and 1000 m3 for gas airships;

(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 1200 kg or less that is not classified as complex motor-powered aircraft;

(ii) a sailplane or powered sailplane of 1200 kg MTOM or less;

(iii) a balloon with a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air balloons, 1050 m3 for gas balloons, 300 m3 for tethered gas balloons;

(iv) an airship designed for not more than 4 occupants and a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air airships and 1000 m3 for gas airships;

(j) ELA2 aircraft means the following manned European Light Aircraft:(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 2000 kg or less that is not classified as complex motor-powered aircraft;(ii) a sailplane or powered sailplane of 2000 kg MTOM or less;(iii) a balloon;(iv) a hot air airship;(v) a gas airship complying with all of the following characteristics:3 % maximum static heaviness, Non-vectored thrust (except reverse thrust), Conventional and simple design of: structure, control system and ballonet system, Non-power assisted controls; (vi) a Very Light Rotorcraft.

(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 2000 kg or less that is not classified as complex motor-powered aircraft;

(ii) a sailplane or powered sailplane of 2000 kg MTOM or less;

(iii) a balloon;

(iv) a hot air airship;

(v) a gas airship complying with all of the following characteristics:3 % maximum static heaviness, Non-vectored thrust (except reverse thrust), Conventional and simple design of: structure, control system and ballonet system, Non-power assisted controls;

(vi) a Very Light Rotorcraft.

OJ L 79, 19.3.2008, p. 1 .

(1) Commission Regulation (EC) No 1702/2003 of 24 September 2003 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisationsOJ L 243, 27.9.2003, p. 6 . has been substantially amended several timesSee Annex II. . Since further amendments are to be made, it should be recast in the interests of clarity.

(2) Regulation (EC) No 216/2008 establishes common essential requirements to provide for a high uniform level of civil aviation safety and environmental protection. It requires the Commission to adopt the necessary implementing rules to ensure their uniform application. It establishes the European Aviation Safety Agency (hereinafter referred to as the Agency) to assist the Commission in the development of such implementing rules.

(3) It is necessary to lay down common technical requirements and administrative procedures to ensure the airworthiness and environmental compatibility of aeronautical products, parts and appliances, subject to Regulation (EC) No 216/2008. Such requirements and procedures should specify the conditions to issue, maintain, amend, suspend or revoke the appropriate certificates.

(4) Organisations involved in the design and production of products, parts and appliances should be required to comply with certain technical requirements in order to demonstrate their capability and means to discharge their obligations and associated privileges. The Commission is required to lay down measures to specify conditions to issue, maintain, amend, suspend or revoke certificates attesting such compliance.

(5) In laying down measures for the implementation of common essential requirements in the field of airworthiness, the Commission must take care that they reflect the state of the art and the best practices, take into account worldwide aircraft experience and scientific and technical progress and allow for immediate reaction to established causes of accidents and serious incidents.

(6) The need to ensure uniformity in the application of common airworthiness and environmental requirements for aeronautical products, parts and appliances requires that common procedures be followed by the competent authorities of the Member States and, where applicable, the Agency to assess compliance with these requirements. The Agency should develop certification specifications and guidance material to facilitate the necessary regulatory uniformity.

(7) It is necessary to recognise the continuing validity of certificates issued before the entry into force of Regulation (EC) No 1702/2003, in accordance with Article 69 of Regulation (EC) No 216/2008.

(8) In order to maintain a high uniform level of aviation safety in Europe, it is necessary to introduce changes to requirements and procedures for the certification of aircraft and related products, parts and appliances and of design and production organisations, in particular to elaborate the rules related to the demonstration of compliance with the type-certification basis and environmental protection requirements and to introduce the possibility to choose to comply with later standards for changes to type-certificates.

(9) The concept and complexity of auxiliary power units (APU) resembles that of aircraft engines and in some cases APU designs are even derived from engine designs. Changes to provisions for repairs to APU are therefore needed to restore consistency with repairs process to engines.

(10) In order to subject non-complex motor-powered aircraft, recreational aircraft and related products, parts and appliances to measures that are proportionate to their simple design and type of operation, while maintaining a high uniform level of aviation safety in Europe, it is necessary to introduce changes to requirements and procedures for the certification of those aircraft and related products, parts and appliances and of design and production organisations and in particular, for the owners of European Light Aircraft below 2000 kg (ELA2) or below 1200 kg (ELA1), to introduce the possibility to accept certain not safety critical parts for installation without an EASA Form 1.

3 % maximum static heaviness,

(11) The Agency prepared draft implementing rules and submitted them as opinions No 01/2009 on Possibility to deviate from airworthiness code in case of design changes, No 02/2009 on Repair and design changes to European Technical Standard Order, No 01/2010 on SubPart J DOA and Opinion No 01/2011 on ELA Process and standard changes and repairs to the Commission in accordance with Article 19(1) of Regulation (EC) No 216/2008.

(12) The measures provided for in this Regulation are in accordance with the opinion of the European Aviation Safety Agency Committee established by Article 65(1) of Regulation (EC) No 216/2008,

Non-vectored thrust (except reverse thrust),

Conventional and simple design of: structure, control system and ballonet system,

Non-power assisted controls;

Products, parts and appliances shall be issued certificates as specified in Annex I (Part 21).

By way of derogation from point 1, aircraft, including any installed product, part and appliance, which are not registered in a Member State shall be exempted from the provisions of Subparts H and I of Annex I (Part 21). They shall also be exempted from the provisions of Subpart P of Annex I (Part 21) except when aircraft identification marks are prescribed by a Member State.

OJ L 243, 27.9.2003, p. 6 .

Article 1 Article 1 Scope and definitions 1.This Regulation lays down, in accordance with Article 5(5) and Article 6(3) of Regulation (EC) No 216/2008, common technical requirements and administrative procedures for the airworthiness and environmental certification of products, parts and appliances specifying: (a) the issue of type-certificates, restricted type-certificates, supplemental type-certificates and changes to those certificates;(b) the issue of certificates of airworthiness, restricted certificates of airworthiness, permits to fly and authorised release certificates;(c) the issue of repair design approvals;(d) the showing of compliance with environmental protection requirements;(e) the issue of noise certificates;(f) the identification of products, parts and appliances;(g) the certification of certain parts and appliances;(h) the certification of design and production organisations;(i) the issue of airworthiness directives. 2.For the purpose of this Regulation, the following definitions shall apply: (a) JAA means the Joint Aviation Authorities;(b) JAR means Joint Aviation Requirements;(c) Part 21 means the requirements and procedures for the certification of aircraft and related products, parts and appliances, and of design and production organisations laid down in Annex I to this Regulation;(d) Part M means the applicable continuing airworthiness requirements adopted in pursuance of Regulation (EC) No 216/2008;(e) principal place of business means the head office or registered office of the undertaking within which the principal financial functions and operational control of the activities referred to in this Regulation are exercised;(f) article means any part and appliance to be used on civil aircraft;(g) ETSO means European Technical Standard Order. The European Technical Standard Order is a detailed airworthiness specification issued by the European Aviation Safety Agency (the Agency) to ensure compliance with the requirements of this Regulation as a minimum performance standard for specified articles;(h) EPA means European Part Approval. European Part Approval of an article means the article has been produced in accordance with approved design data not belonging to the type-certificate holder of the related product, except for ETSO articles;(i) ELA1 aircraft means the following manned European Light Aircraft:(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 1200 kg or less that is not classified as complex motor-powered aircraft;(ii) a sailplane or powered sailplane of 1200 kg MTOM or less;(iii) a balloon with a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air balloons, 1050 m3 for gas balloons, 300 m3 for tethered gas balloons;(iv) an airship designed for not more than 4 occupants and a maximum design lifting gas or hot air volume of not more than 3400 m3 for hot air airships and 1000 m3 for gas airships; (j) ELA2 aircraft means the following manned European Light Aircraft:(i) an aeroplane with a Maximum Take-off Mass (MTOM) of 2000 kg or less that is not classified as complex motor-powered aircraft;(ii) a sailplane or powered sailplane of 2000 kg MTOM or less;(iii) a balloon;(iv) a hot air airship;(v) a gas airship complying with all of the following characteristics:3 % maximum static heaviness, Non-vectored thrust (except reverse thrust), Conventional and simple design of: structure, control system and ballonet system, Non-power assisted controls; (vi) a Very Light Rotorcraft.

Article 2 Article 2 Products, parts and appliances certification 1.Products, parts and appliances shall be issued certificates as specified in Annex I (Part 21). 2.By way of derogation from point 1, aircraft, including any installed product, part and appliance, which are not registered in a Member State shall be exempted from the provisions of Subparts H and I of Annex I (Part 21). They shall also be exempted from the provisions of Subpart P of Annex I (Part 21) except when aircraft identification marks are prescribed by a Member State.

Article 3 Article 3 Continued validity of type-certificates and related certificates of airworthiness 1.With regard to products which had a type-certificate, or a document allowing the issuing of a certificate of airworthiness, issued before 28 September 2003 by a Member State, the following provisions shall apply: (a) the product shall be deemed to have a type-certificate issued in accordance with this Regulation when:(i) its type-certification basis was:the JAA type-certification basis, for products that have been certificated under JAA procedures, as defined in their JAA data sheet, or for other products, the type-certification basis as defined in the type-certificate data sheet of the State of design, if that State of design was: a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation. The Agency shall make a first evaluation of the implication of the provisions of the second indent in view of producing an opinion to the Commission including possible amendments to this Regulation; (ii) the environmental protection requirements were those laid down in Annex 16 to the Chicago Convention, as applicable to the product;(iii) the applicable airworthiness directives were those of the State of design; (b) the design of an individual aircraft, which was on the register of a Member State before 28 September 2003 , shall be deemed to have been approved in accordance with this Regulation when:(i) its basic type design was part of a type-certificate referred to in point (a);(ii) all changes to this basic type design, which were not under the responsibility of the type-certificate holder, had been approved; and(iii) the airworthiness directives issued or adopted by the Member State of registry before 28 September 2003 were complied with, including any variations to the airworthiness directives of the State of design agreed by the Member State of registry. 2.With regard to products for which a type-certification process was proceeding through the JAA or a Member State on 28 September 2003 , the following shall apply: (a) if a product is under certification by several Member States, the most advanced project shall be used as the reference;(b) points 21.A.15(a), (b) and (c) of Annex I (Part 21) shall not apply;(c) by way of derogation from point 21.A.17(a) of Annex I (Part 21), the type-certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the approval;(d) compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.20(a) and (b) of Annex I (Part 21). 3.With regard to products that have a national type-certificate, or equivalent, and for which the approval process of a change carried out by a Member State was not finalised at the time when the type-certificate had to be in accordance with this Regulation, the following shall apply: (a) if an approval process is being carried out by several Member States, the most advanced project shall be used as the reference;(b) point 21.A.93 of Annex I (Part 21) shall not apply;(c) the applicable type-certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the approval of change;(d) compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.103(a)(2) and (b) of Annex I (Part 21). 4.With regard to products that had a national type-certificate, or equivalent, and for which the approval process of a major repair design carried out by a Member State was not finalised at the time when the type-certificate had to be determined in accordance with this Regulation, compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.433(a) of Annex I (Part 21). 5.A certificate of airworthiness issued by a Member State attesting conformity with a type-certificate determined in accordance with point 1 shall be deemed to comply with this Regulation.

Article 4 Article 4 Continued validity of supplemental type-certificates 1.With regard to supplemental type-certificates issued by a Member State under JAA procedures or applicable national procedures and with regard to changes to products proposed by persons other than the type-certificate holder of the product, which were approved by a Member State under applicable national procedures, if the supplemental type-certificate, or change, was valid on 28 September 2003 , the supplemental type-certificate, or change shall be deemed to have been issued under this Regulation. 2.With regard to supplemental type-certificates for which a certification process was being carried out by a Member State on 28 September 2003 under applicable JAA supplemental type-certificate procedures and with regard to major changes to products, proposed by persons other than the type-certificate holder of the product, for which a certification process was being carried out by a Member State on 28 September 2003 under applicable national procedures, the following shall apply: (a) if a certification process was being carried out by several Member States, the most advanced project shall be used as the reference;(b) point 21.A.113 (a) and (b) of Annex I (Part 21) shall not apply;(c) the applicable certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the supplemental type-certificate or the major change approval;(d) the compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.115(a) of Annex I (Part 21).

Article 5 Article 5 Continued operation of certain aircraft registered by Member States

Article 6 Article 6 Continued validity of parts and appliances certificates 1.Approvals of parts and appliances issued by a Member State and valid on 28 September 2003 shall be deemed to have been issued in accordance with this Regulation. 2.With regard to parts and appliances for which an approval or authorisation process was being carried out by a Member State on 28 September 2003 , the following shall apply: (a) if an authorisation process was being carried out by several Member States, the most advanced project shall be used as the reference;(b) point 21.A.603 of Annex I (Part 21) shall not apply;(c) the applicable data requirements laid down in point 21.A.605 of Annex I (Part 21) shall be those established by the relevant Member State, at the date of application for the approval or authorisation;(d) compliance findings made by the relevant Member State shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.606(b) of Annex I (Part 21).

Article 7 Article 7 Permit to fly

Article 8 Article 8 Design organisations 1.An organisation responsible for the design of products, parts and appliances or for changes or repairs thereto shall demonstrate its capability in accordance with Annex I (Part 21). 2.By way of derogation from point 1, an organisation whose principal place of business is in a non-member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies, provided: (a) that State is the State of design; and(b) the Agency has determined that the system of that State includes the same independent level of checking of compliance as provided by this Regulation, either through an equivalent system of approvals of organisations or through direct involvement of the competent authority of that State. 3.Design organisation approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before 28 September 2003 shall be deemed to comply with this Regulation.

Article 9 Article 9 Production organisations 1.An organisation responsible for the manufacture of products, parts and appliances shall demonstrate its capability in accordance with the provisions of Annex I (Part 21). 2.By way of derogation from point 1, a manufacturer whose principal place of business is in a non-member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies, provided: (a) that State is the State of manufacture; and(b) the Agency has determined that the system of that State includes the same independent level of checking of compliance as provided by this Regulation, either through an equivalent system of approvals of organisations or through direct involvement of the competent authority of that State. 3.Production organisation approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before 28 September 2003 shall be deemed to comply with this Regulation.

Article 10 Article 10 Agency measures 1.The Agency shall develop acceptable means of compliance (hereinafter called AMC) that competent authorities, organisations and personnel may use to demonstrate compliance with the provisions of the Annex I (Part 21) to this Regulation. 2.The AMC issued by the Agency shall neither introduce new requirements nor alleviate the requirements of the Annex I (Part 21) to this Regulation. 3.Without prejudice to Articles 54 and 55 of Regulation (EC) No 216/2008, when the acceptable means of compliance issued by the Agency are used, the related requirements of the Annex I (Part 21) to this Regulation shall be considered as met without further demonstration.

Article 11 Article 11 Repeal

Article 12 Article 12 Entry into force

With regard to products which had a type-certificate, or a document allowing the issuing of a certificate of airworthiness, issued before 28 September 2003 by a Member State, the following provisions shall apply:

(a) the product shall be deemed to have a type-certificate issued in accordance with this Regulation when:(i) its type-certification basis was:the JAA type-certification basis, for products that have been certificated under JAA procedures, as defined in their JAA data sheet, or for other products, the type-certification basis as defined in the type-certificate data sheet of the State of design, if that State of design was: a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation. The Agency shall make a first evaluation of the implication of the provisions of the second indent in view of producing an opinion to the Commission including possible amendments to this Regulation; (ii) the environmental protection requirements were those laid down in Annex 16 to the Chicago Convention, as applicable to the product;(iii) the applicable airworthiness directives were those of the State of design;

(i) its type-certification basis was:the JAA type-certification basis, for products that have been certificated under JAA procedures, as defined in their JAA data sheet, or for other products, the type-certification basis as defined in the type-certificate data sheet of the State of design, if that State of design was: a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation. The Agency shall make a first evaluation of the implication of the provisions of the second indent in view of producing an opinion to the Commission including possible amendments to this Regulation;

(ii) the environmental protection requirements were those laid down in Annex 16 to the Chicago Convention, as applicable to the product;

(iii) the applicable airworthiness directives were those of the State of design;

a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or

a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation.

(b) the design of an individual aircraft, which was on the register of a Member State before 28 September 2003 , shall be deemed to have been approved in accordance with this Regulation when:(i) its basic type design was part of a type-certificate referred to in point (a);(ii) all changes to this basic type design, which were not under the responsibility of the type-certificate holder, had been approved; and(iii) the airworthiness directives issued or adopted by the Member State of registry before 28 September 2003 were complied with, including any variations to the airworthiness directives of the State of design agreed by the Member State of registry.

(i) its basic type design was part of a type-certificate referred to in point (a);

(ii) all changes to this basic type design, which were not under the responsibility of the type-certificate holder, had been approved; and

(iii) the airworthiness directives issued or adopted by the Member State of registry before 28 September 2003 were complied with, including any variations to the airworthiness directives of the State of design agreed by the Member State of registry.

With regard to products for which a type-certification process was proceeding through the JAA or a Member State on 28 September 2003 , the following shall apply:

(a) if a product is under certification by several Member States, the most advanced project shall be used as the reference;

(b) points 21.A.15(a), (b) and (c) of Annex I (Part 21) shall not apply;

(c) by way of derogation from point 21.A.17(a) of Annex I (Part 21), the type-certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the approval;

(d) compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.20(a) and (b) of Annex I (Part 21).

With regard to products that have a national type-certificate, or equivalent, and for which the approval process of a change carried out by a Member State was not finalised at the time when the type-certificate had to be in accordance with this Regulation, the following shall apply:

(a) if an approval process is being carried out by several Member States, the most advanced project shall be used as the reference;

(b) point 21.A.93 of Annex I (Part 21) shall not apply;

(c) the applicable type-certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the approval of change;

(d) compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with points 21.A.103(a)(2) and (b) of Annex I (Part 21).

With regard to products that had a national type-certificate, or equivalent, and for which the approval process of a major repair design carried out by a Member State was not finalised at the time when the type-certificate had to be determined in accordance with this Regulation, compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.433(a) of Annex I (Part 21).

A certificate of airworthiness issued by a Member State attesting conformity with a type-certificate determined in accordance with point 1 shall be deemed to comply with this Regulation.

See Annex II.

the JAA type-certification basis, for products that have been certificated under JAA procedures, as defined in their JAA data sheet, or

for other products, the type-certification basis as defined in the type-certificate data sheet of the State of design, if that State of design was: a Member State, unless the Agency determines, taking into account, in particular, airworthiness codes used and service experience, that such type-certification basis does not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation, or a State with which a Member State had concluded a bilateral airworthiness agreement or similar arrangement under which such products have been certificated on the basis of the airworthiness codes of that State of design, unless the Agency determines that such airworthiness codes or service experience or the safety system of that State of design do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 and this Regulation.

With regard to supplemental type-certificates issued by a Member State under JAA procedures or applicable national procedures and with regard to changes to products proposed by persons other than the type-certificate holder of the product, which were approved by a Member State under applicable national procedures, if the supplemental type-certificate, or change, was valid on 28 September 2003 , the supplemental type-certificate, or change shall be deemed to have been issued under this Regulation.

With regard to supplemental type-certificates for which a certification process was being carried out by a Member State on 28 September 2003 under applicable JAA supplemental type-certificate procedures and with regard to major changes to products, proposed by persons other than the type-certificate holder of the product, for which a certification process was being carried out by a Member State on 28 September 2003 under applicable national procedures, the following shall apply:

(a) if a certification process was being carried out by several Member States, the most advanced project shall be used as the reference;

(b) point 21.A.113 (a) and (b) of Annex I (Part 21) shall not apply;

(c) the applicable certification basis shall be that established by the JAA or, where applicable, the Member State at the date of application for the supplemental type-certificate or the major change approval;

(d) the compliance findings made under JAA or Member State procedures shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.115(a) of Annex I (Part 21).

For EU-15: 28 September 2003 ; for EU-10: 1 May 2004 and for EU-2: 1 January 2007 .

With regard to an aircraft that cannot be deemed to have a type-certificate issued in accordance with Article 3(1)(a) of this Regulation, that has been issued a certificate of airworthiness by a Member State before Regulation (EC) No 1702/2003 became applicable in that Member StateFor EU-15: 28 September 2003 ; for EU-10: 1 May 2004 and for EU-2: 1 January 2007 . , was on its register on that date, and was still on the register of a Member State on 28 March 2007 , the combination of the following shall be deemed to constitute the applicable specific airworthiness specifications issued in accordance with this Regulation:

(a) the type-certificate data sheet and type-certificate data sheet for noise, or equivalent documents, of the State of design, provided that the State of design has concluded the appropriate working arrangement in accordance with Article 27(2) of Regulation (EC) No 216/2008 with the Agency covering the continued airworthiness of the design of such an aircraft;

(b) the environmental protection requirements laid down in Annex 16 to the Chicago Convention, as applicable to that aircraft; and

(c) the mandatory continuing airworthiness information of the State of design.

Approvals of parts and appliances issued by a Member State and valid on 28 September 2003 shall be deemed to have been issued in accordance with this Regulation.

With regard to parts and appliances for which an approval or authorisation process was being carried out by a Member State on 28 September 2003 , the following shall apply:

(a) if an authorisation process was being carried out by several Member States, the most advanced project shall be used as the reference;

(b) point 21.A.603 of Annex I (Part 21) shall not apply;

(c) the applicable data requirements laid down in point 21.A.605 of Annex I (Part 21) shall be those established by the relevant Member State, at the date of application for the approval or authorisation;

(d) compliance findings made by the relevant Member State shall be deemed to have been made by the Agency for the purpose of complying with point 21.A.606(b) of Annex I (Part 21).

The conditions determined before 28 March 2007 by the Member States for permits to fly or other airworthiness certificate issued for aircraft which did not hold a certificate of airworthiness or restricted certificate of airworthiness issued under this Regulation, are deemed to have been determined in accordance with this Regulation, unless the Agency has determined before 28 March 2008 that such conditions do not provide for a level of safety equivalent to that required by Regulation (EC) No 216/2008 or this Regulation.

An organisation responsible for the design of products, parts and appliances or for changes or repairs thereto shall demonstrate its capability in accordance with Annex I (Part 21).

By way of derogation from point 1, an organisation whose principal place of business is in a non-member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies, provided:

(a) that State is the State of design; and

(b) the Agency has determined that the system of that State includes the same independent level of checking of compliance as provided by this Regulation, either through an equivalent system of approvals of organisations or through direct involvement of the competent authority of that State.

Design organisation approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before 28 September 2003 shall be deemed to comply with this Regulation.

An organisation responsible for the manufacture of products, parts and appliances shall demonstrate its capability in accordance with the provisions of Annex I (Part 21).

By way of derogation from point 1, a manufacturer whose principal place of business is in a non-member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies, provided:

(a) that State is the State of manufacture; and

(b) the Agency has determined that the system of that State includes the same independent level of checking of compliance as provided by this Regulation, either through an equivalent system of approvals of organisations or through direct involvement of the competent authority of that State.

Production organisation approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before 28 September 2003 shall be deemed to comply with this Regulation.

The Agency shall develop acceptable means of compliance (hereinafter called AMC) that competent authorities, organisations and personnel may use to demonstrate compliance with the provisions of the Annex I (Part 21) to this Regulation.

The AMC issued by the Agency shall neither introduce new requirements nor alleviate the requirements of the Annex I (Part 21) to this Regulation.

Without prejudice to Articles 54 and 55 of Regulation (EC) No 216/2008, when the acceptable means of compliance issued by the Agency are used, the related requirements of the Annex I (Part 21) to this Regulation shall be considered as met without further demonstration.

Regulation (EC) No 1702/2003 is repealed.

References to the repealed Regulation shall be construed as references to this Regulation and shall be read in accordance with the correlation table in Annex III.

This Regulation shall enter into force on the twentieth day following that of its publication in the Official Journal of the European Union .

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