Commission Delegated Regulation (EU) 2022/1358 of 2 June 2022 amending Regulation (EU) No 748/2012 as regards the implementation of more proportionate requirements for aircraft used for sport and recreational aviation

• (a) The procedures for applying for the issuance of permits to fly and related flight conditions for aircraft within the scope of this Annex shall be those established in Subpart P of Section A of Annex I (Part 21) and those established in points (b) and (c) of point 21L.A.241.

• (b) When applying for a permit to fly in accordance with point 21.A.707 of Annex I (Part 21), the applicant shall arrange for the competent authority to conduct a conformity inspection of the aircraft when the application for a permit to fly relates to:

• 1. the demonstration of compliance activities in point 21L.A.25 for an aircraft which is, or is intended to be, type-certified;

• 1. the demonstration of compliance activities in point 21L.A.44 for an aircraft for which design compliance is, or is intended to be, declared.

• (c) When applying for flight conditions in accordance with point 21.A.709 of Annex I (Part 21), the applicant shall arrange for the Agency:

• 1. to physically inspect and assess the aircraft if the flight conditions are related to the demonstration of compliance to support a declaration of design compliance in point 21L.A.44 and if requested by the Agency during the demonstration of compliance activities as referred to in point (b) of point 21L.B.121 and point (c) of point 21L.B.203; or

• 1. to physically inspect and assess the aircraft and to conduct a critical design review if the flight conditions are related to the demonstration of compliance associated with the certification of the design in point 21L.A.25 and if requested by the Agency in point 21L.B.83, point 21L.B.102 and point 21L.B.203.

SUBPART Q –   IDENTIFICATION OF PRODUCTS AND PARTS

21L.A.251   Scope

This Subpart establishes the requirements for the identification of products and parts designed and produced under this Annex.

21L.A.252   Design of markings

• (a) The holder of a type certificate, supplemental type certificate, approval of a change to type certificate or approval of a repair design, or the declarant of a declaration of design compliance shall specify in the design data the marking of products and parts designed in accordance with this Annex.

• (b) The specifications of the marking shall include the following information:

• 1. for products:

• (i) the name of the production organisation;

• (ii) the product designation;

• (iii) the serial number of the product;

• (iv) any other information appropriate to identify the product;

• 1. for parts:

• (i) a name, trademark, or symbol identifying the production organisation;

• (ii) the part number;

• (iii) the serial number, in cases where a part to be fitted on a product has been identified as a critical part.

• (c) The specification of parts in accordance with point (ii) of point (b)(2) shall include the letter ‘(R)’ at the end of the part number when:

• 1. the part is from a design subject to a declaration of design compliance in accordance with Subpart C of this Annex;

• 1. the part is to be released on an EASA Form 1 in accordance with point (a) of point 21L.A.193; and

• 1. the part has been produced in accordance with Subpart R of this Annex.

21L.A.253   Identification of products

• (a) Any natural or legal person who produces products under Subpart G of Section A of Annex I (Part 21) or under Subpart G or R of this Annex for which the design has been approved or declared in accordance with this Annex shall identify that product as specified in accordance with 21L.A.252 by means of a fireproof marking on a fireproof plate.

• (b) The identification plate shall be secured in such a manner that it is accessible and legible, and will not likely be defaced or removed during normal service, or lost or destroyed in an accident, and in the case of a propeller, propeller blade, or propeller hub, placed on a non-critical surface of the item.

• (c) For manned balloons, the identification plate shall be secured to the balloon envelope and shall be located, if practicable, where it is legible to the operator when the balloon is inflated. In addition, the basket, load frame assembly and any heater assembly shall be permanently and legibly marked with the name of the production organisation, part number, or its equivalent, and the serial number, or its equivalent.

21L.A.254   Handling of identification data

• (a) Any natural or legal person performing maintenance work in accordance with Regulation (EU) No 1321/2014 may, in accordance with methods, techniques and practices established by the Agency:

• 1. remove, change, or place the identification information referred to in point 21L.A.253; or

• 1. remove or install an identification plate referred to in point 21L.A.253, when necessary during maintenance operations.

• (b) Unless for the purposes stated in point (a) of point 21L.A.254, no person shall remove, change, or place the identification information referred to in point (a) of point 21L.A.253.

• (c) Unless for the purposes stated in point (a) of point 21L.A.254, no person shall remove or install any identification plate referred to in point (a) of point 21L.A.253.

• (d) No person shall install an identification plate removed in accordance with point (a)(2) on any aircraft, engine, propeller, propeller blade, or propeller hub other than the one from which it was removed.

21L.A.255   Identification of parts

Any natural or legal person who produces parts under Subpart G of Section A of Annex I (Part 21) or under Subpart G or R of this Annex for a product for which the design has been approved or declared in accordance with this Annex shall permanently and legibly mark that part as specified in accordance with point 21L.A.252.

SUBPART R –   STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATE (EASA FORM 1) FOR ENGINES AND PROPELLERS, OR PARTS THEREOF, WHICH CONFORM TO A DECLARATION OF DESIGN COMPLIANCE

21L.A.271   Scope

This Subpart establishes the procedures for the issuance of statements of conformity for aircraft (EASA Form 52B) and authorised release certificates (EASA Form 1) for engines and propellers, or parts thereof, that have been produced in conformity with the design data of a declaration of design compliance, and the rights and obligations of the declarant.

21L.A.272   Eligibility

Any natural or legal person who is granted access to the applicable design data and is able to undertake the obligations stated in point 21L.A.275 may issue a statement of conformity (EASA Form 52B) for an aircraft or an authorised release certificate (EASA Form 1) for an engine or propeller, or a part thereof, under the conditions laid down in this Subpart.

21L.A.273   Production control system

A natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) with the applicable declared design data of an aircraft, engine or propeller, or a part thereof, that they have produced, shall establish, implement and maintain a system for controlling production that:

• (a) includes processes and procedures that ensure that the aircraft, engine or propeller, and any part thereof, conforms with the applicable declared design data;

• (b) ensures that each statement of conformity (EASA Form 52B) or authorised release certificate (EASA Form 1) is only signed by authorised persons;

• (c) if flight tests are necessary within the scope of production, has processes in place that ensure that any flight tests are conducted in a safe manner;

• (d) ensures that the natural or legal person is in receipt of all the necessary airworthiness and environmental compatibility data to determine conformity;

• (e) has procedures in place that ensure that the airworthiness and environmental compatibility data is correctly incorporated in its production data, kept up to date and made available to all the personnel who need access to such data to perform their duties;

• (f) includes an inspection system that ensures that any aircraft, engine or propeller, and any part thereof, that are produced by the natural or legal person including their partners, or are supplied from or subcontracted to outside parties, conform with the applicable declared design data and are in a condition for safe operation;

• (g) includes an archiving system that records the requirements that have been placed on other organisations such as suppliers and subcontractors. The archived data shall be made available to the competent authority for continuing airworthiness purposes;

• (h) ensures that the maintenance of a newly manufactured aircraft is conducted in accordance with the applicable maintenance instructions and that the aircraft is kept in an airworthy condition, and if applicable, a certificate of release to service is issued for any maintenance that has been completed;

• (i) includes an internal occurrence reporting system in the interest of safety, to enable the collection and assessment of the occurrence reports collected in accordance with point 21L.A.3 in order to identify adverse trends or to address deficiencies, and to extract reportable occurrences. This system shall include the evaluation of relevant information relating to occurrences and the promulgation of the related information.

21L.A.274   Issuance of a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)

• (a) When issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1), the natural or legal person shall include all of the following:

• 1. a statement that the aircraft, engine or propeller, or any part thereof, conforms to the applicable declared design data and is in a condition for safe operation;

• 1. for each aircraft, a statement that the aircraft has been ground- and flight-checked;

• 1. for each engine or variable pitch propeller, a statement that the engine or variable pitch propeller has been subjected to a final functional test;

• 1. if applicable, a statement that the completed engine is in compliance with the applicable engine exhaust emissions requirements in force on the date of production of the engine.

• (b) The natural or legal person shall issue a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) upon:

• 1. the initial transfer of the ownership of the aircraft, engine or propeller, or parts thereof; or

• 1. for aircraft, the application for the issue of the restricted certificate of airworthiness for the aircraft.

21L.A.275   Obligations of a natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1)

The natural or legal person issuing a statement of conformity (EASA Form 52B) or an authorised release certificate (EASA Form 1) shall:

• (a) inform the competent authority that they intend to produce an aircraft, engine or propeller, or a part thereof, in conformity with the design data of a declaration of design compliance and that they will issue statements of conformity (EASA Form 52B) or authorised release certificates (EASA Form 1) in accordance with this Subpart;

• (b) ensure that the details of any completed work are recorded;

• (c) maintain, at the place of production, the technical data and drawings necessary to determine whether the aircraft, engine or propeller, or a part thereof, conforms to the applicable declared design data;

• (d) provide continuing airworthiness support to the declarant of a declaration of design compliance for any aircraft, engine or propeller, or a part thereof, that they have produced;

• (e) for new aircraft that they have produced, ensure that the aircraft is kept in an airworthy condition and that maintenance is performed, unless Regulation (EU) No 1321/2014 requires the maintenance to be performed under such rules, including any necessary repairs in accordance with the applicable design data prior to the issuance of an aircraft statement of conformity (EASA Form 52B);

• (f) when issuing a certificate of release to service after such maintenance, determine that each completed aircraft has been subjected to the necessary maintenance and is in a condition for safe operation, prior to issuing the certificate;

• (g) undertake the obligations of a natural or legal person issuing statements of conformity (EASA Form 52B) or authorised release certificates (EASA Form 1) of Subpart A of this Annex;

• (h) inform the competent authority about the cessation of their activities under this Subpart.

SECTION B

PROCEDURES FOR COMPETENT AUTHORITIES

SUBPART A –   GENERAL PROVISIONS

(reserved)

SUBPART B –   TYPE CERTIFICATES

21L.B.41   Certification specifications

The Agency, in accordance with Article 76(3) of Regulation (EU) 2018/1139, shall issue certification specifications and other detailed specifications, including certification specifications for airworthiness, and environmental compatibility that competent authorities, organisations and personnel may use to demonstrate the compliance of products and parts with the relevant essential requirements set out in Annexes II, IV and V to that Regulation, as well as with those for environmental protection set out in Article 9(2) of and Annex III to that Regulation. Such specifications shall be sufficiently detailed and specific to indicate to applicants the conditions under which certificates are to be issued, amended or supplemented.

21L.B.42   Initial investigation

• (a) Upon receiving an application for a type certificate under this Annex, the Agency shall verify whether the product is within the scope established in point 21L.A.21 and whether the applicant is eligible in accordance with point 21L.A.22 to apply for a type certificate for the product.

• (b) When the conditions of point (a) are not fulfilled, the Agency shall reject the application.

21L.B.43   Type-certification basis for a type certificate

• (a) The Agency shall establish the type-certification basis and notify it to the applicant. The type-certification basis shall consist of:

• 1. the certification specifications for airworthiness designated by the Agency from those applicable to the product at the date of application for that certificate, unless:

• (i) the applicant chooses to comply with certification specifications which became applicable after the date of the application; if an applicant chooses to comply with a certification specification which became applicable after the date of the application, the Agency shall include in the type-certification basis any other certification specification that is directly related; or

• (ii) the Agency accepts any alternative to a designated certification specification that cannot be complied with, for which compensating factors have been found that provide an equivalent level of safety; or

• (iii) the Agency accepts or prescribes other means that demonstrate compliance with the essential requirements of Annex II to Regulation (EU) 2018/1139;

• 1. any special condition prescribed by the Agency in accordance with point 21L.B.44(a).

• (b) The Agency may amend the type-certification basis at any point before the issuance of the type certificate if it has determined that experience from other similar products in service, or products that have similar design features, has shown that unsafe conditions may develop, and the type-certification basis that was established and notified to the applicant does not address this unsafe condition.

21L.B.44   Special conditions

• (a) The Agency shall prescribe special detailed technical specifications, named ‘special conditions’, for a product if the related certification specifications do not contain adequate or appropriate safety standards for the product because:

• 1. the product has novel or unusual design features relative to the design practices on which the applicable certification specifications are based;

• 1. the intended use of the product is unconventional; or

• 1. experience from other similar products in service or products having similar design features or newly identified hazards have shown that unsafe conditions may develop.

• (b) Special conditions contain such safety standards as the Agency finds necessary in order to establish a level of safety equivalent to that of the applicable certification specifications.

21L.B.45   Designation of the applicable environmental protection requirements for a type certificate

The Agency shall designate and notify to the applicant for a type certificate for an aircraft or for an engine, the applicable environmental requirements in accordance with point 21.B.85 of Annex I (Part 21).

21L.B.46   Investigation

Upon receiving an application for a type certificate under this Annex, the Agency shall:

• (a) conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis established in accordance with point 21L.B.43 and with the applicable environmental protection requirements designated in accordance with point 21L.B.45; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it;

• (b) when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan;

• (c) after receiving the declaration of compliance in accordance with point (f) of point 21L.A.25, conduct a physical inspection and assessment of the first article of that product in the final configuration, taking into consideration the critical design review carried out in accordance with point (a) of point 21L.B.242, in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements; the Agency shall verify the compliance of the product, considering the likelihood of an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product;

• (d) if during the establishment of the type-certification basis, designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan the Agency determines that the product design contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the product, the Agency shall determine which investigations are necessary in addition to those described in point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of any additional investigations and which elements of the design would be subject to those investigations.

21L.B.47   Issuance of a type certificate

• (a) The Agency shall issue without undue delay an aircraft, engine or propeller type certificate, provided that:

• 1. the applicant has complied with point 21L.A.27;

• 1. the Agency, through the investigation carried out pursuant to point 21L.B.46, has not found any non-compliance with the type-certification basis or with the applicable environmental protection requirements;

• 1. there are no unresolved issues from the investigation carried out pursuant to point (c) of point 21L.B.46 of that product in the final configuration;

• 1. no feature or characteristic has been identified that may make the product unsafe or environmentally incompatible for the uses for which the certification is requested.

• (b) The type certificate shall include:

• 1. the type design;

• 1. the operating limitations;

• 1. the instructions for continued airworthiness;

• 1. the type certificate data sheet for airworthiness and, if applicable, the record of engine exhaust emissions compliance;

• 1. the applicable type-certification basis and the applicable environmental protection requirements with which the Agency records compliance;

• 1. if applicable, the type certificate data sheet for noise; and

• 1. any other conditions or limitations prescribed for the product in the applicable type-certification basis and the applicable environmental protection requirements.

21L.B.48   Continuing airworthiness oversight of products for which a type certificate has been issued

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

21L.B.49   Transfer of a type certificate

• (a) When the Agency receives an application for verification of whether a type certificate can be transferred by its holder in accordance with point 21L.A.29 or when the Agency considers a request to adopt a type certificate in accordance with point 21L.A.29, the Agency shall verify corresponding to points 21L.B.42 and 21L.B.46 whether the transferee is eligible to be a type-certificate holder in accordance with point 21L.A.22 and is able to undertake the obligations of a type-certificate holder under point 21L.A.28.

• (b) When the Agency concludes that the conditions referred to in point (a) are met by the transferee, it shall inform the type-certificate holder or the natural or legal person requesting to adopt a type certificate that a transfer of the type certificate to that natural or legal person is accepted by the Agency.

SUBPART C –   DECLARATIONS OF DESIGN COMPLIANCE

21L.B.61   Detailed technical specifications and applicable environmental protection requirements for declarations of product design compliance

• (a) The Agency, in accordance with Article 76(3) of Regulation (EU) 2018/1139, shall establish and make available the detailed technical specifications that natural and legal persons can use to demonstrate compliance with the relevant essential requirements set out in Annex II to that Regulation when declaring compliance of the aircraft design in accordance with Subpart C of Section A of this Annex.

• (b) The detailed technical specifications referred to in point (a) shall provide design standards which reflect the state of the art and best design practices, and which build on the best available experience and scientific and technical progress, and on the best available evidence and analysis of aircraft design, for aircraft that are within the scope established under point 21L.A.41. These detailed technical specifications may include or refer to:

• 1. certification specifications established by the Agency in accordance with point 21.B.70 of Annex I (Part 21) for the airworthiness of the aircraft design;

• 1. special conditions that have been prescribed by the Agency in accordance with point 21.B.75 of Annex I (Part 21) or point 21L.B.44 for other aircraft and which are of a general nature;

• 1. detailed technical standards developed by standardisation and other industry bodies.

• (c) For the purposes of ensuring the environmental compatibility of the design, the Agency shall establish and make available the environmental protection requirements to be used as the basis for the declaration of design compliance, which shall include:

• 1. environmental protection requirements for the relevant product categories as contained in Annex 16 to the Convention on International Civil Aviation, Volumes I to III, at an amendment level referred to in Article 9(2) of Regulation (EU) 2018/1139; for this purpose, the references to:

• (i) the date of application for a type certificate contained in those volumes shall be understood as references to the date on which the declaration of design compliance is made by the declarant; and

• (ii) the certification requirements contained in those volumes shall be understood as requirements for the declaration of design compliance.

• 1. [reserved]

21L.B.62   Initial oversight investigation

• (a) Upon receiving a declaration of design compliance, the Agency shall verify that the aircraft is within the scope of Subpart C of Section A of this Annex and that the declaration contains all the information specified in point 21L.A.43. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant for that aircraft configuration.

• (b) The Agency shall conduct a physical inspection and assessment of the first article of that aircraft in the final configuration, taking into consideration the safety review carried out in accordance with point (a)(2) of point 21L.B.242. If the Agency finds evidence, in the declaration or through the physical inspection and assessment carried out in accordance with the first sentence, indicating that the aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21.

21L.B.63   Registration of a declaration of design compliance

The Agency shall register a declaration of design compliance for an aircraft provided that:

• (a) the declarant has declared compliance in accordance with point (a) of point 21L.A.43;

• (b) the declarant has provided to the Agency the documents required in accordance with point (c) of point 21L.A.43;

• (c) the declarant has made a commitment that the obligations in accordance with point 21L.A.47 will be undertaken;

• (d) there are no unresolved findings from the physical inspection and assessment of the first article of the aircraft in the final configuration carried out in accordance with point (b) of point 21L.B.62.

21L.B.64   Continuing airworthiness oversight of aircraft for which design compliance has been declared

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the applicable detailed technical specifications or the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

SUBPART D –   CHANGES TO TYPE CERTIFICATES

21L.B.81   Type-certification basis and applicable environmental protection requirements for a major change to a type certificate

• (a) The Agency shall establish the type-certification basis for a major change to a type certificate and notify it to the applicant.

• (b) For a major change to a type certificate and the areas affected by the change, the type-certification basis shall consist of the certification specifications incorporated by reference in the type certificate, unless:

• 1. the Agency finds that the certification specifications referenced in the type certificate do not provide adequate standards with respect to the proposed change, therefore the change and the areas affected by the change shall also comply with any special conditions, and amendments to those special conditions, prescribed by the Agency in accordance with point 21L.B.44, to provide a level of safety equivalent to that established by the certification specifications applicable on the date of the application for the change;

• 1. an applicant chooses to comply with a certification specification set out in an amendment that is applicable on the date of the application for the change.

• (c) The Agency shall designate the applicable environmental protection requirements for the major change to a type certificate in accordance with point 21.B.85 of Annex I (Part 21) and notify them to the applicant.

21L.B.82   Investigation and issuance of an approval of a minor change to a type certificate

• (a) Upon receiving an application for the approval of a minor change to a type certificate under this Annex, the Agency shall approve the minor change when:

• 1. the applicant has provided the substantiation data and justifications, and has demonstrated and declared the compliance of the change with the applicable type-certification basis and the applicable environmental protection requirements, or with the certification specifications chosen in accordance with point 21L.A.67;

• 1. the Agency, through its verification of the demonstration of compliance, taking into account the design features, complexity and overall criticality of the design or technology, as well as previous experience of design activities with the applicant, has not found:

• (i) any non-compliances with the type-certification basis or, where applicable, with the applicable environmental protection requirements, or with the certification specifications chosen;

• (ii) any feature or characteristic of the change that may make the changed product unsafe or environmentally incompatible for the uses for which certification is requested.

• (b) An approval of a minor change to a type certificate shall be limited to the specific configuration(s) in the type certificate to which the change relates.

21L.B.83   Investigation of a major change to a type certificate

Upon receiving an application for a major change to a type certificate under this Annex, the Agency shall:

• (a) conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.81; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it;

• (b) when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and also approve any subsequent updates of the compliance demonstration plan;

• (c) determine the likelihood of an unidentified non-compliance of the major change with the type-certification basis or with the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final changed configuration is necessary in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements, taking into consideration the critical design review if carried out in accordance with point (a)(3) of point 21L.B.242; the Agency shall notify the applicant before conducting this inspection and assessment;

• (d) if during the establishment of the type-certification basis, the designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan, the Agency determines that the design of the major change contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to investigation.

21L.B.84   Issuance of an approval of a major change to a type certificate

• (a) The Agency shall approve the major change when:

• 1. the applicant has demonstrated that the change and the areas affected by the change comply with the type-certification basis and the applicable environmental protection requirements, as established and designated by the Agency in accordance with point 21L.B.81;

• 1. the applicant has demonstrated and declared compliance in accordance with point (f) of point 21L.A.66;

• 1. the Agency through its verification of the demonstration of compliance has not found:

• (i) any non-compliances with the type-certification basis or, where applicable, with the applicable environmental protection requirements;

• (ii) any feature or characteristic of the change that may make the changed product unsafe or environmentally incompatible for the uses for which certification is requested.

• (b) An approval of a major change to a type certificate shall be limited to the specific configuration(s) in the type certificate to which the change relates.

21L.B.85   Continuing airworthiness oversight of changed products for which a type certificate has been issued

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements of a product for which a change to a type certificate has been approved, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

SUBPART E –   SUPPLEMENTAL TYPE CERTIFICATES

21L.B.101   Type-certification basis and applicable environmental protection requirements for a supplemental type certificate

• (a) The Agency shall establish the type-certification basis for a supplemental type certificate and notify it to the applicant.

• (b) For major changes to a type certificate in the form of a supplemental type certificate, the type-certification basis for the areas affected by the change shall be that which is incorporated by reference in the type certificate, unless:

• 1. the Agency finds that the certification specifications referenced in the type certificate do not provide adequate standards with respect to the proposed change, therefore the change and the areas affected by the change shall also comply with any special conditions, and amendments to those special conditions, prescribed by the Agency in accordance with point 21L.B.44, to provide a level of safety equivalent to that established by the certification specifications applicable on the date of the application for the change;

• 1. an applicant chooses to comply with a certification specification set out in an amendment that is applicable on the date of the application for the change.

• (c) The Agency shall designate the applicable environmental protection requirements for a major change to a type certificate in accordance with point 21.A.85 of Annex I (Part 21) and notify them to the applicant.

21L.B.102   Investigation

Upon receiving an application for a supplemental type certificate under this Annex, the Agency shall:

• (a) conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.101; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it;

• (b) when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan;

• (c) determine the likelihood of an unidentified non-compliance of the major change with the type-certification basis or the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final changed configuration is necessary in order to verify the compliance of the product with the applicable type-certification basis and the applicable environmental protection requirements, taking into consideration the critical design review if carried out in accordance with point (a) of point 21L.B.242; the Agency shall notify the applicant before conducting this inspection and assessment;

• (d) if during the establishment of the type-certification basis, the designation of the applicable environmental protection requirements or during the review of the compliance demonstration plan, the Agency determines that the major change to the design contains any element for which an unidentified non-compliance with the type-certification basis or the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to this investigation.

21L.B.103   Issuance of a supplemental type certificate

• (a) Upon receiving an application for a supplemental type certificate under this Annex, the Agency shall issue a supplemental type certificate when:

• 1. the applicant has demonstrated that the change and the areas affected by the change comply with the type-certification basis and the applicable environmental protection requirements, as established and designated by the Agency in accordance with point 21L.B.101;

• 1. the applicant has demonstrated and declared compliance in accordance with point (f) of point 21L.A.85;

• 1. the owner of the type-certificate data, if the applicant has specified in accordance with point (b)(2) of 21L.A.84 that the certification data has been provided on the basis of an arrangement with the owner of the type-certificate data, has:

• (i) no technical objection to the information submitted under point (a)(2) of point 21L.B.103; and

• (ii) agreed to collaborate with the holder of the repair design approval to discharge all the obligations for the continued airworthiness of the product with the repair design through compliance with point 21L.A.88;

• 1. the Agency, through its verification of the demonstration of compliance, has not found:

• (i) any non-compliances with the type-certification basis or, where applicable, the applicable environmental protection requirements;

• (ii) any feature or characteristic of the change that may make the changed product unsafe or environmentally incompatible for the uses for which certification is requested.

• (b) A supplemental type certificate shall be limited to the specific configuration(s) in the type certificate to which the related major change relates.

21L.B.104   Continuing airworthiness oversight of products for which a supplemental type certificate has been issued

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the type-certification basis or the applicable environmental protection requirements of a product for which a supplemental type certificate has been issued, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

SUBPART F –   CHANGES TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED

21L.B.121   Initial oversight investigation of a declaration of design compliance of a major change to the design of an aircraft for which design compliance has been declared

• (a) Upon receiving a declaration of design compliance for a major change to the design of an aircraft for which design compliance has been declared, the Agency shall verify that the change is within the scope of point 21L.A.101 and that the declaration contains all the information specified in point 21L.A.107. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant.

• (b) The Agency shall assess, based upon the risk of a non-compliance leading to a design that is not capable of safe flight or being environmentally incompatible, whether a physical inspection and assessment of the changed product is needed, and subsequently inform the declarant if that is the case. This assessment of the risk shall take into consideration:

• 1. the complexity of the major change and the overall effect on the aircraft structures, flight characteristics and systems;

• 1. previous experience of physical inspections of aircraft and major changes that have been designed by the declarant;

• 1. the response by the declarant to any previous findings that have been raised for non-compliances for the specific aircraft or similar aircraft designed by the declarant that have also been subject to a declaration of design compliance.

• (c) If the Agency finds evidence in the declaration, or through the physical inspection and assessment if carried out in accordance with point (b) of point 21L.B.121, indicating that the changed aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21.

21L.B.122   Registration of a declaration of design compliance for a major change to an aircraft design

• (a) The Agency shall register a declaration of design compliance for a major change to the design of an aircraft for which design compliance has been declared, provided that:

• 1. the declarant has declared compliance in accordance with point (a) of point 21L.A.107;

• 1. the declarant has provided to the Agency the documents required in accordance with point (d) of point 21L.A.107;

• 1. the declarant has made a commitment that the obligations in accordance with point 21L.A.47 will also be undertaken in respect of the changed aircraft design;

• 1. there are no unresolved issues from the physical inspection, if carried out in accordance with point (b) of point 21L.B.121.

• (b) The Agency shall only register a declaration of a major change to the design of an aircraft for which design compliance has been declared if it is limited to the specific configuration(s) in the registered declaration of design compliance to which the change relates.

21L.B.123   Continuing airworthiness oversight of a changed aircraft for which design compliance has been declared

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance with the applicable detailed technical specifications or the applicable environmental protection requirements of a change for which design compliance has been declared, the Agency shall act in accordance with point 21L.B.64.

SUBPART G –   DECLARED PRODCUTION ORGANISATIONS

(reserved)

SUBPART H –   CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS

(reserved)

SUBPART I –   NOISE CERTIFICATES

(reserved)

SUBPART J –   DECLARED DESIGN ORGANISATIONS

21L.B.181   Initial oversight investigation

• (a) Upon receiving a declaration from an organisation declaring their design capability, the Agency shall verify that:

• 1. the declarant is eligible to declare their design capability in accordance with point 21L.A.172;

• 1. the declaration contains all the information specified in point (c) of point 21L.A.173; and

• 1. the declaration does not contain information that indicates a non-compliance with the requirements of Subpart J of Section A of this Annex.

• (b) The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declared design organisation reference number to the declarant.

21L.B.182   Registration of a declaration of design capability

The Agency shall register the declaration of design capability on a suitable database, including the declared scope of work, provided that:

• (a) the declarant has declared their capability in accordance with point 21L.A.173;

• (b) the declarant has made a commitment that the obligations in accordance with point 21L.A.177 will be undertaken;

• (c) there are no unresolved issues in accordance with point 21L.B.181.

21L.B.183   Oversight

• (a) The Agency shall oversee the declared design organisation in order to verify the continuous compliance of the organisation with the applicable requirements of Section A.

• (b) The oversight shall include a product critical design review or physical inspection, and a first article inspection of every new design of the declared design organisation.

21L.B.184   Oversight programme

• (a) The Agency shall establish and maintain an oversight programme in order to ensure compliance with point 21L.B.183. The oversight programme shall take into account the specific nature of the organisation, the complexity of its activities and the results of past certification and/or oversight activities, and it shall be based on the assessment of the associated risks. It shall include, within each oversight planning cycle:

• 1. assessments, audits and inspections, including as appropriate:

• (i) management system assessments and process audits;

• (ii) product audits of a relevant sample of the design and certification of the products, and parts that are under the scope of the organisation;

• (iii) sampling of the work performed;

• (iv) unannounced inspections;

• 1. meetings convened between the head of the design organisation and the Agency to ensure that both remain informed of any significant issues.

• (b) The oversight programme shall include records of the dates when assessments, audits, inspections and meetings are due, and when assessments, audits, inspections and meetings have been effectively carried out.

• (c) An oversight planning cycle that does not exceed 24 months shall be applied.

• (d) Notwithstanding point (c), the oversight planning cycle may be extended to 36 months if the Agency has established that during the previous 24 months:

• 1. the organisation has demonstrated that it can effectively identify aviation safety hazards and manage the associated risks;

• 1. the organisation has continuously demonstrated compliance with point 21L.A.178 and that it has full control over all changes to the design management system;

• 1. no level 1 findings have been issued;

• 1. all corrective actions have been implemented within the time period that was accepted or extended by the Agency as defined in point 21L.B.21.

• (e) Notwithstanding point (c), the oversight planning cycle may be further extended to a maximum of 48 months if, in addition to the conditions provided in point (d), the organisation has established, and the Agency has approved, an effective continuous system for reporting to the Agency on the safety performance and regulatory compliance of the organisation itself.

• (f) The oversight planning cycle may be reduced if there is evidence that the safety performance of the organisation has decreased.

• (g) At the completion of each oversight planning cycle, the Agency shall issue a recommendation report on the continuation of the activities conducted by the declared design organisation based on its declaration of design capability, reflecting the results of the oversight.

21L.B.185   Oversight activities

• (a) When the Agency verifies the compliance of the declared design organisation in accordance with point 21L.B.183 and the oversight programme established in accordance with point 21L.B.184, it shall:

• 1. provide the personnel responsible for oversight with guidance to perform their functions;

• 1. conduct assessments, audits, inspections, and, if needed, unannounced inspections;

• 1. collect the evidence needed in case further action is required, including the measures provided for in point 21L.B.21 and 21L.B.22;

• 1. inform the declared design organisation about the results of the oversight activities.

• (b) The Agency shall collect and process any information deemed necessary for conducting oversight activities.

• (c) If the Agency detects a non-compliance of the declared design organisation with the applicable requirements of Section A, with a procedure or manual required by Section A, or with the declaration submitted, the Agency shall act in accordance with points 21L.B.21 and 21L.B.22.

21L.B.186   Changes to declarations

• (a) Upon receiving a notification of changes in accordance with point 21L.A.178, the Agency shall verify the completeness of the notification in accordance with point 21L.B.181.

• (b) The Agency shall update its oversight programme established according to point 21L.B.184 and investigate whether it is necessary to establish any conditions under which the organisation may operate during the change.

• (c) When the change affects any aspect of the declaration that is registered in accordance with point 21L.B.182, the Agency shall update the register.

• (d) Upon completion of the activities required by points (a) to (c), the Agency shall acknowledge the receipt of the notification to the declared design organisation.

SUBPART K –   PARTS

(Reserved)

SUBPART M –   DESIGN OF REPAIRS TO TYPE-CERTIFIED PRODUCTS

21L.B.201   Type-certification basis and applicable environmental protection requirements for a repair design approval

The Agency shall designate any amendments to the type-certification basis and the applicable environmental requirements incorporated by reference in, as applicable, either the type certificate or the supplemental type certificate, which the Agency considers necessary for maintaining a level of safety and environmental compatibility equal to that previously established and notify them to the applicant for the approval of a repair design.

21L.B.202   Investigation and issuance of an approval for a minor repair design

• (a) Upon receiving an application for the approval of a minor repair design to a type-certified product under this Annex, the Agency shall approve the minor repair design when:

• 1. the applicant has provided the substantiation data and justifications and has demonstrated and declared the compliance of the repair design with the applicable type-certification basis and the applicable environmental protection requirements established in accordance with point 21L.B.201;

• 1. the Agency, through its verification of the demonstration of compliance, taking into account the design features of the repair design, complexity and overall criticality of the repair design, as well as previous experience of design activities with the applicant, has not found:

• (i) any non-compliances with the type-certification basis or, where applicable, with the applicable environmental protection requirements;

• (ii) any feature or characteristic of the repair design that may make the product with the repair design unsafe for the uses for which certification is requested.

• (b) An approval of a minor repair design shall be limited to the specific configuration(s) in the type certificate to which the repair design relates.

21L.B.203   Investigation of an application for the approval of a major repair design

Upon receiving an application for the approval of a major repair design under this Annex, the Agency shall:

• (a) conduct a review of the initial compliance demonstration plan and any subsequent update provided by the applicant in order to establish the completeness of the plan and the appropriateness of the proposed means and methods of demonstrating compliance with the type-certification basis and the applicable environmental protection requirements established and designated in accordance with point 21L.B.201; if the compliance demonstration plan is incomplete or the means and methods are not appropriate to achieve compliance demonstration, the Agency shall inform the applicant and request an amendment of it;

• (b) when satisfied that the compliance demonstration plan provided is appropriate so that the applicant can demonstrate compliance, approve the compliance demonstration plan and any subsequent updates of the compliance demonstration plan;

• (c) determine the likelihood of an unidentified non-compliance of the major repair design with the type-certification basis or with the applicable environmental protection requirements, and the potential impact of that non-compliance on the safety or environmental compatibility of the product, and determine on that basis whether a physical inspection and assessment of the first article of that product in the final configuration with the repair design is necessary in order to verify the compliance of the product with the applicable type-certification basis; the Agency shall notify the applicant before conducting this inspection and assessment;

• (d) if, during the review of the compliance demonstration plan, the Agency determines that the major repair design contains any element for which an unidentified non-compliance with the type-certification basis or with the applicable environmental protection requirements may have an adverse impact on the safety or environmental compatibility of the changed product, the Agency shall determine which investigations are necessary in addition to those of point (c) in order to verify the compliance demonstration; the Agency shall notify the applicant of those additional investigations and which elements of the design would be subject to investigation.

21L.B.204   Issuance of an approval of a major repair design

• (a) Upon receiving an application for the approval of a major repair design to a type-certified product under this Annex, the Agency shall approve the major repair design when:

• 1. the applicant has been demonstrated that the repair design and the areas affected by the repair design comply with the type-certification basis and with the applicable environmental protection requirements, as established by the Agency in accordance with point 21L.B.201; and

• 1. the applicant has demonstrated and declared compliance in accordance with point 21L.A.208;

• 1. the owner of the type-certificate data, if the applicant has specified in accordance with point 21L.A.205(b)(5) that they provided the certification data on the basis of an arrangement with the owner of the type-certificate data, has:

• (i) no technical objection to the information submitted under point (a)(2) of point 21L.B.204; and

• (ii) agreed to collaborate with the holder of the repair design approval to discharge all the obligations for the continued airworthiness of the product with the repair design through compliance with point 21L.A.210;

• 1. the Agency, through its verification of the demonstration of compliance, has not found:

• (i) any non-compliances with the type-certification basis or, where applicable, the applicable environmental protection requirements;

• (ii) any feature or characteristic of the change that may make the product with the repair design unsafe for the uses for which certification is requested.

• (b) An approval of a major repair design shall be limited to the specific configuration(s) in the type certificate to which the repair design relates.

21L.B.205   Continuing airworthiness oversight of products for which a repair design has been approved

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means detects a non-compliance of a product, for which a repair design has been approved, with the type-certification basis or with the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

21L.B.206   Unrepaired damage

An evaluation of the airworthiness consequences shall be conducted by the Agency, when requested to do under point 21L.A.211, in the event that a damaged product is left unrepaired and is not covered by previously approved data. The Agency shall establish any limitations necessary to ensure a safe flight with the damaged product.

SUBPART N –   DESIGN OF REPAIRS TO AIRCRAFT FOR WHICH DESIGN COMPLIANCE HAS BEEN DECLARED

21L.B.221   Initial oversight investigation of a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared

• (a) Upon receiving a declaration of design compliance of a major repair design to an aircraft for which design compliance has been declared, the Agency shall verify that that the repair design is within the scope of point 21L.A.221 and that the declaration contains all the information specified in point 21L.A.226. The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant.

• (b) The Agency shall assess, based upon the risk of a non-compliance leading to a design that is not capable of safe flight or being environmentally incompatible, whether a physical inspection and assessment of the aircraft with the major repair design is needed, and subsequently inform the declarant if that is the case. This assessment of the risk shall take into consideration:

• 1. the complexity of the major repair design and the overall effect on the aircraft structures, flight characteristics and systems;

• 1. previous experience of physical inspections of aircraft and major repair designs and changes that have been designed by the declarant;

• 1. the response by the declarant to any previous findings that have been raised for non-compliances of the specific aircraft or similar aircraft designed by the declarant that have also been subject to a declaration of design compliance.

• (c) If the Agency finds evidence in the declaration, or through the physical inspection and assessment if carried out in accordance with point (b) of point 21L.B.221, indicating that the aircraft with the major repair design could be incapable of conducting a safe flight or could be environmentally incompatible during in-service operations, the Agency shall raise a finding in accordance with point 21L.B.21.

21L.B.222   Registration of a declaration of a major repair design to an aircraft for which design compliance has been declared

• (a) The Agency shall register a declaration of a major repair design to an aircraft for which design compliance has been declared provided that:

• 1. the declarant has declared compliance in accordance with point (a) of point 21L.A.226;

• 1. the declarant has provided to the Agency the documents required in accordance with point (d) of point 21L.A.226;

• 1. the declarant has made a commitment that the obligations in accordance with point 21L.A.228 will be undertaken;

• 1. there are no unresolved issues from the physical inspection, if carried out in accordance with point (b) of point 21L.B.221.

• (b) The Agency shall only register a declaration of a major repair design to an aircraft for which design compliance has been declared if it is limited to the specific configuration(s) in the registered declaration of design compliance to which the major repair design relates.

21L.B.223   Continuing airworthiness oversight of a repair design for which design compliance has been declared

If the Agency, through its continuing airworthiness oversight, including through reports received in accordance with point 21L.A.3, or by any other means, detects a non-compliance of a repair design, for which design compliance has been declared, with the applicable detailed technical specifications or with the applicable environmental protection requirements, the Agency shall raise a finding in accordance with point 21L.B.21, or issue an airworthiness directive under the conditions of point 21L.B.23.

SUBPART O –   EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS

(Reserved)

SUBPART P –   PERMIT TO FLY

(reserved)

SUBPART Q –   IDENTIFICATION OF PRODUCTS AND PARTS

SUBPART R –   STATEMENT OF CONFORMITY FOR AIRCRAFT AND AUTHORISED RELEASE CERTIFICATES (EASA FORM 1) FOR ENGINES AND PROPELLERS, AND PARTS THEREOF, THAT CONFORM TO A DECLARATION OF DESIGN COMPLIANCE

Appendices to ANNEX Ib (Part 21 Light)

EASA FORMS

When the Forms of this Annex are issued in a language other than English, they shall include an English translation.

The EASA (‘European Union Aviation Safety Agency’) Forms referred to in the appendices to this Part shall have the following obligatory features. Member States shall ensure that the EASA Forms they issue are recognisable and shall be responsible for having those Forms printed.

• Appendix I EASA Form 24B Restricted certificate of airworthiness

• Appendix II EASA Form 45B Restricted noise certificate

• Appendix III EASA Form 52B Aircraft statement of conformity

• Appendix IV EASA Form 53B Certificate of release to service

Appendix I

Restricted certificate of airworthiness – EASA Form 24B

Competent authority logo

RESTRICTED CERTIFICATE OF AIRWORTHINESS (DECLARED)

8	[Member State of registry] [COMPETENT AUTHORITY OF THE MEMBER STATE]	[Member State of registry] [COMPETENT AUTHORITY OF THE MEMBER STATE]	4
1. Nationality and registration marks	2. Manufacturer and manufacturer’s designation of aircraft	2. Manufacturer and manufacturer’s designation of aircraft	3. Aircraft serial number
4. Categories	4. Categories	4. Categories	4. Categories
5. This restricted certificate of airworthiness is issued pursuant to Article 18(2)(a) of Regulation (EU) 2018/1139 in respect of the above-mentioned aircraft which is considered to be airworthy when maintained and operated in accordance with the foregoing and the pertinent operating limitations. In addition to above, the following restriction applies: This restricted certificate of airworthiness is issued on the basis of a declaration of design compliance made in accordance with Regulation (EU) No 748/2012 and is valid and recognised in all EU Member States without further requirements or evaluation. This certificate does not comply with all of the applicable Standards of Annex 8 to the Convention on International Civil Aviation and therefore may not be valid for international air navigation over non-EU Member States, unless approved by the state(s) being overflown.	5. This restricted certificate of airworthiness is issued pursuant to Article 18(2)(a) of Regulation (EU) 2018/1139 in respect of the above-mentioned aircraft which is considered to be airworthy when maintained and operated in accordance with the foregoing and the pertinent operating limitations. In addition to above, the following restriction applies: This restricted certificate of airworthiness is issued on the basis of a declaration of design compliance made in accordance with Regulation (EU) No 748/2012 and is valid and recognised in all EU Member States without further requirements or evaluation. This certificate does not comply with all of the applicable Standards of Annex 8 to the Convention on International Civil Aviation and therefore may not be valid for international air navigation over non-EU Member States, unless approved by the state(s) being overflown.	5. This restricted certificate of airworthiness is issued pursuant to Article 18(2)(a) of Regulation (EU) 2018/1139 in respect of the above-mentioned aircraft which is considered to be airworthy when maintained and operated in accordance with the foregoing and the pertinent operating limitations. In addition to above, the following restriction applies: This restricted certificate of airworthiness is issued on the basis of a declaration of design compliance made in accordance with Regulation (EU) No 748/2012 and is valid and recognised in all EU Member States without further requirements or evaluation. This certificate does not comply with all of the applicable Standards of Annex 8 to the Convention on International Civil Aviation and therefore may not be valid for international air navigation over non-EU Member States, unless approved by the state(s) being overflown.	5. This restricted certificate of airworthiness is issued pursuant to Article 18(2)(a) of Regulation (EU) 2018/1139 in respect of the above-mentioned aircraft which is considered to be airworthy when maintained and operated in accordance with the foregoing and the pertinent operating limitations. In addition to above, the following restriction applies: This restricted certificate of airworthiness is issued on the basis of a declaration of design compliance made in accordance with Regulation (EU) No 748/2012 and is valid and recognised in all EU Member States without further requirements or evaluation. This certificate does not comply with all of the applicable Standards of Annex 8 to the Convention on International Civil Aviation and therefore may not be valid for international air navigation over non-EU Member States, unless approved by the state(s) being overflown.
Date of issue:	Date of issue:	Signature:	Signature:
6. This restricted certificate of airworthiness is valid unless revoked by the competent authority of the Member State of registry. A current airworthiness review certificate shall be attached to this certificate.	6. This restricted certificate of airworthiness is valid unless revoked by the competent authority of the Member State of registry. A current airworthiness review certificate shall be attached to this certificate.	6. This restricted certificate of airworthiness is valid unless revoked by the competent authority of the Member State of registry. A current airworthiness review certificate shall be attached to this certificate.	6. This restricted certificate of airworthiness is valid unless revoked by the competent authority of the Member State of registry. A current airworthiness review certificate shall be attached to this certificate.

EASA Form 24B – Issue 1

This certificate shall be carried on board during all flights.

Appendix II

Restricted noise certificate – EASA Form 45B