21.A.130 Statement of conformity

• Regulation (EU) 2021/1088 found in: Initial Airworthiness and Environmental Protection (No 748/2012) Part-21 Part-21L (Jul 2024)

21.A.130 Statement of conformity Regulation (EU) 2021/1088 (a)     Each manufacturer of a product, part or appliance manufactured under this Subpart shall raise a statement of conformity, an [EASA Form 52](#_DxCrossRefBm1649096923) (see [Appendix VIII](#_DxCrossRefBm1649096923)), for complete aircraft, or [EASA Form 1](#_DxCrossRefBm1649096870) (see [Appendix I](#_DxCrossRefBm1649097171)), for other products, parts or appliances. This statement shall be signed by an authorised person who holds a responsible position in the manufacturing organisation. (b)     A statement of conformity shall include all of the below: 1.       for each product, part or appliance, a statement that the product, part or appliance conforms to the approved design data and is in condition for safe operation; 2.       for each aircraft, a statement that the aircraft has been ground- and flight-checked in accordance with point [21.A.127](#_DxCrossRefBm1649097129)(a); 3.       for each engine, or variable pitch propeller, a statement that the engine or variable pitch propeller has been subjected by the manufacturer to a final functional test in accordance with point [21.A.128](#_DxCrossRefBm1649097128); 4.       additionally, in the case of environmental protection requirements: (i)      a statement that the completed engine is in compliance with the applicable engine exhaust emissions requirements on the date of manufacture of the engine, and (ii)     a statement that the completed aeroplane is in compliance with the applicable CO2 emissions requirements on the date its first certificate of airworthiness is issued. (c)      Each manufacturer of such a product, part or appliance shall: 1.       upon the initial transfer by it of the ownership of such a product, part or appliance; or 2.       upon application for the original issue of an aircraft certificate of airworthiness; or 3.       upon application for the original issue of an airworthiness release document for an engine, a propeller, a part or appliance, present a current statement of conformity, for validation by the competent authority. (d)     The competent authority shall validate by counter-signature the statement of conformity if it finds after inspection that the product, part or appliance conforms to the applicable design data and is in condition for safe operation.