Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
Article 2 Certification of products, parts, appliances, control and monitoring unit and control and monitoring unit components
Available versions for ERULES-1963177438-3625
Regulation (EU) 2022/1358
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
Regulation (EU) 2024/1108
found in: Initial Airworthiness and Environmental Protection (748/2012) (Nov 2025)
From
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
From section
To
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
Article 2 Certification of products, parts and appliances Regulation (EU) 2022/1358 1. Products, parts and appliances shall be issued certificates as specified in [Annex I](#_DxCrossRefBm1649096844) (Part 21) 2. By way of derogation from paragraph 1 of this Article, certificates may be alternatively issued as specified in [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light) for the following products: (a) an aeroplane with a maximum take-off mass (MTOM) of 2 000 kg or less and a maximum operational seating configuration of four persons; (b) a sailplane or powered sailplane of 2 000 kg MTOM or less; (c) a balloon; (d) a hot air airship; (e) a passenger gas airship designed for not more than four persons; (f) a rotorcraft of 1 200 kg MTOM or less and a maximum operational seating configuration of four persons; (g) a piston engine or fixed pitch propeller that is intended to be installed on an aircraft referred to in points (a) to (f); or (h) a gyroplane. 3. By way of derogation from paragraphs 1 and 2 of this Article, a declaration of design compliance may alternatively be made, as specified in [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light), for the following products: (a) an aeroplane of 1 200 kg MTOM or less that is not jet-powered and with a maximum operational seating configuration of two persons; (b) a sailplane or a powered sailplane of 1 200 kg MTOM or less; (c) a balloon designed for not more than four persons; (d) a hot air airship designed for not more than four persons. 4. By way of derogation from paragraphs 1 to 3 of this Article, 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 Section A of [Annex I](#_DxCrossRefBm1649096844) (Part 21) and Subparts H and I of Section A of [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light). They shall also be exempted from the provisions of Subpart P of Section A of [Annex I](#_DxCrossRefBm1649096844) (Part 21) and Subpart P of Section A of [Annex Ib](#_DxCrossRefBm1649096843) (Part 21 Light), except where aircraft identification marks are prescribed by a Member State.
## Article 2 Certification of products, parts, appliances, control and monitoring unit and control and monitoring unit components *Regulation (EU) 2024/1108* 1. Products, parts, appliances, control and monitoring units and control and monitoring unit components shall be issued with certificates as specified in [Annex I](#_DxCrossRefBm485230334) (Part 21) 2. By way of derogation from paragraph 1, certificates may be alternatively issued as specified in [Annex I (b)](#_DxCrossRefBm485230333) (Part 21 Light) for the following products other than unmanned aircraft: (a) an aeroplane with a maximum take-off mass (MTOM) of 2 000 kg or less and a maximum operational seating configuration of four persons; (b) a sailplane or powered sailplane of 2 000 kg MTOM or less; (c) a balloon; (d) a hot air airship; (e) a passenger gas airship designed for not more than four persons; (f) a rotorcraft of 1 200 kg MTOM or less and a maximum operational seating configuration of four persons; (g) a piston engine or fixed pitch propeller that is intended to be installed on an aircraft referred to in points (a) to (f); or (h) a gyroplane. 3. By way of derogation from paragraphs 1 and 2, a declaration of design compliance may alternatively be made, as specified in [Annex Ib](#_DxCrossRefBm485230333) (Part 21 Light), for the following products other than unmanned aircraft: (a) an aeroplane of 1 200 kg MTOM or less that is not jet-powered and with a maximum operational seating configuration of two persons; (b) a sailplane or a powered sailplane of 1 200 kg MTOM or less; (c) a balloon designed for not more than four persons; (d) a hot air airship designed for not more than four persons. 4. By way of derogation from paragraphs 1 to 3 of this Article, 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 Section A of [Annex I](#_DxCrossRefBm485230334) (Part 21) and Subparts H and I of Section A of [Annex Ib](#_DxCrossRefBm485230333) (Part 21 Light). They shall also be exempted from the provisions of Subpart P of Section A of [Annex I](#_DxCrossRefBm485230334) (Part 21) and Subpart P of Section A of [Annex Ib](#_DxCrossRefBm485230333) (Part 21 Light), except where aircraft identification marks are prescribed by a Member State.