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21L.A.21 Scope

Annex Ib · Regulation (EU) No 748/2012 · EAR revision 27 Nov 2025

IRImplementing rule

21L.A.21Scope

This Subpart establishes the procedure for applying for type certificates, and establishes the rights and obligations of the applicants for, and holders of, those certificates for products, when the product is one of the following:

(a)an aeroplane with a maximum take-off mass (MTOM) of 2 000 kg or less with a seating configuration of maximum four persons;

(b)a sailplane or powered sailplane with an MTOM of 2 000 kg 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 with an MTOM of 1 200 kg or less with a seating configuration of maximum four persons;

(g)a piston engine and fixed pitch propeller that are intended to be installed on an aircraft referred to in points (a) to (f). In such cases, the type certificate data sheet shall be appropriately annotated to only permit installation of the engine or propeller on such aircraft;

(h)gyroplanes.

IR · 21L.A.21 — Regulation (EU) No 748/2012 · Regulation (EU) 2022/1358 · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21L.A.21Scope

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A type certificate (TC) that is issued under Subpart B of Annex I (Part 21) has the same validity as a TC that is issued under Subpart B of Annex Ib (Part 21 Light). However, the eligibility for design organisations is different (e.g. declared design organisations using Subpart J of Annex Ib are permitted to apply for a TC), and also the means of verifying compliance is different. In addition, the production organisation requirements are also different, and organisations are permitted to become declared production organisations using Subpart G of Annex Ib (Part 21 Light) and produce products and parts within the scope of point 21L.A.21. As per point 21L.A.23(b), an organisation that holds a design organisation approval (DOA) issued under Subpart J of Annex I (Part 21) meets the eligibility criteria of Subpart B of Annex Ib (Part 21 Light). Such organisations may use the privileges that are granted under that approval (as per points (2), (5) and (8) of point 21.A.263(c) of Annex I (Part 21)) and further described in points 21L.A.69(a) and 21L.A.209(a) of Annex Ib (Part 21 Light). Furthermore, an organisation that holds a production organisation approval (POA) issued under Subpart G of Annex I (Part 21) is permitted to use that approval to release products and parts within the scope of Subpart B of Annex Ib (Part 21 Light), and use the privileges that are granted under that approval (as per point 21.A.163(b) of Annex I (Part 21)) and further described under points 21L.A.143(c)(1)(ii) and 21L.A.163(c)(1)(i)(C) of Annex Ib (Part 21 Light).

GM · GM1 21L.A.21 — Regulation (EU) No 748/2012 · ED Decision 2023/013/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

All rules in SECTION A - TECHNICAL REQUIREMENTS

Consolidated from the EASA Easy Access Rules (revision 27 Nov 2025, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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