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Appendix B to GM 21L.A.63 Classification of changes to a type certificate

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

AppendixAppendix

Appendix B to GM 21L.A.63Classification of changes to a type certificate

The following tables provide examples of ‘substantial’ changes. The classification may change due to cumulative effects and/or combinations of individual changes. A.1 Examples of ‘substantial’ changes for small aeroplanes (CS-23) A.1.1 Table A-1 contains examples of changes that are ‘substantial’ for small aeroplanes (CS-23).

Table A-1 — Examples of ‘substantial’ changes for small aeroplanes (CS-23)

ExampleDescription of changeNotes
1.Change to wing location (tandem, forward, canard, high/low).Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
2.Fixed wing to tilt wing.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
3.A change to the number of engines.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
4.Replacement of piston or turboprop engines with turbojet or turbofan engines.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
5.Change to engine configuration (tractor/pusher).Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
6.Change from an all-metal to all-composite aeroplane.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.

A.2 Examples of ‘substantial’ changes for rotorcraft (CS-27) A.2.1 Table A-2 contains examples of changes that are ‘substantial’ for rotorcraft (CS-27).

Table A-2 — Examples of ‘substantial’ changes for rotorcraft (CS-27)

ExampleDescription of changeNotes
1.Change to the number and/or configuration of rotors (e.g. main and tail rotor system to two main rotors).Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.
2.Change from an all-metal rotorcraft to all-composite rotorcraft.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.

A.3 Examples of ‘substantial’ changes for propellers (CS-P) A.3.1 Table A-3 contains an example of a change that is ‘substantial’ for propellers (CS-P).

Table A-3 — Example of a ‘substantial’ change for propellers (CS-P)

ExampleDescription of changeNotes
1.Change to the number of blades.Proposed change to the design is so extensive that a substantially complete investigation of compliance with the applicable type-certification basis is required.

APPENDIX · Appendix B to GM 21L.A.63 — 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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