Navigate / EASA
Appendix B to point 21L.A.103 Classification of changes to the design of an aircraft for which design compliance has been declared

ED Decision 2023/013/R

The following tables provide examples of ā€˜substantial’ changes. The classification may change due to cumulative effects and/or combinations of individual changes.

A.1 Examples of ā€˜substantial’ changes for small aeroplanes (CS‑23)

A.1.1 Table A‑1 contains examples of changes that are ā€˜substantial’ for small aeroplanes (CS‑23).



Table A-1 — Examples of when a new declaration of design compliance would be required under Subpart C for substantial changes for small aeroplanes (CS‑23)

Example

Description of change

Notes

1.

Change to wing location (tandem, forward, canard, high/low).

Proposed change to the design is so extensive that a substantially complete demonstration of compliance with the applicable detailed technical specifications is required.

2.

Change to engine configuration (tractor/pusher).

Proposed change to the design is so extensive that a substantially complete demonstration of compliance with the applicable detailed technical specifications is required.

3.

Change from an all-metal to all-composite aeroplane.

Proposed change to the design is so extensive that a substantially complete demonstration of compliance with the applicable detailed technical specifications is required.