lexiara

anx_IX__cpt_1__cpt_2__cpt_1__cpt_5__text_2

Text with EEA relevance.

Unmanned aircraft and their engines, propellers, parts, non-installed equipment, and equipment to control the unmanned aircraft remotely, considered separately and in relation to each other, must be designed such that the probability of a failure condition and the severity of its effect on people on the ground and other airspace users are mitigated on the basis of the principles laid down in Article 4(2).

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Source: EUR-Lex (Cellar) · retrieved 2026-10-12 · Text as adopted (Official Journal); later amendments are not incorporated in this text.