Division 3 OPERATING CONDITIONS DURING TESTF1

United Kingdom

Changes not yet applied. Later legislation changes this provision in ways not yet written into the text below:

Annex Pt. 2 point (12A) inserted by Unmanned Aircraft 2025 reg. 9(2)
Annex Pt. 3 point (14A) inserted by Unmanned Aircraft 2025 reg. 10(2)
Annex Pt. 4 point (9A) inserted by Unmanned Aircraft 2025 reg. 11(2)
Annex Pt. 5 point (4)(a) word omitted by Unmanned Aircraft 2025 reg. 12(2)(a)
Annex Pt. 5 point (4)(a) words inserted by Unmanned Aircraft 2025 reg. 12(2)(b)
Annex Pt. 1 point (7A)-(7D) inserted by Unmanned Aircraft 2025 reg. 8(2)
Annex Pt. 1 point (8)(a) word omitted by Unmanned Aircraft 2025 reg. 8(3)(a)
Annex Pt. 1 point (8)(a) words inserted by Unmanned Aircraft 2025 reg. 8(3)(b)
Annex Pt. 5 point (3A)(3B) inserted by Unmanned Aircraft 2025 reg. 12(1)

The noise tests shall be carried out with the UA’s rotors operating at a speed corresponding to the hovering of the UA under MTOM.

If the UA is placed on the market with accessories that can be fitted to it, it will be tested with and without these accessories in all possible UA configurations.

Annotations

Textual amendments

F1: Substituted by Commission Delegated Regulation (EU) 2020/1058 of 27 April 2020 amending Delegated Regulation (EU) 2019/945 as regards the introduction of two new unmanned aircraft systems classes.