Division 2 INSTALLATION AND MOUNTING CONDITIONSF1

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)

Test area:

The UA will be maintained above one reflecting (acoustically hard) plane. The UA shall be located at a sufficient distance from any reflecting wall or ceiling or any reflecting object so that the requirements given in Annex A of EN ISO 3744:2010 are satisfied on the measurement surface.

Sound measurement surface and microphone array:

The UA will be completely enclosed in a hemispherical measurement surface as par § 7.2.3 of EN ISO 3744:2010.

The number and position of the microphones is defined by Annex F of EN ISO 3744:2010.

The measurement surface shall have its origin at the point O lying in the ground plane directly below the UA.

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.