(3)

in Part A, Category VII (Aerospace and Propulsion), the following sections are inserted: ‘X.A.VII.004 | Servomotors having a torque-to-weight ratio equal or higher than 0,16. Technical Note: The torque-to-weight ratio is computed considering the torque in kgf*cm and the weight in g. X.A.VII.005 | Launch systems for unmanned aerial vehicles (UAVs), and parts thereof, other than those specified in the CML or in Regulation (EU) 2021/821. X.A.VII.006 | Ground support equipment for unmanned aerial vehicles (UAVs). X.A.VII.007 | ‘Flight termination’ systems and specially designed components therefor. Note: This control covers digital and analogue communications standards for ‘Flight termination’ systems, including encrypted operational modes. Technical Notes: 1. For the purpose of this control, ‘flight termination’ can involve a controlled descent, self-destruction of the UAV or missile, or detonation of the warhead to minimise the risk of collateral damage. 2. For the purpose of this control, components include ground and on-board equipment, command exciters, encoders, amplifier controllers, command verification receivers, amplifiers, transmitters, decoders and receivers. X.D.VII.003 | “Software”, for the “use” of equipment controlled by X.A.VII.006 or X.A.VII.007.’.

← anx_II__point_2__table__3 · All articles · anx_II__point_3__table →

Source: EUR-Lex (Cellar) · retrieved 2026-10-14 · Text as adopted (Official Journal); later amendments are not incorporated in this text.