DANSK DSF/ISO/DIS 21384-2 PDF

This International Standard specifies requirements for ensuring the quality and safety of the design and manufacture of unmanned aircraft systems (UAS) that include unmanned aircraft (UA) with lifting devices that are fixed primary wing structures, rotating components of vertical lifting elements, or both. This standard does not cover technical requirements for the design and manufacturing for UAS components. This standard does not include equipment considerations unique to comply with UA traffic management systems. Additional equipment not addressed by this standard may be required. Manufactures should apply requirements where the standard would be applicable to the reasonable expected use of the UAS. The standard is intended for: a) UAS designed for use where a State aviation authority has determined a certificate of airworthiness (C of A) is not required; or b) Where a C of A is required, to complement technical standards published by the aviation authority for the purposes of building the certification basis; or c) As Alternative Means of Compliance if acceptable to the aviation authority.