Flyg- och rymdteknik

This document applies to vertiports of class A (micro) as defined in ISO 5015-2 and defines the
requirements for constructing a vertiport. This scope excludes vertiport operations and services
covered by ISO 5015-2. developed by ISO/TC 20/SC 16 (UAS), which includes ground handling, interface
with Unmanned Aircraft System Traffic Management Service Providers, and safety and quality of
vertiport operators.

This document when used together with ISO 16119-1 specifies the requirements and the means for
verification of the design and performance of Unmanned Aerial Spraying Systems (UASS) mounted on
Unmanned Aircraft Systems (UAS) for application of Plant Protection Products (PPPs) in agriculture,
forestry, turf and amenity areas, with regard to minimising the potential risk of environmental
contamination during use, including misuse foreseeable by the UASS manufacturer.
The requirements of this part of ISO 23117 take precedence over those of ISO 16119-1. The ISO 23117
standard series does not cover human safety aspects of UASS’s or safety aspects concerning UAS’s,
remote pilots or bystanders.
This part of ISO 23117 is not applicable to UASSs manufactured before the date of its publication.

This standard provides a method for evaluating the resonance vibration frequency of multi-copter UA
only. The frequency of the rotor means the frequency within the operating frequency range, and the
frequency of the main body means the global mode frequency. This standard specifies a method to
avoid design of UA that the resonance occurs generated by the coincidence of the natural frequency of
the UA body and the rotational frequency of the rotor.
This standard relates to multi-copter UA weighing less than 150kg.

This standard specifies the composition, functional and performance requirements of payload interface for civil small and light unmanned aircraft system (hereinafter referred to as "UAS"), the maximum take-off mass ranged from 0.25 kg to 25 kg which applies to Level II through IV according to ISO 21895-6.
This standard is applicable to the design and manufacture of physical independent payload interface for an unmanned aircraft/UA, which connects an external payload to a UA.