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ISO 5286:2023

Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods

General information

Valid from 23.10.2023
Directives or regulations
None

Standard history

Status
Date
Type
Name
23.10.2023
Main
This document specifies the test requirements and methods for verifying the specified flight performance items of civil fixed-wing unmanned aircraft systems (UAS).
This document is applicable to the category of civil small and light fixed-wing UAS, which applies to maximum take-off mass (MTOM) level I through V according to ISO 21895.

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