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NATO AEP-83 Ed: C Ver. 1:2023

Current

Current

The latest, up-to-date edition.

LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

24-10-2023

Publisher

NATO

Free

This document contains the minimum set of technical airworthiness requirements intended for the airworthiness certification of fixed-wing Light UAS with a maximum take-off weight not greater than 150 kg and an impact energy1 greater than 66 J (49 ft-lb) that intend to regularly operate in non-segregated airspace.

DocumentType
Standard
Pages
116
PublisherName
NATO
Status
Current
Supersedes

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