NATO AEP-83 Ed: C Ver. 1:2023
Current
The latest, up-to-date edition.
LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS
Hardcopy , PDF
English
10-24-2023
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.
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