NATO AEP-83 Ed: C Ver. 1:2023
Current
LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS
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.
| DocumentType |
Standard
|
| Pages |
116
|
| PublisherName |
NATO
|
| Status |
Current
|
| Supersedes |
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