AEMC INDIA L.L.P.

Reference Library

STANAG-4703(AEP-83):LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS

Edition B Version 1
NOVEMBER 2016

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 energy greater than 66 J (49 ft-lb) that intend to regularly operate in non-segregated airspace.

Download from NATO Website

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Notes:

  1. This is a Public Release Document issued and maintained by the respective agency.
  2. AEMC India LLP neither claims ownership nor responsibility for the downloaded resource.
  3. We have made it available in 'as is' condition for the sole purpose of wider circulation among the intended users.
  4. While we have made every effort to keep the version updated, users are advised to check the same from alternate sources.



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