AEMC INDIA L.L.P.

Reference Library

STANAG-4702(AEP-80):ROTARY WING UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS

Edition B Version 1

NOVEMBER 2016

This document contains a set of technical airworthiness requirements intended for the airworthiness certification of Rotary-Wing Military UAV Systems with a maximum take-off weight between 150 and 3175 kg 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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