Name: AEP-80 : 2016
Brand: NATO

ROTARY WING UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

24-11-2016

Publisher

NATO

1. AIM
2. SCOPE, DERIVATION AND STRUCTURE OF
   USAR-RW
3. USAR-RW STRUCTURE
4. TYPE CERTIFICATION (OR EQUIVALENT)
   PROCESS
5. SPECIAL CONDITIONS & SPECIAL MILITARY
   AIRWORTHINESS REQUIREMENTS
6. SPECIAL MILITARY MODES OF OPERATION
   RESULTING IN REDUCTION OF LEVEL OF SAFETY
7. CROSS-REFERENCE TABLE WITH EASA CS-27
   AMENDMENT 2 FOR PARAGRAPHS TOTALLY OR
   PARTIALLY TRANSFERRED TO SUBPART 1
USAR-RW LEXICON
BOOK 1 - AIRWORTHINESS CODE
BOOK 2 - ACCEPTABLE MEANS OF COMPLIANCE (AMC)

Purpose of this document is to correspond as closely as practicable to a comparable minimum level of airworthiness for rotary-wing aircraft as embodied in documents such as EASA CS-27 amendment 2 (from which it is derived) whilst recognizing that there are certain unique features of rotorcraft UAV Systems that require particular additional requirements or Subparts.