AEP-83 : 2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LIGHT UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS
English - French
24-11-2016
06-11-2023
1. Scope
2. Introduction
3. Type design airworthiness evidence
4. Source documents
5. Restricted Certification
6. Requirements
ANNEX A - Terms and Definitions
ANNEX B - Landing conditions for conventional landing gear
configurations (where applicable)
ANNEX C - Spark and compression ignition reciprocating engines
ANNEX D - Electric engines
ANNEX E - Turbine engines
ANNEX F - Propellers
ANNEX G - Hazard Reference System
ANNEX H - Stability and Response assessment guidance
ANNEX I - The Safety Management Plan
ANNEX J - Guidelines for airworthiness requirements applicable to
UA below the 66J impact energy
Includes 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.
| DocumentType |
Standard
|
| Pages |
104
|
| PublisherName |
NATO
|
| Status |
Superseded
|
| SupersededBy |
| STANAG 4671 : 2017 | UNMANNED AIRCRAFT SYSTEMS AIRWORTHINESS REQUIREMENTS (USAR) |
| DEFSTAN 00-56/1(1991) : 1991 | HAZARD ANALYSIS AND SAFETY CLASSIFICATION OF THE COMPUTER AND PROGRAMMABLE ELECTRONIC SYSTEM ELEMENTS OF DEFENCE EQUIPMENT |
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