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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
06-11-2023
English - French
24-11-2016
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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Superseded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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