DEFSTAN 00-970(PT9)/9(2013) : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 9: REMOTELY PILOTED AIR SYSTEMS
English
01-01-2013
10-01-2014
Preface
SECTION 1 - GENERAL REQUIREMENTS
1.1 Introduction and Purpose
1.2 Applicability and Scope
1.3 Warning
1.4 Definitions
1.5 Normative References
SECTION 2 - FIXED WING - AIRWORTHINESS CODE
AND ACCEPTABLE MEANS OF COMPLIANCE (AMC)
(150 - 20,000kg)
Subpart A - General
Subpart B - UAV Flight
Subpart C - UAV Structure
Subpart D - UAV Design and Construction
Subpart E - UAV Powerplant
Subpart F - Equipment
Subpart G - Operating Limitations and Information
Subpart H - Command and Control Data Link
Subpart I - UAV Control Station
Appendix C - Basic Landing Conditions
Appendix D - Wheel spin-up Loads
Appendix F - Test Procedure for Self-Extinguishing Materials
Appendix G - Instructions for Continued Airworthiness
SECTION 3 - ROTARY WING - AIRWORTHINESS CODE AND ACCEPTABLE
MEANS OF COMPLIANCE (AMC) (150 - 3175kg) (To
be published)
SECTION 4 - LIGHT FIXED WING - AIRWORTHINESS CODE AND
ACCEPTABLE MEANS OF COMPLIANCE (AMC) (Sub
150 kg) (To be published)
SECTION 5 - LIGHT VERTICAL TAKE OFF AND LANDING (VTOL) -
AIRWORTHINESS CODE AND ACCEPTABLE MEANS OF
COMPLIANCE (AMC) (Sub 150 Kg) (To be published)
Specifies Design and Airworthiness guidance for both the contractor/designer and the MOD Project Team.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT9)/8(2012). (07/2013)
|
| DocumentType |
Standard
|
| Pages |
56
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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