DEFSTAN 00-970(PT9)/9(2013) : 2013

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.