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MODUK - DEF STAN 00-970: PART 9

Design and Airworthiness Requirements for Service Aircraft Part 9 UAV Systems

inactive
Organization: MODUK
Publication Date: 31 January 2011
Status: inactive
Page Count: 58
scope:

APPLICABILITY AND SCOPE

General

This Part of the Defence Standard has been written specifically to cover the design and airworthiness requirements for UAV Systems as defined in clause 1.3.

This Part of the Defence Standard does not differentiate between target drones, surveillance, stealth or combat UAV Systems that are, or have been, designed from the outset for operation without an on-board pilot. Neither does it give mandatory requirements for the method of control or launch to be used. These aspects shall be identified and covered in the appropriate UAV System Requirements Specification.

The operational role of the UAV System will determine its complexity and the safe guards needed to ensure that it is capable of performing its defined tasks safely.

Scope

The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy UAV Systems for all three UK Armed Services.

In addition to the mandatory requirements set out in this document, the airworthiness standards set out in NATO STANAG 4671 Unmanned Aerial Vehicles System Airworthiness Requirements (USAR) Edition 2 are also mandated, supplemented by the following UK national reservations.

UK national reservations:

 Amend USAR paragraph U50. Insert new paragraph U50(c) Demonstrate that there is adequate margin (e.g. 15%, to be agreed with the Certifying Authority) between Vs and Vmin FCS (i.e. to take account of gust) and that Vmin FCS is robust.

 Insert after USAR paragraph 201(ii).iii) VminDEMO to be equivalent to VminFCS

 Amend USAR paragraph AMC.1309(b). Insert the additional sentence at (5)(c)(i). more severe criteria may be needed for large aircraft; Insert the additional sub-paragraphs after (5)(c)(1).

 For large aircraft from 5,700kg up to 20,000kg MTOW (with the exception of propeller-driven twin-engine UAS, refer paragraph B). At UAV system level, the combination of all Catastrophic failure conditions is characterised by an occurrence of 10-6 per flying hour or less (with the calculation method subject to Certifying Authority agreement).

 For propeller-driven twin-engine UAS from 8,618kg up to 20,000kg MTOW, at UAV system level, the combination of all Catastrophic failure conditions is characterised by an occurrence of 10-6 per flying hour or less (with the calculation method subject to Certifying Authority agreement).

Document History

September 28, 2017
Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
(a) The mandatory requirements set out in this Standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services based on the requirements...
July 13, 2015
Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
a) The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services. (b) In addition to the...
January 30, 2015
Design and Airworthiness Requirements for Service Aircraft - Part 9: Remotely Piloted Air Systems
Aim This Part of the Defence Standard has been written to provide Design and Airworthiness guidance for both the contractor/designer and the MOD Project Team. It is not intended that it should...
January 10, 2014
Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services. In addition to the mandatory...
Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services. In addition to the mandatory...
July 20, 2012
Design and Airworthiness Requirements for Service Aircraft - Part 9 Remotely Piloted Air Systems
The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services. In addition to the mandatory...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 9 Remotely Piloted Air Systems
a. The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services. b. In addition to the...
DEF STAN 00-970: PART 9
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 9 UAV Systems
APPLICABILITY AND SCOPE General This Part of the Defence Standard has been written specifically to cover the design and airworthiness requirements for UAV Systems as defined in clause 1.3. This...
April 20, 2009
Design and Airworthiness Requirements for Service Aircraft Part 9 – UAV Systems
General a. In 1991, the Ministry of Defence (MOD), looking at its responsibilities for airworthiness, decided that it was necessary to define the design and airworthiness requirements for Unmanned...
January 27, 2006
Design and Airworthiness Requirements for Service Aircraft Part 9 – UAV Systems
The mandatory requirements set out in this standard are those basic requirements needed for the design and development of airworthy UAV Systems for all three UK Armed Services. b. At present this...
January 27, 2006
Design and Airworthiness Requirements for Service Aircraft Part 9 – UAV Systems
General a. In 1991, the Ministry of Defence (MOD), looking at its responsibilities for airworthiness, decided that it was necessary to define the design and airworthiness requirements for Unmanned...
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