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MODUK - DEF STAN 00-970: PT 1: SEC 8

Design and Airworthiness Requirements for Service Aircraft Gas Turbine Auxiliary Power Units

inactive
Organization: MODUK
Publication Date: 1 December 1999
Status: inactive
Page Count: 11
scope:

PREFACE

This document provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated herein shall be applied by the Ministry of Defence (MoD) and the contractor as agreed and defined in the contract.

This document has been produced on behalf of the Defence Aviation Safety Board (DASB) by Airworthiness Design Requirements and Procedures (ADRP), Air/Land Technology Group (A/LTG), MoD Abbey Wood.

The appropriate Parts of this document are to be used, when called up in the Contract, for all future designs, and whenever practicable for amendments to existing designs. If any difficulty arises which prevents application of this document, ADRP shall be informed so that a remedy may be sought.

Any enquiries regarding this document in relation to an invitation to tender or a contract in which it is incorporated are to be addressed to the relevant MoD Project Director/Project Manager named in the invitation to tender or contract.

This document has been devised solely for the use of the MoD and its contractors in the execution of contracts for the MoD. To the extent permitted by law, the MoD hereby excludes all liability whatsoever and howsoever arising (including, but without limitation, liability resulting from negligence) for any loss or damage howsoever caused where the Document is used for any other purpose.

Document History

Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 8: Gas Turbine Auxiliary Power Unit Installation
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
January 10, 2014
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 8: Gas Turbine Auxiliary Power Unit Installation
INTRODUCTION This clause describes the tests that are required on the sources of auxiliary power fitted to an aeroplane (APU, EPU etc) to ensure satisfactory operation in Service. The tests are...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 8: Gas Turbine Auxiliary Power Unit Installation
PREFACE This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military operation....
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 8 Gas Turbine Auxiliary Power Unit Installation
INTRODUCTION This clause describes the tests that are required on the sources of auxiliary power fitted to an aeroplane (APU, EPU etc) to ensure satisfactory operation in Service. The tests are...
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 8 Gas Turbine Auxiliary Power Unit Installation
INTRODUCTION This clause describes the tests that are required on the sources of auxiliary power fitted to an aeroplane (APU, EPU etc) to ensure satisfactory operation in Service. The tests are...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 8 Gas Turbine Auxiliary Power Unit Installation
INTRODUCTION This clause describes the tests that are required on the sources of auxiliary power fitted to an aeroplane (APU, EPU etc) to ensure satisfactory operation in Service. The tests are...
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 8 - Gas Turbine Auxiliary Power Units
INTRODUCTION This clause describes the tests that are required on the sources of auxiliary power fitted to an aeroplane (APU, EPU etc) to ensure satisfactory operation in Service. The tests are...
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 8 - Gas Turbine Auxiliary Power Units
PREFACE This Standard provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated herein shall be applied...
DEF STAN 00-970: PT 1: SEC 8
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft Gas Turbine Auxiliary Power Units
PREFACE This document provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated herein shall be applied...
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