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MODUK - DEF STAN 00-970: PT 1: SEC 7

Design and Airworthiness Requirements for Service Aircraft Part 1 Section 7 - Operating Limitations and Information

inactive
Organization: MODUK
Publication Date: 31 January 2007
Status: inactive
Page Count: 64
scope:

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 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 standard has been agreed by the authorities concerned with its use and is intended to be used whenever relevant in all future designs, contracts, orders etc. and whenever practicable by amendment to those already in existence. If any difficulty arises which prevents application of the Defence Standard, the Directorate of Standardization (DStan) shall be informed so that a remedy may be sought.

Any enquiries regarding this standard in relation to an invitation to tender or a contract in which it is incorporated are to be addressed to the responsible technical or supervising authority named in the invitation to tender or contract.

 Compliance with this Defence Standard shall not in itself relieve any person from any legal obligations imposed upon them.

This standard 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 7: Operating Limitations and Information
INTRODUCTION This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information
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 7: Operating Limitations and Information
INTRODUCTION  This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information
A description is not available for this item.
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 Operating Limitations and Information
INTRODUCTION This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 7 Operating Limitations and Information
INTRODUCTION  This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 Operating Limitations and Information
PREFACE a. This Part of the Defence Standard provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated...
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 - Operating Limitations and Information
INTRODUCTION This chapter specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
DEF STAN 00-970: PT 1: SEC 7
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 7 - Operating Limitations and Information
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...
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft Operating Limitations and Information
INTRODUCTION This chapter specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...

References

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