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MODUK - DEF STAN 00-970: PT 1: SEC 3

Design and Airworthiness Requirements for Service Aircraft Structure

inactive
Organization: MODUK
Publication Date: 1 December 1999
Status: inactive
Page Count: 128
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), AdLand 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 fuhire 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 3: Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: Static Strength and Deformation Fatigue...
January 30, 2015
Design and Airworthiness Requirements for Service Aircraft - Part 1: Fixed Wing - Section 3: Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: Static Strength and Deformation Fatigue...
January 10, 2014
Design and Airworthiness Requirements for Service Aircraft - Part 1: Fixed Wing - Section 3: Structure
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...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 3: Structure
A description is not available for this item.
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 3 - Structure
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...
Design and Airworthiness Requirements for Service Aircraft Part 1 - Fixed Wing - Section 3 - Structure
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...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 3 - Structure
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 3 - Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: Static Strength and Deformation Fatigue...
February 5, 2010
Design and Airworthiness Requirements for Service Aircraft Part 1 – Fixed Wing Section 3 - Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Static Strength and Deformation Fatigue Symmetric Manoeuvres Asymmetric Manoeuvres Gust Loads High...
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 3 - Structure
INTRODUCTION  This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: The section comprises the content of DEF...
DEF STAN 00-970: PT 1: SEC 3
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft Structure
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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