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

Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 3 - Structure

inactive
Organization: MODUK
Publication Date: 31 January 2011
Status: inactive
Page Count: 335
scope:

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

Symmetric Manoeuvres

Asymmetric Manoeuvres

Gust Loads

High Lift Devices and Airbrakes

Pressure Cabins

Spinning and Spin Recovery

Control Systems

Active Control Systems

Strength for Ground Handling

Picketing

Lightning Protection

The section comprises the content of Def Stan 00-970 Issue 1 Chapters 200, 201, 202, 203, 204, 205, 206, 207, 208, 210, 308, 309, 604, 716, 732 and 1015. It is intended to provide information similar to that contained in JAR 25 Section C.

In the electronic version of this document, this line provides a link to Part 0.

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

References

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