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MODUK - DEF STAN 00-970: PT1 SEC3

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

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Organization: MODUK
Publication Date: 13 July 2015
Status: active
Page Count: 323
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 is intended to provide information similar to that contained in CS 25 Section C.

Document History

DEF STAN 00-970: PT1 SEC3
July 13, 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 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...
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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