MODUK - DEF STAN 00-970: PT 1: SEC 3
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 3 - Structure
inactive
| Organization: | MODUK |
| Publication Date: | 31 January 2007 |
| Status: | inactive |
| Page Count: | 296 |
scope:
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 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 provided information similar to that contained in JAR 25 Section
In the electronic version of this document, this line provides a link to Part 0.
Document History
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...
July 5, 2013
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 3: Structure
A description is not available for this item.
January 7, 2013
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...
July 20, 2012
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...
DEF STAN 00-970: PT 1: SEC 3
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...