MODUK - DEF STAN 00-970: PT 1: SEC 3
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 3 - Structure
| 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.
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