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

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Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Russian version):

200 business days

SKU:

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.

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