UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

MODUK - DEF STAN 00-970: PT7 SEC2

Design and Airworthiness Requirements for Service Aircraft Part 7 – Rotorcraft Section 2 STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT

active, Most Current
Buy Now
Organization: MODUK
Publication Date: 29 January 2010
Status: active
Page Count: 167
scope:

INTRODUCTION

The purpose of this Leaflet is to outline the basic principles underlying the strength and deformation requirements in this publication and, in particular, to show why these requirements are sometimes expressed in terms of proof loads, sometimes ultimate load, and sometimes both.

Document History

DEF STAN 00-970: PT7 SEC2
January 29, 2010
Design and Airworthiness Requirements for Service Aircraft Part 7 – Rotorcraft Section 2 STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT
INTRODUCTION The purpose of this Leaflet is to outline the basic principles underlying the strength and deformation requirements in this publication and, in particular, to show why these...

References

Advertisement