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DEF STAN 00-970: V1 B2 P4

Revision I1, March 10, 1998

Complete Document

Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials

Includes all amendments and changes through Amendment 14, December 1994


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Product Details:

  • Revision: Revision I1, March 10, 1998
  • Published Date: December 1994
  • Status: Active, Most Current
  • Document Language: English
  • Published By: MODUK - British Defense Standards (MODUK)
  • Page Count: 230
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

GENERAL

In the detailed design of the aeroplane the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The design of parts and fittings shall be such as to facilitate their manufacture in quantity.

Components and items of equipment shall have at least the same factor as the main structure in all the appropriate stressing cases. Local loads at parts of attachment to the main structure shall be carefully considered to ensure that the main structure is not unduly weakened thereby.