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MODUK - DEF STAN 00-970: V1 B2 P4

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

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Organization: MODUK
Publication Date: 1 October 1992
Status: active
Page Count: 218
scope:

GENERAL

In the detailed design of the aeroplane the variety of materials and parts to 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 factors 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.

Document History

March 10, 1998
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
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....
December 1, 1994
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
This Standard has been devised for the use of the Crown and of its contractors in the execution of contracts for the Crown and, subject to the unfair Contract Terms Act 1977, the Crown will not be...
DEF STAN 00-970: V1 B2 P4
October 1, 1992
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
GENERAL In the detailed design of the aeroplane the variety of materials and parts to be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The...
December 1, 1991
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
This Standard has been devised for the use of the Crown and of its contractors in the execution of contracts for the Crown and, subject to the unfair Contract Terms Act 1977, the Crown will not be...
November 1, 1990
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
INTRODUCTION The requirements of this chapter are applicable to the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems...

References

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