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MODUK DEF STAN 00-970: PT 4: VOL 1 [ Active ]

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

standard by British Defence Standards , 03/10/1998

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Full Description

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.

 

 

Product Details

Edition:
I1
Published:
03/10/1998
Number of Pages:
230
File Size:
1 file , 5.2 MB
 

Document History

  1. MODUK DEF STAN 00-970: PT 4: VOL 1

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    viewing


    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

    • Most Recent

  2. MODUK DEF STAN 00-970: PT 4: VOL 1


    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

    • Historical Version

  3. MODUK DEF STAN 00-970: PT 4: VOL 1


    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

    • Historical Version

  4. MODUK DEF STAN 00-970: PT 4: VOL 1


    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

    • Historical Version