This paper covers inspection programs which will become a part of small airplane certification and operation as a result of Amendment 7 to FAR 23. Amendment 7 adds fatigue evaluation to wings and associated structure, reference paragraph 23.572.Paragraph 23.572 allows two basic methods of providing the required fatigue evaluation fatigue strength investigation or fail-safe strength investigation.The fail-safe strength investigation allows compliance with the regulations without running long and expensive fatigue analyses and/or tests but must be supplemented with proper inspections for complete FAR 23 compliance. Designing for inspectability and inspection methods will be covered.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Inspectability Criteria for Airframes Designed to Fatigue/Fail-Safe Requirements


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Business Aircraft Meeting and Engineering Display ; 1972



    Publication date :

    1972-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Implementation Analysis of Brake Inspectability Requirements

    A. L. Cross / W. Wakeley / O. J. Viergutz et al. | NTIS | 1979


    The Impact of Inspectability Requirements on Spacecraft Design

    Wannlund, Wallace R. | SAE Technical Papers | 1968



    Economic life criteria for metallic airframes

    MANNING, S. / SMITH, V. | AIAA | 1980


    Fatigue Management and Verification of Airframes

    A. F. Blom / H. Ansell | NTIS | 1994