ASTM WK41317

    New Specification for Structural Durability of Small Airplane

    (What is a Work Item?)

    Developed by Subcommittee: F44.30 | Committee F44 | Contact Staff Manager



    WK41317

    1. Scope

    This specfication requires that effects of fatigue loading must be considered where appropriate.


    Keywords

    structure, fatigue loading, general aviation, aircraft

    The title and scope are in draft form and are under development within this ASTM Committee.

    Citing ASTM Standards
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    Work Item Status

    Date Initiated:
    03-12-2013

    Technical Contact:
    Terry Ercolani

    Item:
    001

    Ballot:
    F44 (14-12)

    Status:
    In Balloting

    Item:
    005

    Ballot:
    F44 (14-07)

    Status:
    Withdrawn From Balloting