The V-22 avionic hardware is the first to be designed under MIL-STD-2165 testability program requirements. This paper presents an overview of the avionics design-for-testability approach and lessons learned to date relative to the application of MIL-STD-2165. The paper will discuss incorporation of testability requirements up front in the avionics design which will drive the supportability philosophy at both the Organizational and Depot levels of maintenance. The paper will compare previous avionics hardware testability requirements versus those applied to the V-22 avionics and highlight areas of improvement. A discussion of testability design impacts on reduced level of testing (i.e. WRA/SRA/System) will be included. In addition, the paper discusses an innovative approach to meeting the user requirements for a man-portable forward deployed maintenance capability that forms the basis for a two level support scenario (Organizational and Depot). The innovation comes from the fact that the on-board Central Integrated Checkout system will provide data as well as fault isolation and will use this data as a mechanism to reduce the size and complexity of the stimulus and measurement hardware at either the Organizational or Depot level depending on the deployment requirements.


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    Title :

    V-22 osprey aircraft application of MIL-STD-2165 testability specification


    Additional title:

    Spezifikation der Prueffaehigkeit nach MIL-STD-2165 und die Anwendung auf das V-22-Programm in der Avionik


    Contributors:
    Croke, D. (author) / Brameyer, J. (author) / Thom, J.K. (author)


    Publication date :

    1986


    Size :

    4 Seiten, 2 Bilder


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Designing to MIL-STD-2165: Testability

    Croke, Don / Brameyer, Jan / Thom, Jet K. | IEEE | 1987



    Nr. 2165

    DataCite | 1887


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