Conclusion of this study include: (1) Avionics corrosion damage can be minimized on aircraft and other military equipment by a dynamic corrosion prevention/control program; (2) Detailed training of involved personnel must be provided; (3) As new material becomes available the occurrence of avionics corrosion can be reduced through a) designing boxes that will not leak and b) materials selection, i.e., non-corrosive materials for construction of component/equipment; (4) Close cooperation between the avionics/aerospace community is needed to insure that the most durable, reliable/avionics/electronics are provided to the armed forces.


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    Titel :

    US Naval Air Force Avionic and Electrical System Corrosion Prevention and Control Maintenance


    Beteiligte:
    G. T. Browne (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design guidelines for avionic corrosion prevention and control

    Carrato, A.F. / DeLong, G.E. / Shaffar, I.S. | Tema Archiv | 1981


    Design guidelines for avionic corrosion prevention and control

    Carrato, A.F. / Delong, G.E. / Shaffer, I.S. | Tema Archiv | 1982


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987