Current status, proposed test evaluation, existing installations, and development of aircraft integral weight and balance systems (IWBS) as applied by Lockheed-Georgia Co, to cargo aircraft; testing, installation, and calibration procedures including related problems, errors, accuracy requirements, and system functions are described; military and operational requirements of C-130 aircraft, description of four proposed systems, Fairchild Controls (STAN System), National Water Lift (STOW System), Baldwin-Lima-Hamilton, and Electro Development Corp; details of C-5A IWBS system and its components, calibration procedures and problems.


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    Title :

    Integral weight and balance system applications on cargo aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1968 Freight



    Publication date :

    1968


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Integral Weight and Balance System Applications on Cargo Aircraft

    Tritton, Charles B. | SAE Technical Papers | 1968



    Weight and balance computer speeds cargo distribution

    Jakosky, M. | Engineering Index Backfile | 1944


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