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.
Integral weight and balance system applications on cargo aircraft
SAE -- Paper
SAE Meeting ; 1968 Freight
1968
9 pages
Aufsatz (Konferenz)
Englisch
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