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Pan American Operational Experience with STAN
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1968 by SAE International in United States
Annotation ability available
Event: Space Technology Conference
STAN is the on-board weight and balance system presently used by Pan American on its cargo aircraft. Based on 1-1/2 years of operational experience as a secondary or check system to the weight and balance manifest, STAN has substantially justified itself through its accuracy and reliability. Its success suggests the feasability of developing a primary weight and balance system, which would be of significant value, especially on the forthcoming supersonic and jumbo jets.
CitationHart, R. and Erickson, J., "Pan American Operational Experience with STAN," SAE Technical Paper 680355, 1968, https://doi.org/10.4271/680355.
- Frese, V. “Determination of Actual Airplane Take-off Weight and C. G. Position by Cockpit Instrumentation.” Pan American World Airways, OE-1-63, July 1, 1963.
- Frese, V. “B707-300C Aircraft Take-off Weight and % MAC by Means of Cockpit Instrumentation,” Pan American World Airways, OE-1-65, July 1, 1965.
- De Pietto, A. “Statistical Survey for Operational On-Board Weight/Balance System (Fortran Program AE-56).” Pan American World Airways, OE-6-67, June 1967.