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Integral Weight and Balance System Applications on Cargo Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1968 by SAE International in United States
Annotation ability available
Event: Space Technology Conference
A current status of development of aircraft integral weight and balance systems (IWBS) as applied to cargo aircraft is presented. This discussion describes testing, installation, and calibration procedures including related problems, errors, accuracy requirements, and system functions. Knowledge of these current system limitations and problems will provide a better appreciation of the design requirements and complexities of the IWBS.
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CitationTritton, C., "Integral Weight and Balance System Applications on Cargo Aircraft," SAE Technical Paper 680354, 1968, https://doi.org/10.4271/680354.
- “Integral Weight and Balance Subsystem,” Lockheed-Georgia Co. Specification Document No. 41154, August 1967 revision.
- “Integral Weight and Balance Subsystem,” Lockheed-Georgia Co. Manufacturing Functional Test Procedure No. B-88003, Nov. 10, 1967 revision.