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C-5A Flight Control System
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
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The C-5A flight control system is explained with individual schematics illustrating each subsystem. Several mechanical failure situations and necessary pilot actions are described. The distribution of hydraulic power and its importance on an airplane which uses fully powered hydraulic flight controls is explained. The handling quality requirements and some results of ground based simulation studies are presented.
CitationJamison, G., "C-5A Flight Control System," SAE Technical Paper 670574, 1967, https://doi.org/10.4271/670574.