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The Cessna Model 210 Hydraulic System and Its Development
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English
Abstract
This paper presents the current hydraulic system on the Cessna Model 210 aircraft and some of the problems encountered during its development. Several cross-section views of the various components are illustrated, along with a schematic of the system, to aid in explaining how the necessary sequencing is accomplished with a combination of electrically and hydraulically controlled sequencing devices. In view of the demands made of the system, it is a practical, reasonably simple, and reliable light aircraft landing gear retraction system.
Authors
Citation
Mabe, A., "The Cessna Model 210 Hydraulic System and Its Development," SAE Technical Paper 660202, 1966, https://doi.org/10.4271/660202.Also In
References
- Conway H. G. “Aircraft Hydraulics,” 1 35 Chapman & Hall, Ltd. 37 Essex Street, London, England
- Kuchler T. C. “Clearance Seals,” Machine Design June 11 1964 Penton Publishing Company Cleveland, Ohio