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The Cessna Model 210 Hydraulic System and Its Development
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1966 by SAE International in United States
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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.
CitationMabe, A., "The Cessna Model 210 Hydraulic System and Its Development," SAE Technical Paper 660202, 1966, https://doi.org/10.4271/660202.
- Equation (1)
- Conway H. G., “Aircraft Hydraulics,” Vol. 1, Page 35, Chapman & Hall, Ltd., 37 Essex Street, London, England.
- Kuchler T. C., “Clearance Seals,” Machine Design, June 11, 1964, Penton Publishing Company, Cleveland, Ohio.