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SAE AIR825 Rev D

Current Revision

Oxygen Equipment for Aircraft

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This report provides information on the design and use of aircraft oxygen systems. It explains the physiological oxygen requirements of the human body in both a normal environment and in an hypoxic environment. It includes an overview of the continuous flow, demand and pressure demand, and liquid oxygen systems. A basic understanding of how each system operates is then specifically addressed in its own titled section. The charts, tables, and schematics provide a specific example of a theoretical oxygen system design and the calculations showing how that system would meet the regulations established by the FAR’s. A comprehensive overview of the theoretical oxygen requirements of the human body at altitude is also provided. A detailed list of specifications and standards applicable to aircraft oxygen systems is included.

SDO SAE: SAE International
Document Number AIR825
Publication Date Dec. 3, 2012
Language en - English
Page Count 105
Revision Level D
Supercedes
Committee
Publish Date Document Id Type View
Dec. 3, 2012 AIR825D Revision
May 1, 1999 AIR825C Revision
Sept. 1, 1986 AIR825B Revision
Dec. 1, 1974 AIR825A Revision
March 25, 1965 AIR825 Revision