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Full Description

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 shown 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.
 

Document History

  1. SAE AIR825D


    Oxygen Equipment for Aircraft (Stabilized: Dec 2012)

    • Most Recent
  2. SAE AIR 825C

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    Oxygen Equipment for Aircraft ( Reaffirmed: Apr 2006 Nov 2009 Dec 2010 )

    • Historical Version