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Oxygen Equipment, Provisioning and Use in High Altitude (to 40,000 ft.) Commercial Transport Aircraft
- Aerospace Standard
Published October 16, 2014 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The recommendations embodied in this document are applicable to commercial transport aircraft for operations between 8,000 and 40,000 ft. altitude.
The A-10 Committee concluded that the content of this document will not be updated in the future. New documents updating the issues previously addressed have been or are being developed that addresses current technologies and practices specific to commercial operations above 40,000 ft. Therefore, the Committee decided to stabilize this document in its current state.
|Aerospace Standard||The Control of Excess Humidity in Avionics Cooling|
|Technical Paper||Heat Exchanger Fouling Detection in Aircraft Environmental Control Systems|
|Aerospace Standard||Environmental Control Systems Terminology|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|TABLE I||Oxygen Mixtures Required to Provide a 5,000 Ft. Equivalent Altitude Between Sea Level & 36,000 Ft.|
Welcome to the SAE A-10 Aircraft Oxygen Equipment Committee public forum area.The SAE A-10 Aircraft Oxygen Equipment Committee develops standards and practices in the design and information compiled from users, equipment suppliers, aircraft manufacturers, regulatory agencies and medical groups in the aeronautical oxygen field. The A-10 Committee also promotes safety in the aviation oxygen field. It defines the needs and encourages research needed in the area of aviation physiology, as it relates to respiratory functions and oxygen equipment performance.
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