This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Reducers, Oxygen Pressure
- Aerospace Standard
Published November 07, 2017 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers the requirements for two types of oxygen pressure reducers.
AS17852A has been reaffirmed to comply with the SAE Five-Year Review policy.
|Aerospace Standard||PORT OR FITTING END, INTERNAL TAPER PIPE THREAD, DESIGN STANDARD|
|Aerospace Standard||FITTING END, EXTERNAL TAPER PIPE THREAD, DESIGN STANDARD|
|Aerospace Standard||FITTING, ADAPTER, STRAIGHT PIPE TO FLARED|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Unnamed Dataset 4|
|Unnamed Dataset 5|
|Unnamed Dataset 6|
|TABLE 1||SAMPLING SIZE, ACCEPTANCE CRITERIA, TESTS AND EXAMINATIONS OF THE REDUCERS|
|TABLE 3||LIST OF DEFECTS FOR PACKAGING|
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.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.