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Reducers, Oxygen Pressure
- Aerospace Standard
- AS17852A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the requirements for two types of oxygen pressure reducers.
Rationale
AS17852A has been reaffirmed to comply with the SAE Five-Year Review policy.
Recommended Content
Aerospace Standard | PORT OR FITTING END, INTERNAL TAPER PIPE THREAD, DESIGN STANDARD |
Aerospace Standard | FITTING END, EXTERNAL TAPER PIPE THREAD, DESIGN STANDARD |
Topic
Data Sets - Support Documents
Title | Description | Download |
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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 |
Issuing Committee
A-10 Aircraft Oxygen Equipment Committee
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.Reference
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