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CREW OXYGEN REQUIREMENTS UP TO A MAXIMUM ALTITUDE OF 45, 000 FT.
- Aerospace Standard
Downloadable datasets availableAnnotation ability available
Data Sets - Support Documents
|[Unnamed Dataset 1]||SUMMARY A|
|[Unnamed Dataset 2]||THE INCIDENCE OF HYPOXIA FOLLOWING RAPID DECOMPRESSION FROM 8, 000 FEET IN 1.5 SECONDS|
|TABLE I||EFFECTS OF VARIOUS SIZE DEFECTS IN THE CABIN WALL UPON THE CABIN ALTITUDE|
|[Unnamed Dataset 4]|
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.
|AIR825D||Oxygen Equipment for Aircraft|
|FA-955||This document is not part of the subscrption.|
|IAM183||This document is not part of the subscrption.|
|IAM313||This document is not part of the subscrption.|
|IAMReportFPRC/1||This document is not part of the subscrption.|
|NASASP-3006||This document is not part of the subscrption.|
|RO316/2||This document is not part of the subscrption.|
|RO316/3||This document is not part of the subscrption.|
|RP316/1||This document is not part of the subscrption.|
|USAFSAMTDR63-56||This document is not part of the subscrption.|
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