SAE AIR1069B-2015
Crew Oxygen Requirements Up to a Maximum Altitude of 45@000 Ft

Standard No.
SAE AIR1069B-2015
Release Date
2015
Published By
SAE - SAE International
Latest
SAE AIR1069B-2015
Scope
Determine the required minimum oxygen concentration to be breathed prior to@ during@ and after a loss of cabin pressurization@ and Determine recommended means necessary to provide the required oxygen concentrations. CONCLUSIONS: To prevent impairment of consciousness caused by hypoxia after decompression oxygen must be used as follows: A. Above 24@000 and up to 40@000 feet the system must provide@ in accordance with Figure 1: (1) An increased minimum oxygen concentration prior to a decompression@ (2) A schedule of increased oxygen concentration with increase in cabin altitude@ (3) 100% oxygen at an altitude not higher than 24@000 feet@ and (4) Safety pressure to begin simultaneously with delivery of 100% oxygen. B. Between 40@000 and 45@000 feet the system must provide@ in addition to the above@ (1) Delivery of 100% oxygen under positive pressure@ increasing with altitude to maintain no less than the equivalent of 40@000 feet. C. When cabin altitude can not exceed 25@000 feet (1) No change in present requirements.

SAE AIR1069B-2015 history

  • 2015 SAE AIR1069B-2015 Crew Oxygen Requirements Up to a Maximum Altitude of 45@000 Ft
  • 2012 SAE AIR1069A-2012 Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Ft.
  • 2002 SAE AIR1069A-2002 Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Feet
  • 2001 SAE AIR1069A-2001 Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Ft.
  • 1991 SAE AIR1069-1991 CREW OXYGEN REQUIREMENTS UP TO A MAXIMUM ALTITUDE OF 45, 000 FT.
  • 1968 SAE AIR1069-1968 Crew Oxygen Requirements up to a Maximum Altitude of 45@000 ft. (Errata)
Crew Oxygen Requirements Up to a Maximum Altitude of 45@000 Ft



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