SAE AIR847A-1965
(Noncurrent)Oxygen Equipment for Commercial Transport Aircraft Which Fly Above 45,000 ft R(1991)

Standard No.

SAE AIR847A-1965

Release Date

1965

Published By

Society of Automotive Engineers (SAE)

Status

Withdraw

Replace By

SAE AIR847-1991

Latest

SAE AIR847A-2016

Scope

The purpose of this information report is to provide minimum design criteria for oxygen equipment to be used on commercial transport aircraft which fly above 45,000 ft. To separate these requirements from those for spaceplanes, the maximum flight altitude for aircraft defined by this report is limited to the maximum altitude obtainable by aircraft using air-breathing engines.

SAE AIR847A-1965 history

• 2016 SAE AIR847A-2016 Oxygen Equipment for Commercial Transport Aircraft Which Fly Above 45,000 Ft
• 2000 SAE AIR847A-2000 Oxygen Equipment for Commercial Transport Aircraft Which Fly Above 45@000 ft
• 1991 SAE AIR847-1991 OXYGEN EQUIPMENT FOR COMMERCIAL TRANSPORT AIRCRAFT WHICH FLY ABOVE 45, 000 FT
• 1965 SAE AIR847A-1965 (Noncurrent)Oxygen Equipment for Commercial Transport Aircraft Which Fly Above 45,000 ft R(1991)
• 1965 SAE AIR847-1965 Oxygen Equipment for Commercial Transport Aircraft Which Fly Above 45@000 ft