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MIL-D-19326 Design And Installation Of Liquid Oxygen Systems In Aircraft, General Specification ForThis specification covers the general requirements for the design and installation of liquid oxygen \(70 and 300 pounds per square inch gauge\) \(psig\) \(483KPa and 2068 kPa\) systems in aircraft.

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MIL-D-19326H
FIGURE 5. Single converter - dual regulator mulitiple crew station
(fixed converter installation)



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