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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
NOTES FOR APPENDIX A
The applicable portion of either MIL-V-7908 or MIL-V-25513 maybe used
The applicable portion of either MIL-C-81302 or MIL-T-81533 maybe used
The applicable portion of either MIL-T-8506 or AMS 4071 maybe used
The applicable portion of either MIL-C-19328 or MIL-C-19803 maybe used
The applicable portion of either MIL-A-23121 or AFGS-87235 maybe used
The applicable portion of either MIL-E-2541O or MIL-R-83178 maybe used
The applicable portion of either MIL-I-25645 or MIL-I-81378 maybe used
The applicable portion of either QQ-Z-324 or QQ-P-416 maybe used
The applicable portion of either QQ-S-766 or MIL-S-4043 maybe used
The applicable portion of either MIL-C-81302 or MIL-T-81533 maybe used
The applicable portion of either MIL-D-26392 or MIL-D-26393 maybe used
The applicable portion of either MIL-O-27335 or MIL-S-81018 maybe used
The applicable portion of either MS22059, MS22061, or Drawing 6003570
maybe used
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