MIL-D-19326 Revision H:1990
Current
Current
The latest, up-to-date edition.
Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for
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Published date
08-31-1990
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.Details requirements for the design and installation of liquid oxygen 70 and 300 psig (483 kPa and 2068 kPa) systems in aircraft.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
69
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This 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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