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Page Title:
Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
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|  INCH-POUND
MIL-D-19326H
31 August 1990
MIL-D-19326G
1 October 1985
MILITARY SPECIFICATION
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS
IN AIRCRAFT, GENERAL SPECIFICATION FOR
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
SCOPE
1.
1.1 Scope. 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.
2.
APPLICABLE DOCUMENTS
2.1 Government documents.
* 2.1.1 Specification and standards. The following specifications and standards
form a part of this specification to the extent specified herein. Unless otherwise
specified, the issues of these documents are those listed in the issue of the
Department of Defense Index of specifications and Standards (DoDISS} and supplement
thereto, cited in the solicitation (see 6.2b).
SPECIFICATIONS
MILITARY
MIL-B-5087
-
Bonding, Electrical, and Lighting Protection,
For Aerospace Systems
MIL-H-5088
-
Wiring, Aerospace Vehicle
Beneficial comments (recommendations, additions, deletions} and any pertinent data
which may be of use in improving this document should be addressed to: Systems
Engineering and Standardization Department (Code 53) Naval Air Engineering Center,
Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document
Improvement Proposal (DD Form 1426) appearing at the end of this document or by
1 letter.
AMSC N/A
FSC 1660
DISTRIBUTION STATEMENT A:
Approved for public release; distribution is unlimited.
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