NPFC - MIL-STD-5522
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
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| Organization: | NPFC |
| Publication Date: | 17 March 2000 |
| Status: | active |
| Page Count: | 46 |
scope:
This standard establishes test and test method requirements for aircraft and weapons hydraulic and emergency pneumatic systems design and installation with operating pressure ranges from 3,000 psi to 8,000 psi and temperature ranges from −65 °F to + 450 °F.
intended Use:
This standard is for use in determining methods for testing aircraft hydraulic and emergency pneumatic systems.
Document History
November 13, 2018
Test Requirements and Methods for Aircraft Hydraulic and Emergency Pneumatic Systems
A description is not available for this item.
February 7, 2014
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
January 7, 2005
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
A description is not available for this item.
MIL-STD-5522
March 17, 2000
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
This standard establishes test and test method requirements for aircraft and weapons hydraulic and emergency pneumatic systems design and installation with operating pressure ranges from 3,000 psi to...
References
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