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MIL-STD-5522
TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
Organization:
NAVY - AS - Naval Air Systems Command
Year: 2000
Abstract: 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.
Subject: Air system test
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T16:06:47Z | |
| date available | 2017-09-04T16:06:47Z | |
| date copyright | 03/17/2000 | |
| date issued | 2000 | |
| identifier other | RZLINAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/69999 | |
| description abstract | 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. | |
| language | English | |
| title | MIL-STD-5522 | num |
| title | TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS | en |
| type | standard | |
| page | 46 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;2000 | |
| contenttype | fulltext | |
| subject keywords | Air system test | |
| subject keywords | Engine test | |
| subject keywords | Flight capability | |
| subject keywords | Fluid system test | |
| subject keywords | Functional inspection | |
| subject keywords | Ground cart test | |
| subject keywords | Methodology | |
| subject keywords | Mission profile | |
| subject keywords | Operational inspection | |
| subject keywords | Simulator test |