MIL-PRF-25675 Revision C:1997
Current
The latest, up-to-date edition.
Valves, Check, Miniature, Hydraulic, Aircraft and Missile
26-11-1997
Covers hydraulic, spring-loaded, normally closed aircraft and missile hydraulic system check valves that have an operating pressure of up tp 3,000 pounds per square inch (psi) and operating temperatures from -65 degrees c to 450 degrees c.
| DevelopmentNote |
Supersedes MIL V 25675, MS 24593 and MS 24423. (06/2002) C NOTICE 1 - Notice of Inactivation for New Design. (08/2007) C NOTICE 2 - Notice of Validation but remains Inactive for New Design. (06/2017)
|
| DocumentType |
Standard
|
| Pages |
18
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers hydraulic, spring-loaded, normally closed aircraft and missile hydraulic system check valves with operating pressures up to 3,000 pounds per square inch (psi) and operating temperatures from -65 Deg. to 450 Deg. F.
| SAE AS4395B | FITTING END, FLARED, TUBE CONNECTION, DESIGN STANDARD |
| MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS33514) |
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