Alum alloy; anodized per mil-p-8625c cl 1 or type 1/2; 1100/1200 psi operating pressure, 90/160 degrees f; 6.0 in. L, 4.0 in. W, 4.0 in. H
An item which controls both the direction and the rate of flow of fluid in direct response to a primary control of comparatively low level force. It is used for positioning a linear actuating cylinder assembly, and for controlling the rate of travel of the piston. The primary control force may be mechanical, hydraulic, and/or electrical.
Classification: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)
NSN 5915-01-633-9845
NSN 5950-00-063-2418
NSN 6135-00-921-6487
NSN 2925-01-092-7335
NSN 5975-01-447-2771
NSN 5895-01-519-8062
NSN 2925-01-016-3111
NSN 6135-00-057-2005
NSN 5925-00-356-8007
NSN 6135-01-362-4256
NSN 6685-01-250-4341
NSN 6645-01-538-0425