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 4140-01-063-7192
NSN 5920-00-616-4087
NSN 5975-01-461-3120
NSN 5945-00-529-0409
NSN 6150-00-068-8493
NSN 5965-01-358-4923
NSN 6685-01-202-7823
NSN 6610-00-610-0228
NSN 5835-01-464-7038
NSN 5975-01-498-6442
NSN 6685-01-190-5458
NSN 5910-00-472-3440