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 6105-00-899-0415
NSN 6135-00-299-6918
NSN 5915-00-387-2333
NSN 6145-00-918-7225
NSN 5999-00-078-7702
NSN 6240-00-866-6239
NSN 5905-00-851-7665
NSN 6650-01-284-1158
NSN 5990-01-612-5323
NSN 5915-01-008-6268
NSN 6320-00-857-4073
NSN 6110-01-106-2708