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 6610-01-188-8163
NSN 6135-01-067-8331
NSN 6145-00-432-4840
NSN 5975-01-432-0960
NSN 5945-01-067-9362
NSN 5835-01-228-8666
NSN 6645-01-645-9117
NSN 6650-00-944-1399
NSN 5990-01-453-3552
NSN 5855-01-069-4032
NSN 6110-01-197-6954
NSN 6320-00-228-5678