Rotation clockwise, involute spline drive, 13 teeth, 32/64 diametral pitch, 30 deg. Pressure angle; flow vs speed inlet pressure 25-30 ins hg abs discharge, pressure: 35 psi. Oil: mil-l-780, temp: 180 degrees f, no entrained air.Flow vs inlet pressure speed; 4694rpm; discharge pressure 35 psi; oil mil-l-7808; temp 180 deg. F, no entrained air
A device designed to maintain oil pressure within the moving parts of an internal combustion engine. May contain parts such as shaft, gears, pin, bushing, screen, adjusting screw and the like.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 4140-00-789-2543
NSN 4140-00-248-6089
NSN 6685-00-717-4058
NSN 5920-01-582-5967
NSN 5925-00-192-9630
NSN 6610-00-264-0961
NSN 5915-00-877-7338
NSN 6105-00-187-0094
NSN 4140-01-291-4838
NSN 5998-01-119-1548
NSN 6105-01-121-4610
NSN 7035-01-459-8268