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J69-T-25A engine
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 deg 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
asdifferentiated by drawing
Schedule B number: 8411997050
nmfc 127600
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).
Used on j69-t-25a engine. 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 deg 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
1. | GD252-3 | Cage 86329 |
Nothing similar to this part number was found in our inventory
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.