Two nozzle approx 4.500in.Apart, orfice openings 0.024in.Dia; o/a shape circular on approx 5.13in.Circumference; stem approx 1.66in.Lg, 0.352in.O.D., 0.125in.I.D.; matl ams 5510, ams 5645 and ams 5570 various places; flow min. 52.0lbs per hour
An item designed to direct and control a mist, spray, or stream of lubricating oil inside an engine, gas turbine, aircraft.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5975-00-236-0841
NSN 5996-01-633-7979
NSN 5950-01-164-0327
NSN 5930-00-967-8694
NSN 6110-00-798-4794
NSN 6650-01-019-1550
NSN 5950-01-616-3091
NSN 5950-01-112-8447
NSN 6610-00-998-1355
NSN 6135-01-139-1700
NSN 6105-00-234-1278
NSN 4140-00-628-3546