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 6240-00-532-7770
NSN 6150-00-893-8230
NSN 6220-01-327-4999
NSN 5835-01-078-6126
NSN 5998-00-937-5985
NSN 6650-01-101-4339
NSN 6610-00-012-8072
NSN 5945-01-391-7993
NSN 5998-01-242-8313
NSN 5855-01-524-4474
NSN 5996-00-209-9517
NSN 5999-00-843-8022