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 5930-00-266-8175
NSN 5905-00-359-9325
NSN 6610-01-044-4740
NSN 6240-01-004-9634
NSN 2925-01-337-2508
NSN 5905-01-010-2894
NSN 6685-01-195-1535
NSN 5975-01-605-4708
NSN 5960-01-249-4550
NSN 5910-00-399-0734
NSN 5965-00-706-7005
NSN 6130-01-527-8238