Aircraft Fluid Manifolds - Page 3 of 11

262 part numbers
517D620P01 NSN 2995-00-852-1600 Cross Reference: 517D620P03, 517D620P04, 94479C115, AE700117-2, R11681
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • t.o.2j-j79-44 reference data and literature
  • p/n 512d837p1 fsc application data
517D653P01 NSN 2995-00-853-6929 Cross Reference: 517D653P03, 517D653P04, 530212-2, 94479C116, R11682
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • t.o. 2j-j79-4 reference data and literature
440730 NSN 2995-00-856-4052
  • aircraft eng tf33 end application
  • agav criticality code justification
  • t.o. 2j-tf-33-4 reference data and literature
636E620G01 L.h. Air-fwd Anti-icing Manifold NSN 2995-00-866-1525
  • aircraft eng end application
  • 3 connection quantity
  • agav criticality code justification
482984 NSN 2995-00-867-6450 Cross Reference: 374719, 457183
  • tf33 end application
  • 2j-tf33-4 reference data and literature
107R880G1 NSN 2995-00-871-0757
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • t.o. 2j-j79-54 reference data and literature
440718 NSN 2995-00-872-9551
  • aircraft eng tf33 end application
  • agav criticality code justification
  • t.o. 2j-tf33-4 reference data and literature
106C2622G1 NSN 2995-00-887-2147 Cross Reference: 103C2622G1
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • t.o. 2j-79-54 reference data and literature
431818 Assembly Of Manifold-fuel NSN 2995-00-895-3960 Cross Reference: 489477
  • kc135 end application
  • 2j-j57-54 reference data and literature
583804 NSN 2995-00-911-8135 Cross Reference: 519525, 519526
  • j57 eng end application
547512 NSN 2995-00-918-5720 Cross Reference: 490032, 783030, 797251, 797262, 797313
  • tf33-p-9 aircraft engine end application
  • 2j-tf33-4 reference data and literature
547513 NSN 2995-00-918-5723 Cross Reference: 490034, 783032, 797263, 797312, 797314
  • tf33-p-9 aircraft engine end application
  • 2j-tf33-4 reference data and literature
636E613P1 NSN 2995-00-945-6854 Cross Reference: ER1060
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • t.o. 2j-j79-54 reference data and literature
1-130-720-02 NSN 2995-00-949-8219
  • t53-series engines end application
  • steel, corrosion resisting material
  • stainless steel material
716876 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-956-6553 Cross Reference: 521693
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
521694 Assembly Of Right -fuel Manifold NSN 2995-00-956-6554
  • j57 engine end application
488959 NSN 2995-00-966-2985
  • aircraft eng tf33 end application
  • agav criticality code justification
  • t.o. 2j-tf33-4 reference data and literature
512-024-2001 NSN 2995-00-979-4666 Cross Reference: 105248, 575C748P2, 575C748P3, ER110
471298 NSN 2995-00-980-2647
  • 15.041 inches overall length
  • 2 connection quantity
  • not provided metering valves
471296 NSN 2995-00-980-2649
  • 30.688 inches overall length
  • 2 connection quantity
  • 0.312 inches connection diameter
  • not provided metering valves
  • connector-tube press sens up special features
537254 NSN 2995-00-997-9277
  • aircraft engine tf-30 end application
  • not provided metering valves
748631 NSN 2995-01-004-5661 Cross Reference: 633916, 651996
  • 21.667 inches overall length
  • 5 connection quantity
  • adjustable cover thread protector type
  • not provided metering valves
  • tf-30 turbine engine, acft fsc application data
783011 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-01-086-5195 Cross Reference: 282615, 431293, 431818, 482994, 489477, 521694
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
3480652-2 NSN 2995-01-117-5452
  • 2.400 inches overall length
  • between 0.278 inches and 0.287 inches mounting hole diameter
  • 4 mounting hole quantity
  • 1.400 inches overall thickness
  • 1 and 1 and 1 connection quantity
2171M40G01 NSN 2995-01-146-7571 Cross Reference: 5050M43G01, 5050M43G02
  • f101 aircraft engine end application
  • 52.724 inches connection diameter
  • not provided metering valves