Aircraft Fluid Manifolds - Page 2 of 11

262 part numbers
9658M32G06 NSN 2995-00-421-5163
  • general electric eng t-39 end application
9658M33G06 NSN 2995-00-421-5164
  • tf-39 aircraft engine end application
9666M07G06 NSN 2995-00-421-5165
  • aircraft eng tf39 end application
  • agav criticality code justification
9004M47G01 NSN 2995-00-497-2544
  • aircraft eng tf39 end application
  • agav criticality code justification
  • t.o. 2j-tf39-4 reference data and literature
573E614G1 NSN 2995-00-546-2947
  • 0.281 inches mounting hole diameter
  • 2 mounting hole quantity
  • aircraft eng end application
  • 4 connection quantity
  • manifold foot plate mounting hole location
302568 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-564-7613
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
315062 NSN 2995-00-567-6647
  • 3 connection quantity
  • not provided metering valves
325049 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-588-8947
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
107R135G2 NSN 2995-00-603-1323
  • 8 mounting hole quantity
  • aircraft eng end application
  • 3 connection quantity
  • not provided metering valves
  • manifold foot plate mounting hole location
350171 NSN 2995-00-607-5771
  • j57 aircraft engine end application
  • 3 connection quantity
  • not provided metering valves
7059R71G1 Inlet Guide Vane Actuator Tube-drain NSN 2995-00-613-7308
  • 0.035 inches overall thickness
  • aircraft eng end application
  • 3 connection quantity
  • 0.250 inches connection diameter
  • agav criticality code justification
328315 NSN 2995-00-614-5378
  • aircraft eng j57 end application
  • agav criticality code justification
  • t.o. 2j-57-24 reference data and literature
639E316G1 Manifold-secondary Uniform NSN 2995-00-703-2210 Cross Reference: 7058R62G1
  • j79-11 aircraft engine end application
  • agav criticality code justification
484634 NSN 2995-00-761-0017 Cross Reference: 408019, 457184, 457186, 482980
  • engine, acft, tf33 end application
  • 2j-tf33-4 reference data and literature
484635 NSN 2995-00-761-0018 Cross Reference: 408020, 457185, 457187, 482982
  • engine, acft, tf33 end application
  • 2j-tf33-4 reference data and literature
505569 NSN 2995-00-761-8023
  • aircraft eng tf33 end application
  • agav criticality code justification
  • t.o. 2j-tf33-14 reference data and literature
431294 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-764-6062 Cross Reference: 431295
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
431816M1 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-764-6254 Cross Reference: 431814M1
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
375556 NSN 2995-00-777-0347
  • aircraft eng j75 end application
37E501247P101 NSN 2995-00-786-5122
  • aircraft eng j-85 fsc application data
37E501248P101 NSN 2995-00-786-5123
512D894G1 NSN 2995-00-798-6465
  • aircraft eng j79, j85, t58, t64 end application
  • agav criticality code justification
  • 2j-j79-44 reference data and literature
874C359G1 NSN 2995-00-798-6476
  • aircraft eng j79 end application
  • agav criticality code justification
429312 NSN 2995-00-808-1019
  • aircraft eng tf33 end application
  • agav criticality code justification
  • t.o.2j-tf33-4 reference data and literature
446204 NSN 2995-00-819-6144
  • aircraft eng tf33 end application
  • agav criticality code justification
  • 2j-tf33-4 reference data and literature