Aircraft Fluid Manifolds

262 part numbers
1002M68G01 NSN 2995-00-001-8344
  • aircraft engine tf-39 end application
  • steel, ams5557; includes connectinghardware special features
  • steel material
  • steel material
1002M67G01 NSN 2995-00-001-8345
  • aircraft engine tf-39 end application
  • steel, ams5557 special features
478554 NSN 2995-00-015-4177 Cross Reference: 300620
  • aircraft eng j-75 end application
563215 NSN 2995-00-061-8889 Cross Reference: 483267, 524340
  • 2j-tf33-4 reference data and literature
563217 NSN 2995-00-061-8892 Cross Reference: 483268, 524341
  • 2j-tf33-4 reference data and literature
575C627P2 NSN 2995-00-103-3515 Cross Reference: 04333
  • 2.380 inches overall width
  • between 0.274 inches and 0.288 inches mounting hole diameter
  • 6 mounting hole quantity
  • 0.025 inches overall thickness
  • aircraft eng j79 end application
9678M77G02 NSN 2995-00-112-2160 Cross Reference: 9678M77G01
  • aircraft engine tf-39 end application
  • not provided metering valves
9678M11G01 NSN 2995-00-113-1716
  • aircraft engine tf-39 end application
  • not provided metering valves
  • steel material
  • steel material
9672M49G02 NSN 2995-00-113-6445
  • aircraft eng tf-39 end application
  • agav criticality code justification
9676M74G02 NSN 2995-00-113-6478
  • aircraft eng tf-39 end application
9676M72G03 NSN 2995-00-113-6479 Cross Reference: 9676M72G02
  • aircraft eng tf-39 end application
9658M31G04 NSN 2995-00-113-6492
  • aircraft tf-39 end application
9658M32G05 NSN 2995-00-113-6493
  • general electric eng t-39 end application
9658M29G05 NSN 2995-00-113-6494
  • general electric engine, tf-39 end application
9658M33G05 NSN 2995-00-113-8653
  • aircraft engine tf-39 end application
758228 NSN 2995-00-119-5785 Cross Reference: 644657
  • aircraft eng tf33 end application
  • agav criticality code justification
679799 NSN 2995-00-138-9321
  • aircraft eng tf30p414a end application
  • 3 connection quantity
  • not provided metering valves
6866550 NSN 2995-00-152-2233
  • aircraft eng tf41 end application
  • agav criticality code justification
695217 NSN 2995-00-184-5308 Cross Reference: 695247
  • aircraft eng tf-30 end application
695216 NSN 2995-00-184-5309
  • 20.524 inches overall length
  • aircraft jet engine, tf-30 end application
  • 4 connection quantity
  • adjustable cover thread protector type
  • not provided metering valves
482994 Assembly Of Manifold-fuel NSN 2995-00-225-0737
  • kc135 end application
  • 2j-j57-54 reference data and literature
482993 Assembly Of Right Manifold & Nozzle-fuel NSN 2995-00-225-1100 Cross Reference: 482992, 521714
  • j57 engine end application
  • 24 connection quantity
  • between 0.937 inches and 0.943 inches connection diameter
  • steel, corrosion resisting material
  • stainless steel material
225179 NSN 2995-00-326-3825
4033673 Assembly Of Left Manifold-fuel Supply NSN 2995-00-345-4025
4033674 Assembly Of Right Manifold-fuel Supply NSN 2995-00-345-4029