Aircraft Fluid Manifolds - Page 8 of 11

262 part numbers
1591M95G01 NSN 2995-01-368-2737
  • 0.2185 inches mounting hole diameter
  • 2 mounting hole quantity
  • 3 connection quantity
  • not provided metering valves
  • nickel copper alloy material
1591M94G01 NSN 2995-01-368-3817
  • 4.630 inches overall length
  • 0.4795 inches overall width
  • 0.2185 inches mounting hole diameter
  • 2 mounting hole quantity
  • 3 connection quantity
1591M96G01 NSN 2995-01-368-4769
  • 3 connection quantity
  • 0.438 inches connection diameter
  • not provided metering valves
1615M58G01 NSN 2995-01-388-8345
  • 3 mounting hole quantity
  • pacer special f118 engine, b-2 acft end application
  • 5 connection quantity
  • not provided metering valves
  • mounting flange mounting hole location
1B5126-01 NSN 2995-01-390-3652
1B5127-01 NSN 2995-01-390-3971
1B5176-01 NSN 2995-01-390-7248
3830420-1 NSN 2995-01-411-2238
  • pacer dawn end application
3830430-1 NSN 2995-01-411-2239
  • pacer dawn end application
1B6838-01 NSN 2995-01-414-4877
4082811 Assembly Of Right Fuel Supply Manifold NSN 2995-01-418-4143
  • f100-pw-100/200 aircraft gas turbine engine end application
4082812 Assembly Of Left Manifold-fuel Supply NSN 2995-01-418-4144
  • aircraft, model f-16 end application
3830420-2 NSN 2995-01-419-9695
  • pacer dawn end application
5122T38G01 NSN 2995-01-437-4584
  • f404 engine end application
5103T74G01 NSN 2995-01-443-4142
  • preprovisioning support navicp is poe end application
5105T41P01 NSN 2995-01-443-4164 Cross Reference: 6920404E1
5105T48P03 NSN 2995-01-443-4165 Cross Reference: 6920413E3
  • preprovisioning support navicp is poe end application
5105T42P01 NSN 2995-01-443-4166 Cross Reference: 6920412E1
  • used on ge f414-400 engine end application
5105T49P03 Fuel Feede Manifold NSN 2995-01-443-4168 Cross Reference: 6920414E3
23056096 NSN 2995-01-446-6496 Cross Reference: 23091928
  • c130-j acft. end application
74A710750-2003 NSN 2995-01-454-6712
  • preprovisioning support navicp is poe end application
1554M52G01 NSN 2995-01-461-5908
  • 0.028 inches overall thickness
  • f110 engine end application
  • 3 connection quantity
  • not provided metering valves
5105T42P02 NSN 2995-01-467-5216 Cross Reference: 6920412E2
  • used on ge f414-400 engine end application
  • agav criticality code justification
5105T41P02 NSN 2995-01-467-5223 Cross Reference: 6920404E2
631427-2A9 NSN 2995-01-469-8837
  • beechcraft bonanza trainer aircraft end application