Aircraft Gearbox Assemblies - Page 3 of 17

403 part numbers
4C95012-105D NSN 1680-00-401-5399 Cross Reference: 544082-9-1
  • feat criticality code justification
  • c-5 a/b aircraft mission design series
  • lockheed source control no. 4c95012-105d reference number differentiating characteristics (non-core)
D2208 NSN 1680-00-401-5426 Cross Reference: 671648-101, 671648-103, D2212
  • f-104 aircraft mission design series
  • t.o. 8a1-7-3-4 special features
4C95016-101E NSN 1680-00-412-2735 Cross Reference: 5901-101E
  • feat criticality code justification
  • trailing edge flap aircraft location
4C95016-103E NSN 1680-00-412-2736 Cross Reference: 5901-103E
  • feat criticality code justification
  • trailing edge flap aircraft location
4C95016-102E NSN 1680-00-412-2737 Cross Reference: 5901-102E
  • feat criticality code justification
  • trailing edge flap aircraft location
4C95016-104E NSN 1680-00-412-2738 Cross Reference: 5901-104E
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-104e reference number differentiating characteristics (non-core)
5904-101D NSN 1680-00-418-2796
  • feat criticality code justification
  • flap aircraft location
4C91001-101B Manufacturers Suggested Name - Control Column Stick Shaker NSN 1680-00-435-8801 Cross Reference: 218-1B, 9510
  • t.o. 5f19-6-3 special features
  • source control dwg no. 4c91001-101b reference number differentiating characteristics (non-core)
4C95016-109D NSN 1680-00-443-6443 Cross Reference: 5901-109D
  • feat criticality code justification
  • source control dwg no. 4c95016-109d reference number differentiating characteristics (non-core)
4C95016-111D NSN 1680-00-443-6445 Cross Reference: 5901-111D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • source control dwg no. 4c95016-111d reference number differentiating characteristics (non-core)
4C95016-112D NSN 1680-00-443-6446 Cross Reference: 5901-112D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • source control dwg no. 4c95016-112d reference number differentiating characteristics (non-core)
C933 NSN 1680-00-449-1227
  • actuator aircraft location
4C95016-110D NSN 1680-00-454-6063 Cross Reference: 5901-110D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • source control dwg no. 4c95016-110d reference number differentiating characteristics (non-core)
12M5910-807 Control - Wing And Flap Position Manufacturers Suggested Name - Box Assy NSN 1680-00-470-8515
  • t.o. 16c1-3-17-3 special features
5905-101C Manufacturer Suggested Name - Position Computer Assembly NSN 1680-00-482-1825
  • feat criticality code justification
  • c-5a aircraft mission design series
4C95009-178A NSN 1680-00-488-9419 Cross Reference: 2021082-2-1
  • feat criticality code justification
4C95009-176A NSN 1680-00-488-9420 Cross Reference: 2021084-2-1
  • feat criticality code justification
  • leading edge slat aircraft location
4C95009-175A NSN 1680-00-488-9423 Cross Reference: 2021084-1-1
  • feat criticality code justification
  • leading edge slat aircraft location
4C95009-177A NSN 1680-00-488-9424 Cross Reference: 2021082-1-1
  • feat criticality code justification
  • leading edge slat aircraft location
209-040-400-11 NSN 1680-00-490-5877
  • h-1 aircraft mission design series
  • u/a: gearbox assembly, tail rotor special features
43523 NSN 1680-00-510-2499
1650R21 NSN 1680-00-510-8671
  • c-130 aircraft end application
50-7332-1 NSN 1680-00-511-4708
50-7332-2 NSN 1680-00-511-4709
D115-2 Boom Extension Manufacturer Suggested Name - Actuator NSN 1680-00-511-5280 Cross Reference: 10-945-3, D115-3
  • kc-135 end application
  • t.o. 6a1-2-4-4 special features