Aircraft Gearbox Assemblies

403 part numbers
42252R151 NSN 1680-00-009-0878 Cross Reference: 4G94033-103A
  • 14.281 inches overall length
  • 11.922 inches overall width
20537-1 Manufactures Suggested Name - Throttle Box And Torque Shaft Assembly NSN 1680-00-017-9367 Cross Reference: 53-65050-5
  • f-4c aircraft end application
  • t.o. 2ja12-4-4 special features
4F90009-123C NSN 1680-00-026-4424 Cross Reference: 544996-3-1
  • c-5a aircraft mission design series
  • a-7 aircraft mission design series
  • t.o. 5f19-7-2 special features
67D29700 NSN 1680-00-064-0884
  • c-130h end application
  • landing gear aircraft location
5-87199-3003 NSN 1680-00-072-0265 Cross Reference: 5-87199-3001, 5-87199-3002
523EA8 NSN 1680-00-078-4322
  • forward stabilizer trim aircraft location
  • kd-135 aircraft mission design series
  • t.o. 16c1-10-4-4 special features
14-51100-1 NSN 1680-00-139-8020 Cross Reference: 14-51100-3, 71024-000
  • f-5 aircraft mission design series
4C95016-120D NSN 1680-00-140-2528 Cross Reference: 5901-120D
  • feat criticality code justification
  • trailing edge flaps aircraft location
  • c-5a aircraft mission design series
4C95016-119D NSN 1680-00-140-2529 Cross Reference: 5901-119D
  • feat criticality code justification
  • trailing edge flaps aircraft location
  • c-5a aircraft mission design series
20537-3 NSN 1680-00-159-8730 Cross Reference: 20537-4, 53-65050-15
544340-2-1 NSN 1680-00-178-8528 Cross Reference: CM0042-2-4
  • flap drive aircraft location
530949-4 NSN 1680-00-179-0316
  • f-111 aircraft mission design series
177890-1 NSN 1680-00-185-1139
  • c-5a aircraft mission design series
5-53182 NSN 1680-00-217-5134
  • aircraft model b-52b end application
  • b-52h aircraft mission design series
4C95017-165D NSN 1680-00-230-6905 Cross Reference: 5902-165D
  • flap drive aircraft location
  • c-5a aircraft mission design series
4C95016-117E NSN 1680-00-248-7634 Cross Reference: 5901-117E
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-117e reference number differentiating characteristics (non-core)
4C95016-116D NSN 1680-00-248-7636 Cross Reference: 5901-116D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-116d reference number differentiating characteristics (non-core)
4C95016-115D NSN 1680-00-248-7638 Cross Reference: 5901-115D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-115d reference number differentiating characteristics (non-core)
5901-114D NSN 1680-00-248-7639 Cross Reference: 4C95016-114D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-114d reference number differentiating characteristics (non-core)
4C95016-113D NSN 1680-00-248-7641 Cross Reference: 5901-113D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-113d reference number differentiating characteristics (non-core)
5901-108D NSN 1680-00-248-8500 Cross Reference: 4C95016-108D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-108d reference number differentiating characteristics (non-core)
4C95016-107D NSN 1680-00-248-8549 Cross Reference: 5901-107D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • lockheed source control dwg no. 4c95016-107d reference number differentiating characteristics (non-core)
4C95016-105D NSN 1680-00-248-8553 Cross Reference: 5901-105D
  • feat criticality code justification
  • trailing edge flap aircraft location
  • c-5 acft aircraft mission design series
  • lockheed source control dwg no. 4c95016-105d reference number differentiating characteristics (non-core)