Remote Control Levers - Page 18 of 32

798 part numbers
65404-03412-042 NSN 1680-00-915-6912
  • between 1.814 inches and 1.815 inches bore diameter
  • between 1.307 inches and 1.312 inches bore length
  • plain straight bore type
  • 4.835 inches center to center distance between link and shaft holes
  • between 1.307 inches and 1.312 inches shaft end thickness
65404-03417-041 NSN 1680-00-915-6914 Cross Reference: 65404-03414-041
  • between 1.814 inches and 1.815 inches bore diameter
  • between 1.495 inches and 1.500 inches bore length
  • plain straight bore type
  • 2.255 inches center to center distance between link and shaft holes
  • between 1.495 inches and 1.500 inches shaft end thickness
65404-03612-041 NSN 1680-00-915-6916
  • 2.000 inches overall width
  • between 1.814 inches and 1.815 inches bore diameter
  • between 1.280 inches and 1.285 inches bore length
  • plain straight bore type
  • 5.000 inches center to center distance between link and shaft holes
65401-02420-041 NSN 1680-00-915-7223
  • between 1.437 inches and 1.438 inches bore diameter
  • 1.469 inches bore length
  • plain straight bore type
  • 3.000 inches center to center distance between link and shaft holes
  • 1.469 inches shaft end thickness
65401-02423-041 NSN 1680-00-915-7613
  • between 1.437 inches and 1.438 inches bore diameter
  • 1.434 inches bore length
  • plain straight bore type
  • 7.460 inches center to center distance between link and shaft holes
  • 1.434 inches shaft end thickness
209-001-115-1 NSN 1680-00-919-4644
  • between 1.980 inches and 2.050 inches overall width
  • 0.656 inches bore diameter
  • between 0.550 inches and 0.600 inches bore length
  • ah-1 series helicopters end application
  • plain straight bore type
3G11776-103 NSN 1680-00-927-0502
  • between 0.312 inches and 0.313 inches bore diameter
  • 0.730 inches bore length
  • plain straight bore type
  • between 0.925 inches and 0.935 inches center to center distance between link and shaft holes
  • 0.730 inches shaft end thickness
3G11798-103 NSN 1680-00-927-0642
  • c-141 aircraft end application
  • splined bore type
  • counterbore and keyway features provided
  • keyway shaft securing method
  • includes splines special features
12M5139-1 NSN 1680-00-927-6643
  • plain straight bore type
  • 3.610 inches center to center distance between link and shaft holes
  • 4.430 inches shaft end thickness
  • 0.954 inches link end thickness
  • 0.250 inches link end hole diameter
3822727-1 NSN 1680-00-928-6897
  • 1.562 inches overall width
  • serrated bore type
  • 4.000 inches center to center distance between link and shaft holes
  • 1.243 inches shaft end thickness
  • 0.640 inches link end thickness
3822727-2 NSN 1680-00-928-6898
  • 1.562 inches overall width
  • serrated bore type
  • 4.000 inches center to center distance between link and shaft holes
  • 1.243 inches shaft end thickness
  • 0.640 inches link end thickness
2-13684-1 NSN 1680-00-928-8753
  • 0.900 inches overall width
  • between 0.755 inches and 0.765 inches bore diameter
  • between 0.580 inches and 0.620 inches bore length
  • plain straight bore type
  • between 0.580 inches and 0.620 inches shaft end thickness
3822587-1 NSN 1680-00-929-6019
  • 1.250 inches major diameter
  • 0.125 inches keyway width
  • 1.563 inches keyway length
  • 0.750 inches minor diameter
  • serrated bore type
3822588-1 NSN 1680-00-929-6020
  • between 0.654 inches and 0.656 inches major diameter
  • serrated bore type
  • keyway features provided
  • keyway shaft securing method
  • aluminum material
540-011-495-2 NSN 1680-00-930-5227 Cross Reference: 540-011-448-2
  • uh-1 series helicopters end application
  • steel material
  • sae 4340 assn standard single material response material specification
  • cadmium surface treatment
4141616-2 NSN 1680-00-932-2501 Cross Reference: 4190955-3
  • 39 spline quantity
  • splined bore type
  • 5.120 inches center to center distance between link and shaft holes
  • 0.480 inches shaft end thickness
  • 1.000 inches link end thickness
32-35306-3 NSN 1680-00-939-3236 Cross Reference: 32-35306-5
  • 1.870 inches bore length
  • plain straight bore type
  • 1.500 inches center to center distance between link and shaft holes
  • 1.870 inches shaft end thickness
  • 0.807 inches link end thickness
65301-03004-101 NSN 1680-00-941-3180
  • 0.625 inches overall width
  • serrated bore type
  • 1.558 inches center to center distance between link and shaft holes
  • between 0.495 inches and 0.505 inches shaft end thickness
  • 0.156 inches link end thickness
65402-02121-041 NSN 1680-00-941-3281
  • between 1.312 inches and 1.313 inches bore diameter
  • between 1.248 inches and 1.252 inches bore length
  • plain straight bore type
  • 3.045 inches center to center distance between link and shaft holes
  • between 1.248 inches and 1.252 inches shaft end thickness
65402-02127-041 NSN 1680-00-941-3283
  • between 2.312 inches and 2.313 inches bore diameter
  • 1.030 inches bore length
  • plain straight bore type
  • 2.680 inches center to center distance between link and shaft holes
  • 1.030 inches shaft end thickness
706565-1 NSN 1680-00-944-0512
  • control, air inlet, aircraft 743655l1 1650003501034 end application
  • knurled handle special features
  • steel material
706571-1 NSN 1680-00-944-3333
  • f-111 aircraft end application
  • used on p/n 728152; t.o. 9p11-7-4 special features
  • aluminum alloy material
  • anodize surface treatment
707280-1 NSN 1680-00-944-3334
  • f-111 aircraft end application
  • used on p/n 728152; t.o. 9p11-7-4 special features
  • aluminum alloy material
  • anodize surface treatment
706576-1 NSN 1680-00-944-3367
  • f-111 aircraft end application
  • used on p/n 728152; t.o. 9p11-7-4 special features
  • aluminum alloy material
  • anodize surface treatment
706578-1 NSN 1680-00-944-3368
  • stainless steel material
  • passivate surface treatment