Remote Control Levers - Page 27 of 32

798 part numbers
742313 NSN 1680-01-416-8369
  • aircraft c-17a end application
  • lever, release special features
3342086-3 NSN 1680-01-417-1778
  • c-130 aircraft end application
  • aluminum alloy material
  • qq-a-250/4 federal specification single material response material specification
377250-5 NSN 1680-01-417-3420
  • c-130 aircraft end application
357015-7 NSN 1680-01-418-1868
  • aircraft c-130 end application
  • lever, manual control special features
A451-16 NSN 1680-01-418-6045
  • aircraft c-130 end application
  • err default err default
  • lever assembly landing gear control. special features
66-4874 NSN 1680-01-419-0986
  • joint stars target radar system end application
  • b-2 special end application
  • 2.250 inches center to center distance between link and shaft holes
  • 0.458 inches distance between fork inside spread
  • b-2 aircraft end application
  • 2.250 inches center to center distance between link and shaft holes
  • 0.458 inches distance between fork inside spread
17P1F6052-1 NSN 1680-01-422-3388
  • aircraft c-17a end application
  • lever, remote control special features
6051-0026-01 NSN 1680-01-422-3398
  • aircraft c-17a end application
  • end fitting, assembly special features
17P1F6094-1 NSN 1680-01-422-3402
  • aircraft c-17a end application
  • guide, lever, flap-sl special features
3166259-1 NSN 1680-01-424-8127
  • pacer dawn end application
  • 1.000 inches center to center distance between link and shaft holes
  • 0.570 inches shaft end thickness
  • 0.500 inches link end thickness
  • 0.300 inches distance between fork inside spread
  • 0.900 inches overall width
  • b-2 aircraft end application
  • 3.873 inches center to center distance between link and shaft holes
  • 0.860 inches shaft end thickness
  • 0.890 inches link end thickness
  • 0.900 inches overall width
  • b-2 aircraft end application
  • 4.502 inches center to center distance between link and shaft holes
  • 0.860 inches shaft end thickness
  • 0.890 inches link end thickness
  • 0.900 inches overall width
  • b-2 aircraft end application
  • 3.873 inches center to center distance between link and shaft holes
  • 0.860 inches shaft end thickness
  • 0.890 inches link end thickness
  • 1.000 inches overall width
  • b-2 aircraft end application
  • 0.440 inches shaft end thickness
  • 0.890 inches link end thickness
  • 0.590 inches distance between fork inside spread
  • 1.000 inches overall width
  • b-2 aircraft end application
  • 0.440 inches shaft end thickness
  • 0.890 inches link end thickness
  • 0.590 inches distance between fork inside spread
  • 0.900 inches overall width
  • b-2 acft end application
  • 4.502 inches center to center distance between link and shaft holes
  • 0.860 inches shaft end thickness
  • 0.890 inches link end thickness
975943-6 Actuating Arm Assembly NSN 1680-01-428-7770
  • pacer dawn end application
  • 1.000 inches center to center distance between link and shaft holes
  • between 0.440 inches and 0.580 inches shaft end thickness
  • 0.500 inches link end thickness
  • aluminum alloy material
42305E514-1 NSN 1680-01-428-8770
9139766-10 NSN 1680-01-433-8109
  • helicopter, uh-60a/uh-60d end application
  • aluminum alloy material
  • b-52 aircraft end application
  • t.o. 16c1-10-2-4, fig 5, ind 21 special features
  • 1.312 inches overall width
  • f-15 aircraft end application
  • 2.875 inches center to center distance between link and shaft holes
17P3A1845-1 NSN 1680-01-436-9465
  • c-17a aircraft end application
  • 0.790 inches overall width
  • between 1.060 inches and 1.111 inches bore diameter
  • between 0.310 inches and 0.320 inches bore length
  • between 0.060 inches and 0.080 inches bore radius
  • splined bore type