Remote Control Levers - Page 29 of 32

798 part numbers
KC52006-001 NSN 1680-01-481-2318
  • 1.760 inches overall width
  • 4.500 inches center to center distance between link and shaft holes
  • 1.760 inches shaft end thickness
  • 1.000 inches link end thickness
  • aluminum alloy material
3F13490026E NSN 1680-01-481-3119
  • f18 e/f fighter aircraft end application
  • agav criticality code justification
109559-2 Torsion Tube Fitting NSN 1680-01-481-6146
  • eh101 helicopter end application
  • 1.100 inches center to center distance between link and shaft holes
  • 0.300 inches shaft end thickness
  • black hard anodize special features
  • aluminum material
133-550047-7 NSN 1680-01-482-2052
  • t-6 joint primary acft. trainer (j-pat) end application
133-524038-5 NSN 1680-01-482-4027
  • joint primary aircraft trainer, t-6 end application
133-524050-5 NSN 1680-01-482-4038
  • joint primary aircraft trainer, t-6 end application
17P3A1667-1 Ramp Toe Actuator Arm Assembly Idler NSN 1680-01-483-5315
  • c-17 globemaster end application
  • plain straight bore type
  • aluminum alloy material
4316764 NSN 1680-01-484-8126
4316765 NSN 1680-01-485-5158
806154-1 NSN 1680-01-491-0197 Cross Reference: 806154
  • 0.525 inches overall width
  • aircraft b-2 bomber (atb) end application
  • plain straight bore type
  • 2.550 inches center to center distance between link and shaft holes
  • 0.370 inches shaft end thickness
93303-1 NSN 1680-01-491-4168
  • c-5 aircraft end application
545-7395-002 Arm-off Flag NSN 1680-01-493-3260
  • 522-1859-066 indicator, distance end application
  • nha 545-7422-027 counter assembly distance 339d-1 special features
730-5914 NSN 1680-01-493-8774 Cross Reference: 730-5912, 74-800072-130, 74-800072-136, 74-800072-140
  • f18e/f end application
  • agav criticality code justification
4423-060 NSN 1680-01-498-1949
105531-1 Handle NSN 1680-01-500-4798 Cross Reference: 105531
  • hh-60 wing panel end application
  • 2.065 inches center to center distance between link and shaft holes
  • 0.250 inches shaft end thickness
  • 0.250 inches link end thickness
  • copilot side special features
105531-2 Handle NSN 1680-01-500-4799 Cross Reference: 105531
  • hh-60 wing panel end application
  • 2.065 inches center to center distance between link and shaft holes
  • 0.250 inches shaft end thickness
  • 0.250 inches link end thickness
  • pilot side special features
74A733070-1006 NSN 1680-01-500-6655 Cross Reference: 10400002, 3930AS630-2
  • umbilical connector right hand side special features
14711-203-3 NSN 1680-01-502-2518
  • c-130 aircraft end application
  • part of the cargo handling system special features
9-65341-2 NSN 1680-01-503-0721 Cross Reference: 9-65341
  • c-135 aircraft end application
0411037-15 NSN 1680-01-506-2194
  • c130k hercules end application
74A672466-2003 NSN 1680-01-507-0744 Cross Reference: 74A672466
17P2G5513-501 NSN 1680-01-507-8467
  • c-17 acft end application
  • spline shaft securing method
  • titanium material
  • paint surface treatment
17P2G5513-1 NSN 1680-01-507-8468
  • c-17 acft end application
  • spline shaft securing method
  • titanium material
  • paint surface treatment
74A733108-2001 NSN 1680-01-513-0122 Cross Reference: 10381102
  • cf18 aircraft launcher end application
  • 1.406 inch long; 0.562 inch diameter one end special features
31015 NSN 1680-01-514-7544
  • b-52h acft end application