Remote Control Levers - Page 20 of 32

798 part numbers
1215401-101 NSN 1680-01-019-7693 Cross Reference: 1202608-101
  • 1.275 inches major diameter
  • 39 spline quantity
  • 1.187 inches minor diameter
  • splined bore type
  • two bushings in fork tongue special features
K652095-5 NSN 1680-01-022-1775
  • between 0.317 inches and 0.319 inches major diameter
  • 24 serration quantity
  • between 0.292 inches and 0.294 inches minor diameter
  • serrated bore type
  • split end screw clamping feature features provided
216-78327-103 NSN 1680-01-029-4368 Cross Reference: 216-78327-101
  • 0.440 inches overall width
  • between 0.260 inches and 0.263 inches bore diameter
  • 0.380 inches bore length
  • plain straight bore type
  • 1.950 inches center to center distance between link and shaft holes
715017 NSN 1680-01-033-4590
4050822 NSN 1680-01-037-5611
  • aircraft engine f100-pw-100 end application
  • stainless steel material
A51F23608-7 NSN 1680-01-038-7737
  • 0.187 inches bore diameter
  • 0.690 inches bore length
  • plain straight bore type
  • aluminum alloy material
18-50828-1 NSN 1680-01-049-5364
  • plain straight bore type
  • 8.100 inches center to center distance between link and shaft holes
  • 0.290 inches link end thickness
  • 0.193 inches link end hole diameter
A15P2519-2 NSN 1680-01-052-0648
  • between 0.350 inches and 0.353 inches major diameter
  • 36 serration quantity
  • 0.345 inches minor diameter
  • serrated bore type
  • steel material
16P2001-803 NSN 1680-01-052-5325 Cross Reference: 16P2001-3, 16P2001-5, 16P2001-801
  • aircraft model f-16; engine control throttle end application
16P2002-803 NSN 1680-01-052-6081 Cross Reference: 16P2002-5, 16P2002-801
  • aircraft model f-16; throttle, engine control end application
16K2856-4 NSN 1680-01-060-4302 Cross Reference: 16K2856-2
  • between 0.499 inches and 0.500 inches bore diameter
  • 1.223 inches bore length
  • plain straight bore type
  • 1.500 inches center to center distance between link and shaft holes
  • 0.550 inches shaft end thickness
D114927-503 NSN 1680-01-079-6195 Cross Reference: D114927-501
  • 1.000 inches overall width
  • aircraft f-16; aces 2-aircraft ejection seat end application
  • aluminum alloy material
70400-02620-041 NSN 1680-01-079-6379
  • uh-60a helicopter end application
  • plain straight bore type
70400-01608-042 NSN 1680-01-092-1983
  • uh-60a helicopter end application
  • 3.000 inches center to center distance between link and shaft holes
  • aluminum alloy material
  • anodize surface treatment
70217-02708-043 NSN 1680-01-095-7189
  • 0.191 inches bore diameter
  • between 0.740 inches and 0.750 inches bore length
  • plain straight bore type
  • aluminum alloy material
70217-01031-045 NSN 1680-01-096-1139
70217-01031-044 NSN 1680-01-096-1140
70217-01031-043 NSN 1680-01-096-1141
70217-01031-042 NSN 1680-01-096-1142
70217-01031-041 NSN 1680-01-096-1143
70217-01031-046 NSN 1680-01-096-1144
A22482-001 NSN 1680-01-096-5550 Cross Reference: A22482
  • uh-60, rotary wing aircraft end application
70217-01000-065 NSN 1680-01-096-5552
70217-01000-064 NSN 1680-01-096-5553
9059-30-1 NSN 1680-01-101-9838