Bell Cranks - Page 23 of 59

1465 part numbers
121CM10082-2 NSN 1680-00-717-2620
  • 0.811 inches bore diameter
  • 0.406 inches bore length
  • aluminum alloy material
121CM10109-1 NSN 1680-00-717-6351
  • 1.312 inches bore diameter
  • between 2.750 inches and 2.760 inches bore length
  • aluminum alloy material
121CM10109-2 NSN 1680-00-717-6352
  • 1.312 inches bore diameter
  • between 2.750 inches and 2.760 inches bore length
  • aluminum alloy material
121CM10055-2 NSN 1680-00-717-6355
305-637205-3 NSN 1680-00-719-7037
  • 0.500 inches bore diameter
  • aluminum alloy material
53-630553-1 NSN 1680-00-724-7627
94383-1 NSN 1680-00-727-9485
305-637207-3 NSN 1680-00-728-2256
  • 0.500 inches bore diameter
  • 2.060 inches bore length
  • aluminum alloy material
305-637208-3 NSN 1680-00-728-9399
  • 0.500 inches bore diameter
  • aluminum alloy material
786827-1 NSN 1680-00-730-5398
204-001-148-1 NSN 1680-00-731-7992 Cross Reference: 204-001-148-001
  • 1.000 inches bore diameter
  • 0.812 inches bore length
  • aluminum alloy material
204-001-963-1 NSN 1680-00-731-8095 Cross Reference: 204-001-963-001
  • between 0.749 inches and 0.750 inches counterbore diameter
  • 0.800 inches counterbore depth
  • 0.730 inches bore diameter
  • between 6.292 inches and 6.297 inches bore length
  • 5.266 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
791573-1 NSN 1680-00-734-3599
  • fulcrum shaft features provided
3F31067-103 NSN 1680-00-736-7258
53-32556-5 NSN 1680-00-738-2637
  • 0.375 inches bore diameter
  • 3.442 inches bore length
  • f-4 aircraft end application
  • used on photo flash mechanism, upper special features
  • aluminum alloy material
53-32556-6 NSN 1680-00-738-2663
4F54357-103B NSN 1680-00-738-4890 Cross Reference: 4F54112-101A, 4F54357-101A, 4F54357-103A
  • c-5 aircraft end application
  • steel material
4F54357-104B NSN 1680-00-738-4891 Cross Reference: 4F54112-102A, 4F54357-102A, 4F54357-104A
32-65066-1 NSN 1680-00-739-3170
  • 1.000 inches bore diameter
  • 1.070 inches bore length
  • f-4 aircraft end application
  • aluminum alloy material
32-62023-9 NSN 1680-00-739-3221
  • f-4 aircraft end application
  • aluminum alloy material
32-63006-15 NSN 1680-00-739-3222
32-30166-1 NSN 1680-00-739-3229
  • 0.150 inches bore diameter
  • aluminum alloy material
204-060-743-5 NSN 1680-00-739-4577 Cross Reference: 204-060-743-005
  • 0.449 inches bore length
  • 3.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • zinc surface treatment
  • clevis ends style designator
  • fuselage sect., acft fsc application data
32-19357-5 NSN 1680-00-740-3757
  • f-4 aircraft end application
  • steel material
  • used on flap, leading edge, center supplementary features
32-19357-6 NSN 1680-00-740-3758
  • f-4 aircraft end application
  • steel material
  • used on mech. flap leading edge, center supplementary features