Bell Cranks - Page 24 of 59

1465 part numbers
6-54873-1 NSN 1680-00-753-8962 Cross Reference: 6-55554873-1
  • fulcrum shaft features provided
907327-101 NSN 1680-00-757-8037
204-001-373-001 NSN 1680-00-758-3668 Cross Reference: 204-001-373-1
  • 1.000 inches bore diameter
  • between 0.802 inches and 0.812 inches bore length
  • 3.750 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.250 inches 2nd end end hole/ball diameter
  • aluminum alloy material
6-54864-1 NSN 1680-00-758-8595
  • between 0.803 inches and 0.805 inches bore diameter
  • between 3.980 inches and 4.020 inches bore length
  • 1.125 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
368330-7 NSN 1680-00-758-8867 Cross Reference: 368330-1
  • between 0.501 inches and 0.502 inches bore diameter
  • 0.826 inches bore length
  • 3.570 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
363727-6 NSN 1680-00-758-8872
  • between 1.437 inches and 1.438 inches counterbore diameter
  • between 0.360 inches and 0.370 inches counterbore depth
  • between 1.249 inches and 1.262 inches bore diameter
  • 1.594 inches bore length
  • aluminum alloy material
204-030-482-2 NSN 1680-00-759-7486 Cross Reference: 204-030-482-002
  • 0.250 inches bore diameter
  • 0.080 inches bore length
  • 1.790 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.125 inches 1st end end hole/ball diameter
  • flat, one or more holes both arms style designator
204-030-488-002 NSN 1680-00-759-7487 Cross Reference: 204-030-488-2
  • between 0.188 inches and 0.189 inches bore diameter
  • 0.640 inches bore length
  • 1.720 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • copper alloy material
12C851-807 NSN 1680-00-761-5466 Cross Reference: 12C851-803
  • between 0.752 inches and 0.753 inches counterbore diameter
  • between 0.224 inches and 0.229 inches counterbore depth
  • between 0.625 inches and 0.630 inches bore diameter
  • between 1.464 inches and 1.474 inches bore length
  • titanium alloy material
12C851-808 NSN 1680-00-761-5467 Cross Reference: 12C851-804
  • between 0.752 inches and 0.753 inches counterbore diameter
  • between 0.224 inches and 0.229 inches counterbore depth
  • between 0.625 inches and 0.630 inches bore diameter
  • between 1.464 inches and 1.474 inches bore length
  • titanium alloy material
12K3096-12 NSN 1680-00-762-0231 Cross Reference: 12K3096-10
  • 0.625 inches counterbore diameter
  • 0.490 inches counterbore depth
  • between 1.260 inches and 1.280 inches bore length
  • 1.100 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.191 inches 2nd end end hole/ball diameter
2-74126-1 NSN 1680-00-765-1076
  • 0.876 inches counterbore diameter
  • 0.920 inches counterbore depth
  • 0.750 inches bore diameter
  • 1.250 inches bore length
  • feat criticality code justification
134P10083-1 NSN 1680-00-765-7909
  • 0.938 inches bore diameter
  • 0.125 inches bore length
  • fuselage sect., acft fsc application data
134P10082-3 NSN 1680-00-765-8572
  • 1.000 inches bore diameter
  • flat-bolt circle around pivot hole style designator
  • fuselage sect., acft fsc application data
782194-1 NSN 1680-00-765-9288
782349-1 NSN 1680-00-765-9307
4F73380-101B NSN 1680-00-766-6048 Cross Reference: 4F73380-101A
  • 5.230 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
  • flat, one or more holes both arms style designator
124C011-1-53 NSN 1680-00-767-9736 Cross Reference: 124C011-1
  • between 1.125 inches and 1.127 inches bore diameter
  • 0.750 inches bore length
  • 2.250 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.190 inches 2nd end end hole/ball diameter
3-13486-1 NSN 1680-00-768-0975
  • 0.748 inches bore diameter
  • between 0.760 inches and 0.770 inches bore length
  • 2.750 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.190 inches 2nd end end hole/ball diameter
  • magnesium alloy material
2-13009-5 NSN 1680-00-768-9478
  • 0.257 inches bore diameter
  • 0.625 inches bore length
  • feat criticality code justification
  • magnesium alloy material
47-727-160-1 NSN 1680-00-769-6593
  • 1.029 inches bore diameter
  • between 0.330 inches and 0.335 inches bore length
  • aluminum alloy material
782098-5 NSN 1680-00-775-5558
  • between 1.312 inches and 1.313 inches bore diameter
  • 4.855 inches bore length
  • 2.350 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
4F61014-101A NSN 1680-00-775-7970
  • c-5 aircraft end application
2811887 NSN 1680-00-776-5966
8-46901-3 NSN 1680-00-776-6048