Bell Cranks - Page 11 of 59
1465 part numbers
S14-30-2430
NSN 1680-00-397-1513
Cross Reference:
1560H19-169-1, SWM79
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0.375 inches bore diameter
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0.750 inches bore length
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steel material
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0.875 inches bore diameter
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0.125 inches bore length
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1.750 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.189 inches 2nd end end hole/ball diameter
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aluminum alloy material
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0.623 inches bore diameter
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between 0.699 inches and 0.701 inches bore length
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between 0.250 inches and 0.254 inches bore diameter
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between 0.218 inches and 0.224 inches bore length
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2.810 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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steel material
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passivate surface treatment
12K3096-11
NSN 1680-00-420-3119
Cross Reference:
12K3096-9
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0.625 inches counterbore diameter
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between 1.260 inches and 1.280 inches bore length
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1.100 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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aluminum alloy material
12C490-5
NSN 1680-00-420-3179
Cross Reference:
12C490-3
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between 0.752 inches and 0.753 inches counterbore diameter
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between 0.224 inches and 0.229 inches counterbore depth
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between 0.625 inches and 0.630 inches bore diameter
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between 1.214 inches and 1.224 inches bore length
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titanium alloy material
12C333-5
NSN 1680-00-420-8504
Cross Reference:
12C333-3
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between 0.751 inches and 0.752 inches counterbore diameter
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between 0.224 inches and 0.229 inches counterbore depth
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between 0.625 inches and 0.630 inches bore diameter
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between 1.964 inches and 1.974 inches bore length
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6.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
2-73881-3
NSN 1680-00-421-5402
Cross Reference:
2-73881-1
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t-38 aircraft end application
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t-38 aircraft end application
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between 0.873 inches and 0.874 inches bore diameter
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0.790 inches bore length
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aluminum alloy material
4F63137-101A
NSN 1680-00-435-9223
Cross Reference:
4F63137-101B
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c-5 aircraft end application
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bearing features provided
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between 0.900 inches and 0.901 inches counterbore diameter
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0.375 inches counterbore depth
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0.830 inches bore diameter
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between 5.120 inches and 5.125 inches bore length
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steel material
4F52816-104B
NSN 1680-00-438-3995
Cross Reference:
4F52816-104A
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c-5 aircraft end application
4F52816-103B
NSN 1680-00-438-3996
Cross Reference:
4F52816-103A, 4F54113-105B
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2.460 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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aluminum alloy material
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raised face pivot hole w/heel, clevis one end style designator
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0.313 inches bore diameter
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0.938 inches bore length
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4.560 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.190 inches 2nd end end hole/ball diameter
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aluminum alloy material