Bell Cranks - Page 39 of 59

1465 part numbers
7-311512085-7 NSN 1680-01-233-8362
107C2253-8 NSN 1680-01-237-9760
  • helicopter model h-46 end application
  • 4.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • clevis ends style designator
380223-3 NSN 1680-01-240-3756
  • steel material
  • raised face pivot and end holes style designator
75A613780-1003 NSN 1680-01-242-3918
  • 0.637 inches bore diameter
  • 1.550 inches bore length
  • aircraft model av-8 end application
  • aluminum alloy material
7-311661003 NSN 1680-01-243-1084 Cross Reference: 7-311660003, 7-311661003-7
  • ah-64 airframe, rotary wing aircraft end application
123CM12025-503 NSN 1680-01-248-9173 Cross Reference: 123CM12025-501
  • aircraft model e-2c end application
  • aluminum alloy material
123CM12025-504 NSN 1680-01-248-9174
  • aircraft model c-2/e-2 end application
  • aluminum material
7-311517070-13 NSN 1680-01-248-9971 Cross Reference: 7-311517070, 7-311517070-7
  • apache airframe ah-64 end application
65-13005-8 NSN 1680-01-251-8945
  • aircraft accessory equipment fsc application data
7-311512085-9 NSN 1680-01-252-0380 Cross Reference: 7-311512085-7
  • ah-64 airframe, rotary wing aircraft end application
7-311518020-5 NSN 1680-01-253-8764 Cross Reference: 7-311518020
  • ah-64 airframe rotary wing aircraft end application
75A612302-1001 NSN 1680-01-256-7952
  • 0.750 inches counterbore diameter
  • 0.229 inches counterbore depth
  • 0.625 inches bore diameter
  • 1.005 inches bore length
  • 2.400 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
75A353360-2003 NSN 1680-01-256-8382
  • 1.000 inches bore diameter
  • 1.348 inches bore length
  • titanium material
75A612004-1001 NSN 1680-01-261-3098
  • 0.750 inches counterbore diameter
  • 0.300 inches counterbore depth
  • 0.625 inches bore diameter
  • 0.281 inches bore length
  • 3.304 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
75A612304-1001 NSN 1680-01-261-3099
  • between 0.749 inches and 0.750 inches counterbore diameter
  • between 0.229 inches and 0.300 inches counterbore depth
  • 0.625 inches bore diameter
  • 2.146 inches bore length
  • 2.404 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
75A612300-2003 NSN 1680-01-261-3100
  • 1.000 inches bore diameter
  • 1.510 inches bore length
  • 2.400 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
75A612003-1001 NSN 1680-01-266-1003
  • 1.188 inches counterbore diameter
  • 0.260 inches counterbore depth
  • 1.062 inches bore diameter
  • 1.785 inches bore length
  • 2.625 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
75A612301-2001 NSN 1680-01-271-4551
  • 0.999 inches bore diameter
  • 2.290 inches bore length
  • aluminum alloy material
  • anodize surface treatment
68A411074-2007 NSN 1680-01-271-5575 Cross Reference: 68A411074-2005
70400-02209-046 NSN 1680-01-273-7591
  • uh-60 rotary wing aircraft end application
70400-02209-045 NSN 1680-01-273-7592
  • uh-60 rotary wing aircraft end application
413-10970-1 NSN 1680-01-279-3176
75A612306-1001 NSN 1680-01-286-5683
  • aluminum alloy material
7406-76211-3 NSN 1680-01-304-4941
  • 0.193 inches bore diameter
  • 0.120 inches bore length
  • mc-130h acft end application
  • 1.670 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.776 inches 1st end end hole/ball diameter
16S1531-15 NSN 1680-01-306-8327 Cross Reference: 16S1531-11, 16S1531-9
  • 0.6275 inches bore diameter
  • 2.950 inches bore length
  • aim 7/aim 120 launcher end application
  • 0.3125 inches 2nd end end hole/ball diameter
  • aluminum material