Bell Cranks - Page 28 of 59

1465 part numbers
114C1168-1 NSN 1680-00-830-4340
  • 0.245 inches counterbore depth
  • 1.350 inches bore diameter
  • 4.690 inches bore length
  • magnesium material
  • fuselage sect., acft fsc application data
114C1168-2 NSN 1680-00-830-4341
  • 0.245 inches counterbore depth
  • 1.350 inches bore diameter
  • 4.690 inches bore length
  • fuselage sect., acft fsc application data
114C1231-1 NSN 1680-00-830-4348
  • 1.580 inches bore diameter
  • 2.750 inches bore length
  • 7.500 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • fuselage sect., acft fsc application data
114C1230-1 NSN 1680-00-831-2262
  • 1.749 inches counterbore diameter
  • 0.235 inches counterbore depth
  • 1.580 inches bore diameter
  • 1.960 inches bore length
  • 4.350 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
4C90000-105A NSN 1680-00-833-3947 Cross Reference: 0501146-5
  • between 1.062 inches and 1.063 inches bore diameter
  • 9.042 inches bore length
114C3310-20 NSN 1680-00-834-2237
  • between 1.812 inches and 1.814 inches bore diameter
  • between 3.650 inches and 3.670 inches bore length
  • magnesium material
  • chromate surface treatment
  • fuselage sect., airframe fsc application data
65302-12534-041 NSN 1680-00-835-2589
  • between 0.578 inches and 0.586 inches bore diameter
  • 1.190 inches bore length
  • aluminum alloy material
12S708-801 NSN 1680-00-840-1255
  • f-111 aircraft end application
215-28161-4 NSN 1680-00-852-9195
  • mil-a-22771, alloy 7075, t73 special features
  • aluminum alloy material
215-28301-3 NSN 1680-00-852-9202
  • between 0.748 inches and 0.753 inches bore diameter
  • 0.690 inches bore length
215-28301-4 NSN 1680-00-852-9206
  • between 0.748 inches and 0.753 inches bore diameter
  • 0.690 inches bore length
215-38105-2 NSN 1680-00-853-0180
  • between 0.748 inches and 0.749 inches bore diameter
  • 2.218 inches bore length
215-68104-3 NSN 1680-00-853-1088
  • 3.530 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • magnesium material
  • raised face pivot hole, clevis both ends style designator
215-78104-7 NSN 1680-00-853-1983
  • magnesium material
215-78104-12 NSN 1680-00-853-1984 Cross Reference: 215-78104-8
215-78108-3 NSN 1680-00-853-2001
  • between 0.875 inches and 0.880 inches bore diameter
  • between 1.650 inches and 1.700 inches bore length
215-78108-4 NSN 1680-00-853-2002
  • between 0.875 inches and 0.880 inches bore diameter
  • between 1.650 inches and 1.700 inches bore length
215-88021-2 NSN 1680-00-853-2323
  • 1.562 inches bore diameter
  • 2.880 inches bore length
  • 4.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.625 inches 2nd end end hole/ball diameter
  • steel material
215-88109-3 NSN 1680-00-853-2364
215-88109-4 NSN 1680-00-853-2365
  • 0.873 inches bore diameter
  • between 2.069 inches and 2.070 inches bore length
  • 3.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.375 inches 2nd end end hole/ball diameter
  • aluminum alloy material
12S712-1 NSN 1680-00-853-7030
  • f-111 aircraft end application
S6140-62124-5 NSN 1680-00-858-1473
  • aluminum alloy material
  • anodize surface treatment
S6140-62620-8 NSN 1680-00-858-1707
  • aluminum alloy material
  • anodize surface treatment
S6140-62602-005 NSN 1680-00-858-1723 Cross Reference: S6140-62602-5
  • aluminum alloy material
  • anodize surface treatment
4C90000-103A NSN 1680-00-860-3650 Cross Reference: 0501146-3
  • between 1.062 inches and 1.063 inches bore diameter
  • 9.042 inches bore length