Bell Cranks - Page 30 of 59

1465 part numbers
65403-07620-041 NSN 1680-00-915-6721 Cross Reference: 65403-07618-041
  • between 0.873 inches and 0.874 inches bore diameter
  • between 0.839 inches and 0.844 inches bore length
  • 3.596 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • clevis ends style designator
65404-03115-041 NSN 1680-00-915-6906
65404-03116-041 NSN 1680-00-915-6907
  • between 2.250 inches and 2.251 inches bore diameter
  • between 1.090 inches and 1.092 inches bore length
  • aluminum alloy material
65404-03611-041 NSN 1680-00-915-6915
  • 0.683 inches 1st end slot width
  • 0.8741 inches bore diameter
  • 4.540 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.4373 inches 2nd end end hole/ball diameter
  • aluminum alloy material
65404-03112-041 NSN 1680-00-915-7233
  • between 0.748 inches and 0.749 inches bore diameter
  • between 0.776 inches and 0.781 inches bore length
  • 4.672 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • clevis ends style designator
65404-03114-041 NSN 1680-00-915-7234
  • 0.874 inches bore diameter
  • between 0.839 inches and 0.844 inches bore length
  • aluminum alloy material
65403-06611-041 NSN 1680-00-915-7238
  • between 1.248 inches and 1.249 inches bore diameter
  • between 0.925 inches and 0.930 inches bore length
  • aluminum alloy material
65403-06613-041 NSN 1680-00-915-7240
65405-06012-041 NSN 1680-00-915-7371
  • between 1.405 inches and 1.406 inches bore diameter
  • 3.430 inches bore length
  • aluminum alloy material
65403-02624-041 NSN 1680-00-915-7438
3P22013-108 NSN 1680-00-916-0291
10-1013 Throttle Lever Assembly-outboard Quadrant Assembly NSN 1680-00-918-3396
  • t-37 aircraft end application
  • flat, offset both arms style designator
288-337534-21 NSN 1680-00-918-4452
  • 0.563 inches bore diameter
  • 1.062 inches bore length
  • aluminum alloy material
209-001-107-1 NSN 1680-00-918-8132
53-32558-9 NSN 1680-00-919-3700
  • 0.438 inches bore diameter
  • 3.322 inches bore length
  • bell crank has 3 arms, all slotted special features
  • aluminum alloy material
3P22013-107 NSN 1680-00-919-3928
369N2684 NSN 1680-00-922-9373 Cross Reference: 10363508, 369A7527
  • 0.900 inches bore length
  • 5.270 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • magnesium material
  • dichromate surface treatment
  • raised face pivot hole, clevis both ends style designator
32-64010-301 NSN 1680-00-927-4083
  • between 1.437 inches and 1.439 inches bore diameter
  • 2.130 inches bore length
  • 3.640 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.314 inches 1st end end hole/ball diameter
  • aluminum alloy material
12L235-1 NSN 1680-00-927-6635
  • 0.375 inches bore diameter
  • 0.655 inches bore length
  • aluminum alloy material
12M9583-1 NSN 1680-00-928-7697
  • between 0.495 inches and 0.500 inches bore diameter
  • 1.062 inches bore length
  • aluminum alloy material
  • raised face pivot hole, clevis both ends style designator
32-65830-9 NSN 1680-00-928-9143
  • 2.172 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 0.191 inches 1st end end hole/ball diameter
  • aluminum alloy material
  • raised faced holes, offset arm style designator
3822373-1 NSN 1680-00-928-9182
  • aluminum alloy material
369N2672 NSN 1680-00-933-1310 Cross Reference: 369A7704
  • between 0.249 inches and 0.250 inches bore diameter
  • between 0.870 inches and 0.875 inches bore length
  • 2.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • dichromate surface treatment
  • control column, aircraft fsc application data
369N2680 NSN 1680-00-933-1311 Cross Reference: 369A7702
  • between 0.249 inches and 0.250 inches bore diameter
  • between 0.870 inches and 0.875 inches bore length
  • 3.160 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • dichromate surface treatment
  • control column, aircraft fsc application data
S6140-62122 NSN 1680-00-936-1197
  • between 1.436 inches and 1.437 inches bore diameter
  • between 0.794 inches and 0.799 inches bore length
  • 5.719 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • steel material
  • cadmium and paint surface treatment