Bell Cranks - Page 31 of 59

1465 part numbers
65400-11113-041 NSN 1680-00-938-9606
  • 0.250 inches bore diameter
  • 0.875 inches bore length
  • four bushings required for arm holes special features
  • aluminum alloy material
  • anodize surface treatment
65400-11123-041 NSN 1680-00-938-9610
65400-11122-041 NSN 1680-00-938-9615
  • aluminum alloy material
  • anodize surface treatment
65400-11112-041 NSN 1680-00-938-9616
65207-03002-123 NSN 1680-00-938-9652
  • steel material
65403-02624-042 NSN 1680-00-938-9702
3C11295-111 NSN 1680-00-939-3718
3C11295-109 NSN 1680-00-939-6423
65401-02424-042 NSN 1680-00-941-3265
65402-02133-041 NSN 1680-00-941-3266 Cross Reference: 65402-02128-041
  • 0.749 inches bore diameter
  • between 0.776 inches and 0.781 inches bore length
  • 3.666 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
65402-02129-041 NSN 1680-00-941-3267
  • 0.749 inches bore diameter
  • 0.778 inches bore length
  • surface treatment: chemical film special features
  • aluminum alloy material
65403-02630-041 NSN 1680-00-941-3269
  • surface treatment: chemical film special features
  • aluminum alloy material
65401-03411-041 NSN 1680-00-941-3295
  • 0.749 inches bore diameter
  • 1.088 inches bore length
  • 3.466 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
65402-03113-041 NSN 1680-00-941-3305 Cross Reference: 65402-03112-041, V6540-03113-041
  • aluminum alloy material
  • anodize surface treatment
65403-03611-041 NSN 1680-00-941-3306
65207-03002-122 NSN 1680-00-941-3396
  • steel material
53-32558-10 NSN 1680-00-942-9241
  • 0.438 inches bore diameter
  • 3.322 inches bore length
  • f-4 aircraft end application
  • bellcrank has three arms, two slotted special features
  • aluminum alloy material
369N2664 NSN 1680-00-943-0824 Cross Reference: 369A7602
  • between 3.417 inches and 3.427 inches bore length
  • 3.990 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • magnesium alloy material
  • anodize surface treatment
265-522076-1 NSN 1680-00-960-0771
  • aluminum alloy material
265-522076-2 NSN 1680-00-960-0772
  • aluminum alloy material
265-522080-21 NSN 1680-00-960-0787
  • 0.901 inches counterbore diameter
  • between 0.340 inches and 0.438 inches counterbore depth
  • 0.593 inches 1st end slot width
  • 0.781 inches bore diameter
  • 2.625 inches bore length
285-524018-11 NSN 1680-00-963-7189
  • 0.625 inches bore diameter
  • 5.500 inches bore length
  • 3.000 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
205-001-906-1 NSN 1680-00-966-6103 Cross Reference: 205-001-906-001
  • between 0.740 inches and 0.750 inches bore length
  • 3.850 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • fuselage sect., acft fsc application data
12C765-3 NSN 1680-00-967-4253
  • 0.813 inches bore diameter
  • 0.260 inches bore length
  • aluminum alloy material
128LM10151-5 NSN 1680-00-970-9300