Bell Cranks - Page 14 of 59

1465 part numbers
S6140-62144-005 NSN 1680-00-458-7766 Cross Reference: S6140-62144, S6140-62144-5
  • aluminum alloy material
  • anodize surface treatment
4F73151-101B NSN 1680-00-461-6062
  • 4.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • aluminum alloy material
  • raised faced holes, offset both arms style designator
53G970701-46 NSN 1680-00-471-1791
  • 0.7515 inches bore diameter
  • 2.390 inches bore length
  • steel material
265-522079-11 NSN 1680-00-476-1611
  • 4.312 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
265-522079-12 NSN 1680-00-476-1612
  • 4.312 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
C4C1578-1 NSN 1680-00-476-2708
  • 0.930 inches bore diameter
  • 8.150 inches bore length
  • steel material
4C27084-109C NSN 1680-00-477-5417
  • 1.120 inches bore diameter
  • 3.620 inches bore length
  • aluminum alloy material
  • anodize surface treatment
68A411074-2006 NSN 1680-00-477-5478
  • titanium material
12C451-821 NSN 1680-00-477-9138
  • between 0.814 inches and 0.815 inches counterbore diameter
  • between 0.239 inches and 0.244 inches counterbore depth
  • between 0.687 inches and 0.692 inches bore diameter
  • between 1.595 inches and 1.605 inches bore length
  • titanium alloy material
1128LM40608-11 NSN 1680-00-483-2061
  • between 0.437 inches and 0.439 inches bore diameter
  • steel material
  • cadmium surface treatment
1128LM40501-11 NSN 1680-00-483-2067 Cross Reference: 128LM40501-11
1128LM40608-12 NSN 1680-00-483-2068
  • between 0.437 inches and 0.439 inches bore diameter
  • steel material
  • cadmium surface treatment
S6140-20006-005 NSN 1680-00-485-9636
  • between 1.436 inches and 1.437 inches bore diameter
  • between 1.941 inches and 1.946 inches bore length
  • aluminum alloy material
  • anodize surface treatment
  • cyclic pitch control, rotor, helicopter fsc application data
A51M10517-3 NSN 1680-00-486-3464
  • f-14a/b/d acft end application
  • aluminum alloy material
214-001-500-1 NSN 1680-00-487-2668
212-060-745-1 NSN 1680-00-489-9907
212-060-747-001 NSN 1680-00-489-9908 Cross Reference: 212-060-747-1
  • 0.749 inches bore diameter
  • 0.750 inches bore length
  • aluminum alloy material
134CM10035-9 NSN 1680-00-490-1114 Cross Reference: 134CM10035-5
  • 0.312 inches bore diameter
  • between 1.750 inches and 1.760 inches bore length
  • 2.906 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • control column, aircraft fsc application data
32-63044-7 NSN 1680-00-492-3061
32-63043-11 NSN 1680-00-493-8316
4F61077-105A NSN 1680-00-494-7739 Cross Reference: 4F61077-101A
  • aluminum alloy material
S6120-62132-035 NSN 1680-00-497-7373 Cross Reference: S6120-62132-35
4C51790-105A NSN 1680-00-498-3174 Cross Reference: 4C51790-101A
  • c-5 acft end application
A51G10576-2 NSN 1680-00-498-4115
  • between 0.750 inches and 0.751 inches bore diameter
  • 0.875 inches bore length
  • titanium material
  • fuselage, airframe fsc application data
4C22101-105A NSN 1680-00-499-0806