Bell Cranks - Page 38 of 59

1465 part numbers
123CM13056-601 NSN 1680-01-186-6620 Cross Reference: 123CM13056-401
  • between 0.748 inches and 0.749 inches bore diameter
  • between 3.438 inches and 3.448 inches bore length
  • aluminum alloy material
  • anodize surface treatment
123CM43221-601 NSN 1680-01-186-6621 Cross Reference: 123CM43221-1
  • aluminum alloy material
3-40128-503 NSN 1680-01-187-4388
  • t-38 acft end application
  • steel material
  • raised face pivot hole w/heel, clevis one end style designator
300365-101 NSN 1680-01-187-8393
  • 0.625 inches bore diameter
  • 0.250 inches bore length
  • kc-135r aircraft end application
  • aluminum alloy material
  • mil-a-22771 military specification single material response material specification
123AMM41132-601 NSN 1680-01-195-2636 Cross Reference: 123AMM41132-1
  • aluminum alloy material
123AMM41134-601 NSN 1680-01-195-2637 Cross Reference: 123AMM41134-1
  • aluminum alloy material
123AMM41135-601 NSN 1680-01-195-2638 Cross Reference: 123AMM41135-1
  • aluminum alloy material
123AMM41135-602 NSN 1680-01-195-2639 Cross Reference: 123AMM41135-2
  • aluminum alloy material
L6312013-001 NSN 1680-01-199-5306
  • 0.625 inches bore diameter
  • 7.990 inches bore length
  • aircraft model b-1b end application
  • titanium material
123AMM41132-602 NSN 1680-01-205-5971
L5873483-001 NSN 1680-01-206-6364
  • b-1b acft end application
3C13050-101 NSN 1680-01-220-4128
  • c141b aircraft end application
  • t.o.1c-141b-4-6, fig-45, ind10 special features
  • aircraft brake system fsc application data
70400-08166-041 NSN 1680-01-221-2863
  • bearing and fulcrum bore features provided
65661-06260-056 NSN 1680-01-222-8438 Cross Reference: 65661-06260-047, 65661-06260-054
65661-06260-055 NSN 1680-01-222-8439 Cross Reference: 65661-06260-051
  • h53 acft end application
  • airframe structural components fsc application data
123CM41220-601 NSN 1680-01-223-3122 Cross Reference: 123CM41220-1
7-311511117-13 NSN 1680-01-224-2262 Cross Reference: 7-311511117-9
  • ah-64 airframe, rotary wing aircraft end application
7-311511127-7 NSN 1680-01-224-2263 Cross Reference: 7-311511127-5
  • ah-64 airframe, rotary wing aircraft end application
7-311523014-5 NSN 1680-01-224-6688
  • ah-64 airframe, rotary wing aircraft end application
7-311511125-17 NSN 1680-01-225-2538 Cross Reference: 7-311511125-13
  • ah-64 airframe, rotary wing aircraft end application
S6130-80069-6 NSN 1680-01-226-6297
7-311660022-11 NSN 1680-01-232-7712 Cross Reference: 7-311660022, 7-311660022-5
  • ah-64 airframe, rotary wing aircraft end application
145C2510-4 NSN 1680-01-232-7717
145C2516-12 NSN 1680-01-232-7719
E10-09537-1 NSN 1680-01-232-9184
  • 0.873 inches bore diameter
  • between 0.800 inches and 0.810 inches bore length
  • aluminum alloy material
  • clevis ends style designator