Bell Cranks - Page 38 of 59
1465 part numbers
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between 0.748 inches and 0.749 inches bore diameter
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between 3.438 inches and 3.448 inches bore length
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aluminum alloy material
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anodize surface treatment
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t-38 acft end application
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steel material
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raised face pivot hole w/heel, clevis one end style designator
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0.625 inches bore diameter
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0.250 inches bore length
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kc-135r aircraft end application
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aluminum alloy material
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mil-a-22771 military specification single material response material specification
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0.625 inches bore diameter
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7.990 inches bore length
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aircraft model b-1b end application
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titanium material
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b-1b acft end application
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c141b aircraft end application
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t.o.1c-141b-4-6, fig-45, ind10 special features
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aircraft brake system fsc application data
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bearing and fulcrum bore features provided
65661-06260-056
NSN 1680-01-222-8438
Cross Reference:
65661-06260-047, 65661-06260-054
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h53 acft end application
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airframe structural components fsc application data
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ah-64 airframe, rotary wing aircraft end application
7-311511127-7
NSN 1680-01-224-2263
Cross Reference:
7-311511127-5
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ah-64 airframe, rotary wing aircraft end application
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ah-64 airframe, rotary wing aircraft end application
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ah-64 airframe, rotary wing aircraft end application
7-311660022-11
NSN 1680-01-232-7712
Cross Reference:
7-311660022, 7-311660022-5
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ah-64 airframe, rotary wing aircraft end application
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0.873 inches bore diameter
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between 0.800 inches and 0.810 inches bore length
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aluminum alloy material
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clevis ends style designator