Bell Cranks - Page 14 of 59
1465 part numbers
S6140-62144-005
NSN 1680-00-458-7766
Cross Reference:
S6140-62144, S6140-62144-5
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aluminum alloy material
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anodize surface treatment
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4.500 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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aluminum alloy material
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raised faced holes, offset both arms style designator
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0.7515 inches bore diameter
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2.390 inches bore length
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steel material
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4.312 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.250 inches 2nd end end hole/ball diameter
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aluminum alloy material
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4.312 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.250 inches 2nd end end hole/ball diameter
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aluminum alloy material
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0.930 inches bore diameter
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8.150 inches bore length
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steel material
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1.120 inches bore diameter
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3.620 inches bore length
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aluminum alloy material
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anodize surface treatment
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between 0.814 inches and 0.815 inches counterbore diameter
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between 0.239 inches and 0.244 inches counterbore depth
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between 0.687 inches and 0.692 inches bore diameter
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between 1.595 inches and 1.605 inches bore length
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titanium alloy material
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between 0.437 inches and 0.439 inches bore diameter
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steel material
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cadmium surface treatment
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between 0.437 inches and 0.439 inches bore diameter
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steel material
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cadmium surface treatment
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between 1.436 inches and 1.437 inches bore diameter
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between 1.941 inches and 1.946 inches bore length
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aluminum alloy material
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anodize surface treatment
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cyclic pitch control, rotor, helicopter fsc application data
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f-14a/b/d acft end application
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aluminum alloy material
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0.749 inches bore diameter
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0.750 inches bore length
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aluminum alloy material
134CM10035-9
NSN 1680-00-490-1114
Cross Reference:
134CM10035-5
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0.312 inches bore diameter
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between 1.750 inches and 1.760 inches bore length
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2.906 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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control column, aircraft fsc application data
4F61077-105A
NSN 1680-00-494-7739
Cross Reference:
4F61077-101A
4C51790-105A
NSN 1680-00-498-3174
Cross Reference:
4C51790-101A
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between 0.750 inches and 0.751 inches bore diameter
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0.875 inches bore length
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titanium material
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fuselage, airframe fsc application data