Bell Cranks - Page 39 of 59
1465 part numbers
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helicopter model h-46 end application
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4.000 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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clevis ends style designator
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steel material
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raised face pivot and end holes style designator
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0.637 inches bore diameter
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1.550 inches bore length
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aircraft model av-8 end application
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aluminum alloy material
7-311661003
NSN 1680-01-243-1084
Cross Reference:
7-311660003, 7-311661003-7
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ah-64 airframe, rotary wing aircraft end application
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aircraft model e-2c end application
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aluminum alloy material
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aircraft model c-2/e-2 end application
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aluminum material
7-311517070-13
NSN 1680-01-248-9971
Cross Reference:
7-311517070, 7-311517070-7
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apache airframe ah-64 end application
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aircraft accessory equipment fsc application data
7-311512085-9
NSN 1680-01-252-0380
Cross Reference:
7-311512085-7
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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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0.750 inches counterbore diameter
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0.229 inches counterbore depth
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0.625 inches bore diameter
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1.005 inches bore length
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2.400 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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1.000 inches bore diameter
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1.348 inches bore length
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titanium material
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0.750 inches counterbore diameter
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0.300 inches counterbore depth
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0.625 inches bore diameter
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0.281 inches bore length
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3.304 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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between 0.749 inches and 0.750 inches counterbore diameter
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between 0.229 inches and 0.300 inches counterbore depth
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0.625 inches bore diameter
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2.146 inches bore length
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2.404 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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1.000 inches bore diameter
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1.510 inches bore length
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2.400 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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1.188 inches counterbore diameter
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0.260 inches counterbore depth
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1.062 inches bore diameter
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1.785 inches bore length
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2.625 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.999 inches bore diameter
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2.290 inches bore length
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aluminum alloy material
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anodize surface treatment
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uh-60 rotary wing aircraft end application
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uh-60 rotary wing aircraft end application
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0.193 inches bore diameter
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0.120 inches bore length
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mc-130h acft end application
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1.670 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.776 inches 1st end end hole/ball diameter
16S1531-15
NSN 1680-01-306-8327
Cross Reference:
16S1531-11, 16S1531-9
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0.6275 inches bore diameter
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2.950 inches bore length
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aim 7/aim 120 launcher end application
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0.3125 inches 2nd end end hole/ball diameter
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aluminum material