Bell Cranks - Page 33 of 59
1465 part numbers
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steel material
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anodize surface treatment
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aluminum alloy material
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control, fuselage, airframe fsc application data
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aluminum alloy material
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control, rudder, fuselage fsc application data
160D120310-7
NSN 1680-01-010-2818
Cross Reference:
160D120310-5
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aluminum alloy material
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cable, control, fuselage aircraft fsc application data
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aluminum alloy material
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control, pitch, fuselage aircraft fsc application data
160D722110-1
NSN 1680-01-010-2820
Cross Reference:
162D722110-1001
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aluminum alloy material
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trim tab, fuselage aircraft fsc application data
160D622130-1
NSN 1680-01-010-2823
Cross Reference:
162D622130-1001
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aluminum alloy material
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control, fuselage aircraft fsc application data
160D622325-5
NSN 1680-01-010-2824
Cross Reference:
160D622325-1, 160D622325-3, 162D622325-1001
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steel material
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control, fuselage aircraft fsc application data
160D121225-3
NSN 1680-01-010-2825
Cross Reference:
160D121225-1
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between 0.873 inches and 0.874 inches bore diameter
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between 0.813 inches and 0.823 inches bore length
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aluminum alloy material
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clevis ends style designator
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control installation, fuselage, airframe fsc application data
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wing aircraft fsc application data
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between 0.875 inches and 0.876 inches bore diameter
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between 0.965 inches and 0.970 inches bore length
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aircraft model a10 end application
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aluminum alloy material
160D123205-5
NSN 1680-01-012-7145
Cross Reference:
160D123205-7
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between 0.750 inches and 0.751 inches bore diameter
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1.360 inches bore length
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aircraft model a10 end application
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aluminum alloy material
160D627110-1
NSN 1680-01-013-1842
Cross Reference:
160D627110-3, 162D627110-1001
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aluminum alloy material
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pitch control, fuselage aircraft fsc application data
160D622310-2
NSN 1680-01-015-0847
Cross Reference:
162D622310-1002
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0.875 inches bore diameter
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between 2.000 inches and 2.010 inches bore length
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6.212 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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raised face pivot hole, clevis both ends style designator
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control installation, fuselage, airframe fsc application data
160D523120-1
NSN 1680-01-015-0848
Cross Reference:
160D523120-3
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aluminum alloy material
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control installation, fuselage, airframe fsc application data
160D521113-1
NSN 1680-01-015-0849
Cross Reference:
160D521113-3
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aluminum alloy material
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control installation, fuselage, airframe fsc application data
160D725150-1
NSN 1680-01-015-7316
Cross Reference:
160D725150-3, 162D725150-1001
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0.624 inches bore diameter
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0.500 inches bore length
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aluminum alloy material
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control installation, fuselage, airframe fsc application data
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1.062 inches bore diameter
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aluminum alloy material
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between 0.748 inches and 0.749 inches counterbore diameter
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between 0.234 inches and 0.238 inches counterbore depth
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0.625 inches bore diameter
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between 2.938 inches and 2.943 inches bore length
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aluminum alloy material
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between 0.874 inches and 0.875 inches counterbore diameter
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between 0.308 inches and 0.313 inches counterbore depth
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aluminum alloy material
K651083-3
NSN 1680-01-021-8258
Cross Reference:
K651083-1
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between 0.748 inches and 0.749 inches counterbore diameter
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between 0.234 inches and 0.239 inches counterbore depth
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between 0.749 inches and 0.750 inches bore diameter
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between 1.250 inches and 1.255 inches bore length
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aluminum alloy material