Bell Cranks - Page 28 of 59
1465 part numbers
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0.245 inches counterbore depth
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1.350 inches bore diameter
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4.690 inches bore length
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magnesium material
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fuselage sect., acft fsc application data
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0.245 inches counterbore depth
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1.350 inches bore diameter
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4.690 inches bore length
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fuselage sect., acft fsc application data
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1.580 inches bore diameter
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2.750 inches bore length
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7.500 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
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fuselage sect., acft fsc application data
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1.749 inches counterbore diameter
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0.235 inches counterbore depth
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1.580 inches bore diameter
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1.960 inches bore length
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4.350 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
4C90000-105A
NSN 1680-00-833-3947
Cross Reference:
0501146-5
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between 1.062 inches and 1.063 inches bore diameter
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9.042 inches bore length
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between 1.812 inches and 1.814 inches bore diameter
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between 3.650 inches and 3.670 inches bore length
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magnesium material
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chromate surface treatment
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fuselage sect., airframe fsc application data
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between 0.578 inches and 0.586 inches bore diameter
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1.190 inches bore length
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aluminum alloy material
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f-111 aircraft end application
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mil-a-22771, alloy 7075, t73 special features
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aluminum alloy material
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between 0.748 inches and 0.753 inches bore diameter
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0.690 inches bore length
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between 0.748 inches and 0.753 inches bore diameter
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0.690 inches bore length
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between 0.748 inches and 0.749 inches bore diameter
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2.218 inches bore length
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3.530 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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magnesium material
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raised face pivot hole, clevis both ends style designator
215-78104-12
NSN 1680-00-853-1984
Cross Reference:
215-78104-8
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between 0.875 inches and 0.880 inches bore diameter
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between 1.650 inches and 1.700 inches bore length
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between 0.875 inches and 0.880 inches bore diameter
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between 1.650 inches and 1.700 inches bore length
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1.562 inches bore diameter
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2.880 inches bore length
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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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0.625 inches 2nd end end hole/ball diameter
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steel material
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0.873 inches bore diameter
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between 2.069 inches and 2.070 inches bore length
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3.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.375 inches 2nd end end hole/ball diameter
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aluminum alloy material
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f-111 aircraft end application
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aluminum alloy material
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anodize surface treatment
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aluminum alloy material
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anodize surface treatment
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aluminum alloy material
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anodize surface treatment
4C90000-103A
NSN 1680-00-860-3650
Cross Reference:
0501146-3
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between 1.062 inches and 1.063 inches bore diameter
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9.042 inches bore length