Bell Cranks - Page 31 of 59
1465 part numbers
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0.250 inches bore diameter
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0.875 inches bore length
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four bushings required for arm holes special features
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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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0.749 inches bore diameter
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between 0.776 inches and 0.781 inches bore length
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3.666 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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0.749 inches bore diameter
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0.778 inches bore length
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surface treatment: chemical film special features
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aluminum alloy material
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surface treatment: chemical film special features
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aluminum alloy material
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0.749 inches bore diameter
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1.088 inches bore length
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3.466 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
65402-03113-041
NSN 1680-00-941-3305
Cross Reference:
65402-03112-041, V6540-03113-041
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aluminum alloy material
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anodize surface treatment
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0.438 inches bore diameter
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3.322 inches bore length
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f-4 aircraft end application
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bellcrank has three arms, two slotted special features
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aluminum alloy material
369N2664
NSN 1680-00-943-0824
Cross Reference:
369A7602
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between 3.417 inches and 3.427 inches bore length
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3.990 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
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magnesium alloy material
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anodize surface treatment
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0.901 inches counterbore diameter
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between 0.340 inches and 0.438 inches counterbore depth
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0.593 inches 1st end slot width
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0.781 inches bore diameter
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2.625 inches bore length
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0.625 inches bore diameter
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5.500 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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0.250 inches 2nd end end hole/ball diameter
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aluminum alloy material
205-001-906-1
NSN 1680-00-966-6103
Cross Reference:
205-001-906-001
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between 0.740 inches and 0.750 inches bore length
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3.850 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
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aluminum alloy material
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fuselage sect., acft fsc application data
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0.813 inches bore diameter
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0.260 inches bore length
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aluminum alloy material