Bell Cranks - Page 15 of 59
1465 part numbers
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0.375 inches bore diameter
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between 0.545 inches and 0.550 inches bore length
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aluminum alloy material
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anodize surface treatment
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hood, forward fsc application data
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0.750 inches bore diameter
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0.500 inches bore length
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aluminum alloy material
7839338-01
NSN 1680-00-510-4085
Cross Reference:
4041655, 7839338-101
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1.750 inches bore diameter
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1.400 inches bore length
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2.950 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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0.250 inches 1st end end hole/ball diameter
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aluminum alloy material
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feat criticality code justification
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flight safety critical special features
4014204
NSN 1680-00-520-6055
Cross Reference:
4014204-3
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between 0.745 inches and 0.751 inches bore diameter
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0.625 inches bore length
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steel material
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aluminum alloy material
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anodize surface treatment
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0.625 inches bore diameter
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between 1.879 inches and 1.889 inches bore length
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aluminum alloy material
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hu-16 aircraft end application
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0.843 inches bore length
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6.093 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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fuselage sect., acft fsc application data
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between 0.249 inches and 0.251 inches bore diameter
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between 0.620 inches and 0.630 inches bore length
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aluminum material
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zinc surface treatment
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fuselage sect., acft fsc application data
40092-9
NSN 1680-00-532-9368
Cross Reference:
40092-09
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between 0.249 inches and 0.251 inches bore diameter
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between 0.620 inches and 0.630 inches bore length
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aluminum material
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zinc surface treatment
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fuselage sect., acft fsc application data
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between 1.249 inches and 1.250 inches bore diameter
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1.688 inches bore length
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aluminum alloy material
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between 1.249 inches and 1.250 inches bore diameter
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1.688 inches bore length
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aluminum alloy material
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1.9920 inches bore diameter
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aluminum material
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zinc surface treatment
53-650033-6
NSN 1680-00-539-0042
Cross Reference:
53-65033-6
