Bell Cranks - Page 32 of 59
1465 part numbers
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between 0.748 inches and 0.749 inches bore diameter
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0.937 inches bore length
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aluminum alloy material
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0.855 inches bore diameter
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between 2.000 inches and 2.010 inches bore length
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aluminum alloy material
128CM12009-1
NSN 1680-00-971-3490
Cross Reference:
128CN12009-1
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between 2.103 inches and 2.113 inches bore length
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aluminum alloy material
204-001-832-1
NSN 1680-00-991-0318
Cross Reference:
204-001-832-001
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0.066 inches bore diameter
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0.750 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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1.029 inches 2nd end end hole/ball diameter
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aluminum alloy material
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c-141 aircraft end application
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c-141 aircraft end application
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between 1.249 inches and 1.250 inches bore diameter
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between 0.740 inches and 0.750 inches bore length
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abxv criticality code justification
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steel material
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cadmium surface treatment
1292194-101
NSN 1680-01-003-7313
Cross Reference:
1294-101
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1.249 inches bore diameter
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between 2.337 inches and 2.339 inches bore length
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stainless steel material
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between 1.191 inches and 1.192 inches bore diameter
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between 0.980 inches and 0.985 inches bore length
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aluminum alloy material
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anodize surface treatment
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between 0.748 inches and 0.749 inches bore diameter
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0.750 inches bore length
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aluminum alloy material
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clevis ends style designator
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controls, fuselage, airframe fsc application data
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between 0.748 inches and 0.749 inches bore diameter
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0.750 inches bore length
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aluminum alloy material
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clevis ends style designator
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controls, fuselage, airframe fsc application data
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aluminum alloy material
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roll control, fuselage aircraft fsc application data
160D121250-1
NSN 1680-01-004-1591
Cross Reference:
160D121250-3
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0.875 inches bore diameter
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2.218 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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steel material
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nickel surface treatment
160D521210-1
NSN 1680-01-005-3863
Cross Reference:
160D501210-3, 160D521210-3
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trim tab controls, fuselage, airframe fsc application data
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aluminum alloy material
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controls, fuselage, airframe fsc application data
160D950131-3
NSN 1680-01-006-9563
Cross Reference:
160D950131-1
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0.750 inches bore diameter
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0.750 inches bore length
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aluminum alloy material
50-430042-13
NSN 1680-01-007-1243
Cross Reference:
50-430042-7
1292194-102
NSN 1680-01-009-4264
Cross Reference:
1292829-102
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1.249 inches bore diameter
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between 2.337 inches and 2.339 inches bore length
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stainless steel material