Bell Cranks - Page 32 of 59

1465 part numbers
128CM11015-601 NSN 1680-00-970-9728 Cross Reference: 128CM11015-1
128CM12050-1 NSN 1680-00-971-2991
  • steel material
128CM11005-1 NSN 1680-00-971-3239
  • between 0.748 inches and 0.749 inches bore diameter
  • 0.937 inches bore length
  • aluminum alloy material
128C11209-1 NSN 1680-00-971-3241
128CM13006-5 NSN 1680-00-971-3403
  • aluminum alloy material
128CM13002-1 NSN 1680-00-971-3477
  • 0.855 inches bore diameter
  • between 2.000 inches and 2.010 inches bore length
  • aluminum alloy material
128CM12009-1 NSN 1680-00-971-3490 Cross Reference: 128CN12009-1
  • between 2.103 inches and 2.113 inches bore length
  • aluminum alloy material
830755-5 NSN 1680-00-981-7428
32-35248-303 NSN 1680-00-988-9112
204-001-832-1 NSN 1680-00-991-0318 Cross Reference: 204-001-832-001
  • 0.066 inches bore diameter
  • 0.750 inches bore length
  • 4.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
  • 1.029 inches 2nd end end hole/ball diameter
  • aluminum alloy material
3G11520-128 NSN 1680-00-997-4850
  • c-141 aircraft end application
3G11520-127 NSN 1680-00-997-4851
  • c-141 aircraft end application
3822729-1 NSN 1680-01-003-1026
  • between 1.249 inches and 1.250 inches bore diameter
  • between 0.740 inches and 0.750 inches bore length
  • abxv criticality code justification
  • steel material
  • cadmium surface treatment
1292194-101 NSN 1680-01-003-7313 Cross Reference: 1294-101
  • 1.249 inches bore diameter
  • between 2.337 inches and 2.339 inches bore length
  • stainless steel material
1292108-101 NSN 1680-01-003-8038
  • between 1.191 inches and 1.192 inches bore diameter
  • between 0.980 inches and 0.985 inches bore length
  • aluminum alloy material
  • anodize surface treatment
160D965514-1 NSN 1680-01-004-0713
  • between 0.748 inches and 0.749 inches bore diameter
  • 0.750 inches bore length
  • aluminum alloy material
  • clevis ends style designator
  • controls, fuselage, airframe fsc application data
160D965515-1 NSN 1680-01-004-0714
  • between 0.748 inches and 0.749 inches bore diameter
  • 0.750 inches bore length
  • aluminum alloy material
  • clevis ends style designator
  • controls, fuselage, airframe fsc application data
160D121230-1 NSN 1680-01-004-0715
  • aluminum alloy material
  • roll control, fuselage aircraft fsc application data
160D121250-1 NSN 1680-01-004-1591 Cross Reference: 160D121250-3
  • 0.875 inches bore diameter
  • 2.218 inches bore length
  • aluminum alloy material
  • control installation, fuselage, airframe fsc application data
1292894-109 NSN 1680-01-004-1837
  • steel material
  • nickel surface treatment
160D521210-1 NSN 1680-01-005-3863 Cross Reference: 160D501210-3, 160D521210-3
  • trim tab controls, fuselage, airframe fsc application data
160D117237-1 NSN 1680-01-005-7551
  • aluminum alloy material
  • controls, fuselage, airframe fsc application data
160D950131-3 NSN 1680-01-006-9563 Cross Reference: 160D950131-1
  • 0.750 inches bore diameter
  • 0.750 inches bore length
  • 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
  • 1.249 inches bore diameter
  • between 2.337 inches and 2.339 inches bore length
  • stainless steel material