Rotating Shaft Eye Brackets
129 part numbers
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between 1.000 inches and 1.001 inches bore inside diameter
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aluminum alloy material
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3.810 inches width
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4.000 inches overall length
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0.890 inches overall height
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1.250 inches bore inside diameter
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aluminum alloy material
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3.810 inches width
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4.000 inches overall length
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0.890 inches overall height
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1.250 inches bore inside diameter
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aluminum alloy material
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0.531 inches width
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4.540 inches overall length
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0.375 inches bore inside diameter
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aluminum alloy material
339112-7
NSN 1680-00-098-7928
Cross Reference:
339112-3L
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8.090 inches overall length
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4.200 inches overall height
339112-8
NSN 1680-00-098-7929
Cross Reference:
339112-3R
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8.090 inches overall length
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4.200 inches overall height
339112-9
NSN 1680-00-098-7930
Cross Reference:
339112-4
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8.090 inches overall length
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4.200 inches overall height
1211166-101
NSN 1680-00-215-0125
Cross Reference:
1204498-102, 1204499-101
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1.020 inches width
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2.400 inches overall length
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0.820 inches overall height
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between 0.312 inches and 0.313 inches bore inside diameter
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aluminum alloy material
1211166-102
NSN 1680-00-215-0126
Cross Reference:
1204498-101, 1204499-102
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1.020 inches width
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2.400 inches overall length
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0.820 inches overall height
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between 3.312 inches and 3.313 inches bore inside diameter
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aluminum alloy material
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0.625 inches bore inside diameter
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aluminum alloy material
205-031-151-1
NSN 1680-00-415-6394
Cross Reference:
205-031-151-001
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2.120 inches width
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0.252 inches overall length
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3.000 inches overall height
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uh-1 series helicopters end application
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between 0.749 inches and 0.750 inches bore inside diameter
204-070-993-3
NSN 1680-00-435-4825
Cross Reference:
204-070-993-001, 204-070-993-003, 204-070-993-1
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0.890 inches width
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1.920 inches overall length
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1.098 inches overall height
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fuselage section, acft end application
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between 0.374 inches and 0.375 inches bore inside diameter
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2.000 inches width
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2.300 inches overall length
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1.550 inches overall height
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1. fuselage section, acft end application
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0.906 inches bore inside diameter
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0.600 inches width
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1.100 inches overall length
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1.250 inches overall height
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1. fuselage scetion, acft end application
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0.390 inches bore inside diameter
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0.625 inches width
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3.750 inches overall length
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0.875 inches overall height
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0.377 inches bore inside diameter
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used on rod end on forward support body cowl special features
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kc-135aaircraft end application
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oh-58d turbine engine end application
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feat criticality code justification
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flight safety critical aircraft part special features
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3.590 inches overall length
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aluminum alloy material
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qq-a-225/9 federal specification single material response material specification
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4.090 inches overall length
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aluminum alloy material
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qq-a-225/9 federal specification single material response material specification
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1.880 inches width
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4.090 inches overall length
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aluminum alloy material
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qq-a-225/9 federal specification single material response material specification
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4.090 inches overall length
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aluminum alloy material
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qq-a-225/9 federal specification single material response material specification
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c-17a acft end application
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bronze, o/a, 3/4 in. dia, 1 1/2 in. lg. special features
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aluminum alloy material