Nonrotating Shaft Eye Brackets - Page 6 of 12
291 part numbers
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training aircraft end application
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f/a-22 raptor end application
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1.750 inches width
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4.500 inches overall length
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0.550 inches overall height
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f18 e/f end application
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agav criticality code justification
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1.750 inches width
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4.500 inches overall length
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0.550 inches overall height
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f-18 e/f end application
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agav criticality code justification
4-16306-0250
NSN 1680-01-523-0879
Cross Reference:
0333712 REV B ITEM 29, BK-250-S
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mids cass end application
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chassis part no. 11477046 for patriot end application
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aluminum alloy material
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u-2aircraft end application
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e-3a joint stars end application
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f-22a emd end application
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1680 misc aircraft equipment fsc application data
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f-22a emd end application
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bracket, eye, nonrotating shaft end application
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2.191 inches width
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4.335 inches overall length
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f-22a emd end application
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feat criticality code justification
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titanium material
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6.791 inches overall length
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5.184 inches overall height
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f-22 raptor end application
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aluminum material
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6.791 inches overall length
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5.184 inches overall height
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f-22 raptor end application
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called out as connector, rod end special features
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aluminum material
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endi-te-mns-n494 end application
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f-16 end application
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fitting, fwd fairing attach, cft special features
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f-22 raptor end application