Dirt And Liquid Deflectors
25 part numbers
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between 0.010 inches and 0.020 inches chamfer length
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between 0.298 inches and 0.302 inches width
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between 2.490 inches and 2.510 inches outside diameter
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steel, federal standard 66, aisi 410/sae 51410 material
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steel comp 410 material
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aircraft eng end application
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agav criticality code justification
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aircraft eng end application
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agav criticality code justification
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aircraft eng end application
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agav criticality code justification
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2.561 inches inside diameter
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0.047 inches material thickness
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0.724 inches body length
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aircraft eng end application
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agav criticality code justification
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between 1.379 inches and 1.381 inches inside diameter
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between 2.040 inches and 2.100 inches outside diameter
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0.020 inches material thickness
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between 0.080 inches and 0.100 inches body length
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steel, mil-s-5059 material
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u/o f101-102 eng; e/i b1-b acft end application
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steel material
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steel material
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1.530 inches tapered hole minor diameter
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2.495 inches outside diameter
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0.032 inches material thickness
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2.870 inches body length
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1.980 inches tapered hole major diameter
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u/o f101-102 eng; e/i b1-b acft end application
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steel material
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steel material
114D6256-3
NSN 2995-01-247-8477
Cross Reference:
114D6256-1, 74A802615-1019
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f110-ge-400 engine end application
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aluminum material
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cognizant user service italian navy supplementary features
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preprovisioning support navicp is poe end application
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ct7-9 turboprop engine end application
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part name assigned by manufacturer baffel special features
