Shaft Assembly Rigid Casings
16 part numbers
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used on f111 aircraft end application
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tf-41 aircraft engine end application
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steel material
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fsc application data: sheave assembly special features
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steel material
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0.750 inches outside diameter
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6.600 inches overall length
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f-15 eagle aircraft end application
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circumferentially grooved first end end connection type
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aluminum alloy material
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b-1b bomber end application
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used on rudder control servo cylinder input special features
27477-110
NSN 1680-01-432-5821
Cross Reference:
LE162-0043
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12.000 inches overall length
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b-1b aircraft end application
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control system-latching, stairladder special features
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stainless steel material
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zzzy criticality code justification
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1.620 inches outside diameter
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3.765 inches overall length
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c-5a aircraft end application
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aluminum material
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1.750 inches outside diameter
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1.750 inches overall length
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c-5 aircraft; u/o p/n 42093r10 end application
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stainless steel material
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100.250 inches overall length