Bell Cranks - Page 34 of 59
1465 part numbers
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between 0.749 inches and 0.750 inches counterbore diameter
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aluminum alloy material
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between 0.749 inches and 0.750 inches bore diameter
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aluminum alloy material
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0.812 inches counterbore diameter
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aluminum alloy material
160D521113-4
NSN 1680-01-025-5340
Cross Reference:
160D521113-2
160D622310-1
NSN 1680-01-026-4917
Cross Reference:
162D622310-1001
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control installation, fuselage, airframe fsc application data
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between 0.348 inches and 0.358 inches bore length
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aluminum alloy material
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e-3a aircraft end application
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stainless steel material
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0.812 inches counterbore diameter
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between 0.270 inches and 0.280 inches counterbore depth
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between 0.440 inches and 0.447 inches bore diameter
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between 1.901 inches and 1.916 inches bore length
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aluminum alloy material
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0.749 inches counterbore diameter
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1.380 inches bore length
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aluminum alloy material
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anodize surface treatment
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bearing and fulcrum bore features provided
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aluminum alloy material
65-38934-501
NSN 1680-01-033-8038
Cross Reference:
65-38934-1
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0.250 inches bore diameter
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aircraft e-3a end application
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aluminum alloy material
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rudder trim control fsc application data
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0.749 inches counterbore diameter
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0.750 inches bore length
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aluminum alloy material
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anodize surface treatment
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raised faced holes, clamp pivot hole, offset style designator
16T7309-803
NSN 1680-01-045-0500
Cross Reference:
16T7309-5, 16T7309-801
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f-16 aircraft end application
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bushing 2; unthreaded diameter hole: 0.375in special features
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f-16 aircraft end application
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drawing name - bellcrank assembly, drive canopy special features
16K2856-3
NSN 1680-01-052-0937
Cross Reference:
16K2856-1
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f-16 aircraft end application
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1.375 inches bore length
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steel material
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passivate surface treatment