Remote Control Levers - Page 2 of 32
798 part numbers
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between 0.249 inches and 0.255 inches bore diameter
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plain straight bore type
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used on ejection seat special features
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aluminum alloy material
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anodize surface treatment
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alum alloy; aircraft t-33 special features
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c2/ec aircraft end application
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serrated bore type
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2.125 inches center to center distance between link and shaft holes
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0.562 inches shaft end thickness
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0.850 inches link end thickness
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e-2 aircraft end application
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steel material
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c-2 and e-2 aircraft end application
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0.375 inches shaft end thickness
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0.375 inches link end thickness
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steel material
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aisi4340 assn standard single material response material specification
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between 0.755 inches and 0.759 inches bore diameter
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1.000 inches bore length
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plain straight bore type
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1.750 inches center to center distance between link and shaft holes
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1.000 inches shaft end thickness
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0.560 inches overall width
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splined bore type
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0.833 inches center to center distance between link and shaft holes
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0.400 inches shaft end thickness
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stainless steel material
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between 1.015 inches and 1.028 inches bore diameter
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0.750 inches bore length
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plain straight bore type
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1.250 inches center to center distance between link and shaft holes
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0.750 inches shaft end thickness
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between 0.374 inches and 0.376 inches bore diameter
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between 0.770 inches and 0.810 inches bore length
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plain straight bore type
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1.000 inches center to center distance between link and shaft holes
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between 0.770 inches and 0.810 inches shaft end thickness
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1.600 inches bore diameter
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0.690 inches bore length
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t-6 aircraft end application
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plain straight bore type
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between 0.720 inches and 0.800 inches shaft end thickness
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0.625 inches overall width
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0.500 inches bore length
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1.656 inches center to center distance between link and shaft holes
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0.500 inches shaft end thickness
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0.250 inches link end thickness
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serrated bore type
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3.250 inches center to center distance between link and shaft holes
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0.690 inches shaft end thickness
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between 0.770 inches and 0.810 inches link end thickness
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between 0.190 inches and 1.194 inches link end hole diameter
6-13531-3
NSN 1680-00-072-7375
Cross Reference:
6-13531-1
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serrated bore type
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2.710 inches center to center distance between link and shaft holes
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0.640 inches shaft end thickness
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0.880 inches link end thickness
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between 0.250 inches and 0.254 inches link end hole diameter
4-13539-1
NSN 1680-00-072-7377
Cross Reference:
4-13539-4
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serrated bore type
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aluminum alloy material
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serrated bore type
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2.090 inches center to center distance between link and shaft holes
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0.640 inches shaft end thickness
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0.950 inches link end thickness
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between 0.250 inches and 0.254 inches link end hole diameter
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serrated bore type
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2.950 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.750 inches link end thickness
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0.190 inches link end hole diameter
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serrated bore type
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2.950 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.750 inches link end thickness
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0.190 inches link end hole diameter
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between 0.501 inches and 0.502 inches bore diameter
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0.500 inches bore length
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1.500 inches center to center distance between link and shaft holes
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0.500 inches shaft end thickness
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0.410 inches link end thickness
3-13478-5
NSN 1680-00-072-8876
Cross Reference:
3-13478-9
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serrated bore type
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3.250 inches center to center distance between link and shaft holes
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0.500 inches shaft end thickness
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0.720 inches link end thickness
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0.190 inches link end hole diameter
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1.000 inches overall width
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between 0.755 inches and 0.759 inches bore diameter
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0.500 inches bore length
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plain straight bore type
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3.430 inches center to center distance between link and shaft holes
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ch-46 helicopter end application
107C2311-8
NSN 1680-00-074-2169
Cross Reference:
107C2311-3
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0.760 inches overall width
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serrated bore type
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1.500 inches center to center distance between link and shaft holes
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0.400 inches shaft end thickness
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0.190 inches link end thickness