Remote Control Levers - Page 21 of 32
798 part numbers
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0.193 inches bore diameter
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0.188 inches bore length
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1620-00-367-9449; gearbox, landing gear end application
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plain straight bore type
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6.125 inches center to center distance between link and shaft holes
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ch-47, rotary wing aircraft end application
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seat, aircraft ejection end application
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split end screw clamping feature features provided
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stainless steel material
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seat, aircraft ejection end application
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0.750 inches center to center distance between link and shaft holes
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0.560 inches shaft end thickness
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0.300 inches link end thickness
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0.157 inches link end hole diameter
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seat, aircraft ejection end application
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plain straight bore type
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0.750 inches center to center distance between link and shaft holes
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0.562 inches shaft end thickness
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0.300 inches link end thickness
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0.620 inches overall width
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seat, aircraft ejection end application
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0.850 inches center to center distance between link and shaft holes
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0.370 inches shaft end thickness
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0.120 inches link end thickness
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seat, aircraft ejection end application
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plain straight bore type
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0.750 inches center to center distance between link and shaft holes
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0.562 inches shaft end thickness
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0.300 inches link end thickness
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2.265 inches bore length
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plain straight bore type
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aluminum alloy material
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0.500 inches overall width
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0.246 inches bore diameter
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0.250 inches bore length
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plain straight bore type
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3.620 inches center to center distance between link and shaft holes
65-38989-4
NSN 1680-01-138-5882
Cross Reference:
65-38989-501
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1.400 inches bore length
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0.406 inches bore radius
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d-shaped bore type
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counterbore features provided
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both ends forked, has bearing special features
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aircraft model h-53 end application
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between 1.814 inches and 1.815 inches bore diameter
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1.000 inches bore length
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plain straight bore type
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4.000 inches center to center distance between link and shaft holes
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between 0.990 inches and 1.010 inches shaft end thickness
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aircraft f-18 end application
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between 1.814 inches and 1.815 inches bore diameter
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1.370 inches bore length
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plain straight bore type
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7.154 inches center to center distance between link and shaft holes
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1.370 inches shaft end thickness
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between 1.814 inches and 1.815 inches bore diameter
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0.990 inches bore length
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plain straight bore type
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4.000 inches center to center distance between link and shaft holes
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0.990 inches shaft end thickness
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0.500 inches bore diameter
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0.725 inches bore length
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seat, aircraft ejection end application
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plain straight bore type
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1.540 inches center to center distance between link and shaft holes
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ch-47, rotary wing aircraft end application
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1.125 inches overall width
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f-15 acft; aircraft structural component end application
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5.000 inches center to center distance between link and shaft holes
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1.250 inches shaft end thickness
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0.521 inches link end thickness
1168965-103
NSN 1680-01-157-1410
Cross Reference:
AT-101-1350
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0.560 inches overall width
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f-5 acft; aircraft structural component end application
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3.500 inches center to center distance between link and shaft holes
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0.190 inches shaft end thickness
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0.190 inches link end thickness