Remote Control Levers - Page 27 of 32
798 part numbers
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aircraft c-17a end application
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lever, release special features
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c-130 aircraft end application
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aluminum alloy material
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qq-a-250/4 federal specification single material response material specification
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c-130 aircraft end application
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aircraft c-130 end application
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lever, manual control special features
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aircraft c-130 end application
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err default err default
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lever assembly landing gear control. special features
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joint stars target radar system end application
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b-2 special end application
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2.250 inches center to center distance between link and shaft holes
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0.458 inches distance between fork inside spread
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b-2 aircraft end application
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2.250 inches center to center distance between link and shaft holes
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0.458 inches distance between fork inside spread
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aircraft c-17a end application
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lever, remote control special features
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aircraft c-17a end application
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end fitting, assembly special features
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aircraft c-17a end application
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guide, lever, flap-sl special features
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pacer dawn end application
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1.000 inches center to center distance between link and shaft holes
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0.570 inches shaft end thickness
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0.500 inches link end thickness
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0.300 inches distance between fork inside spread
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0.900 inches overall width
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b-2 aircraft end application
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3.873 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.890 inches link end thickness
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0.900 inches overall width
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b-2 aircraft end application
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4.502 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.890 inches link end thickness
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0.900 inches overall width
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b-2 aircraft end application
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3.873 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.890 inches link end thickness
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1.000 inches overall width
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b-2 aircraft end application
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0.440 inches shaft end thickness
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0.890 inches link end thickness
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0.590 inches distance between fork inside spread
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1.000 inches overall width
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b-2 aircraft end application
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0.440 inches shaft end thickness
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0.890 inches link end thickness
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0.590 inches distance between fork inside spread
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0.900 inches overall width
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b-2 acft end application
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4.502 inches center to center distance between link and shaft holes
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0.860 inches shaft end thickness
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0.890 inches link end thickness
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pacer dawn end application
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1.000 inches center to center distance between link and shaft holes
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between 0.440 inches and 0.580 inches shaft end thickness
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0.500 inches link end thickness
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aluminum alloy material
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helicopter, uh-60a/uh-60d end application
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aluminum alloy material
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b-52 aircraft end application
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t.o. 16c1-10-2-4, fig 5, ind 21 special features
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1.312 inches overall width
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f-15 aircraft end application
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2.875 inches center to center distance between link and shaft holes
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c-17a aircraft end application
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0.790 inches overall width
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between 1.060 inches and 1.111 inches bore diameter
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between 0.310 inches and 0.320 inches bore length
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between 0.060 inches and 0.080 inches bore radius
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splined bore type