Remote Control Levers
798 part numbers
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between 1.312 inches and 1.313 inches bore diameter
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between 1.750 inches and 1.755 inches bore length
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plain straight bore type
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flight control, aircraft special features
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aluminum alloy material
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between 1.937 inches and 1.947 inches bore length
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plain straight bore type
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abxv criticality code justification
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flight control, aircraft special features
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aluminum alloy material
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control, ejection seat special features
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aluminum alloy material
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anodize surface treatment
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titanium material
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paint surface treatment
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splined bore type
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keyway features provided
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feat criticality code justification
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minor diameter 0.2813 in., majordia 0.2893 in. special features
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passivate surface treatment
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between 0.256 inches and 0.263 inches bore diameter
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0.460 inches bore length
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plain straight bore type
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aluminum alloy material
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anodize surface treatment
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aluminum alloy material
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zinc surface treatment
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splined bore type
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2.250 inches center to center distance between link and shaft holes
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0.875 inches shaft end thickness
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0.767 inches link end thickness
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0.313 inches link end hole diameter
32-90520-3
NSN 1680-00-015-1453
Cross Reference:
32-90520-5
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between 1.000 inches and 1.010 inches bore diameter
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1.640 inches bore length
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plain straight bore type
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6.667 inches center to center distance between link and shaft holes
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1.640 inches shaft end thickness
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0.508 inches major diameter
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0.880 inches overall width
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36 serration quantity
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c-123 aircraft end application
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0.462 inches minor diameter
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inertia reels, personnel restraint systems end application
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color is gray special features
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aluminum alloy material
4415
NSN 1680-00-024-6336
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1.500 inches major diameter
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1.860 inches overall width
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47 spline quantity
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1.443 inches minor diameter
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splined bore type
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1.250 inches overall width
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0.750 inches bore diameter
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0.625 inches bore length
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plain straight bore type
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2.560 inches center to center distance between link and shaft holes
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between 1.217 inches and 1.219 inches bore diameter
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between 0.990 inches and 1.010 inches bore length
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plain straight bore type
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between 5.052 inches and 5.072 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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c-123 aircraft end application
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between 6.245 inches and 6.255 inches center to center distance between link and shaft holes
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between 0.745 inches and 0.755 inches shaft end thickness
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1.160 inches link end thickness
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0.500 inches link end hole diameter
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c-123 aircraft end application
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between 6.432 inches and 6.442 inches center to center distance between link and shaft holes
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between 0.745 inches and 0.755 inches shaft end thickness
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1.156 inches link end thickness
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0.500 inches link end hole diameter
2-13483-23
NSN 1680-00-033-8615
Cross Reference:
2-13483-15
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serrated bore type
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2.900 inches center to center distance between link and shaft holes
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0.630 inches shaft end thickness
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0.800 inches link end thickness
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0.250 inches link end hole diameter
165-58794-3
NSN 1680-00-035-3383
Cross Reference:
165-58782-7
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0.438 inches overall width
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0.242 inches bore diameter
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0.375 inches bore length
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plain straight bore type
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0.875 inches center to center distance between link and shaft holes
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a-4 aircraft end application
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serrated bore type
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aluminum alloy material
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anodize surface treatment
89LM1883-1
NSN 1680-00-047-1886
Cross Reference:
89L1883-1
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1.437 inches overall width
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plain straight bore type
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3.500 inches center to center distance between link and shaft holes
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1.000 inches shaft end thickness
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0.493 inches link end thickness
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between 0.999 inches and 1.001 inches bore diameter
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between 0.586 inches and 0.588 inches bore length
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t-33 aircraft end application
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plain straight bore type
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3.700 inches center to center distance between link and shaft holes
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splined bore type
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offset, clevis link end style designator