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National Stock Number:
1680-00-915-6847
Federal Supply Class:
1680
National Item Identification Number:
009156847
Description:
LEVER,REMOTE CONTROL
Detail:
A rigid item usually in the form of an arm of various shapes and cross sections, containing two or more holes so spaced that one serves as a pivot with or without hubs and must have a definite means for securing to a shaft (such as threaded hole for set-screw, keyway(s), splines, serrations or some clamping device). The other hole(s) connect(s) to CONNECTING LINK, RIGID; WIRE ROPE ASSEMBLY, SINGLE LEG; or CLEVIS, ROD END; to provide transmission of movement to other parts of the mechanism. See also BELL CRANK. For manually operated items see LEVER, MANUAL CONTROL.
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Manufacturer Information:
| 65403-07619-041 | 59213 | AERO COMPONENTS, LLC | | 65403-07619-041 | 78286 | SIKORSKY AIRCRAFT CORPORATION | | 65403-07619-041 | D1081 | AIRBUS DEUTSCHLAND GMBH -WERK BREMEN- |
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Techincal Specification:
| BORE DIAMETER | 1.001 INCHES MINIMUM AND 1.005 INCHES MAXIMUM | | BORE LENGTH | 1.000 INCHES NOMINAL | | BORE TYPE | PLAIN STRAIGHT | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 3.000 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.593 INCHES MINIMUM AND 0.594 INCHES MAXIMUM | | LINK END HOLE DIAMETER | 0.250 INCHES NOMINAL | | LINK END THICKNESS | 1.025 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-601, ALLOY 356, T6 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 1.000 INCHES NOMINAL | | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END | | SURFACE TREATMENT | ANODIZE |
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