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National Stock Number:
1680-00-915-6914
Federal Supply Class:
1680
National Item Identification Number:
009156914
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:
| 65404-03414-041 | 78286 | SIKORSKY AIRCRAFT CORPORATION | | 65404-03417-041 | 78286 | SIKORSKY AIRCRAFT CORPORATION | | 65404-03417-041 | D1081 | AIRBUS DEUTSCHLAND GMBH -WERK BREMEN- |
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Techincal Specification:
| BORE DIAMETER | 1.814 INCHES MINIMUM AND 1.815 INCHES MAXIMUM | | BORE LENGTH | 1.495 INCHES MINIMUM AND 1.500 INCHES MAXIMUM | | BORE TYPE | PLAIN STRAIGHT | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.255 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 1.050 INCHES MINIMUM AND 1.060 INCHES MAXIMUM | | LINK END HOLE DIAMETER | 0.312 INCHES MINIMUM AND 0.313 INCHES MAXIMUM | | LINK END THICKNESS | 1.380 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-A-22771, COMP 7075-T73 MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 1.495 INCHES MINIMUM AND 1.500 INCHES MAXIMUM | | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
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