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National Stock Number:
1680-00-511-5061
Federal Supply Class:
1680
National Item Identification Number:
005115061
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:
| 4041615 | 1NNE7 | ASES, LLC DBA FIELD AEROSPACE | | 4041615 | 6KCS9 | ASES LLC | | 4041615 | 71379 | CESSNA AIRCRAFT COMPANY | | 4041615 | 7EK50 | TEXTRON AVIATION INC |
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Techincal Specification:
| BORE TYPE | SPLINED | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.500 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.437 INCHES MINIMUM AND 0.447 INCHES MAXIMUM | | FEATURES PROVIDED | COUNTERBORE | | LINK END HOLE DIAMETER | 0.311 INCHES MINIMUM AND 0.314 INCHES MAXIMUM | | LINK END THICKNESS | 0.737 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367, COMP 2014, T6 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 2.440 INCHES NOMINAL | | SHAFT SECURING METHOD | SPLINE | | SPECIAL FEATURES | OFFSET HEIGHT: 1.368 IN. NOMINAL | | SPLINE QUANTITY | 44 | | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
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