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National Stock Number:
3040-00-863-6405
Federal Supply Class:
3040
National Item Identification Number:
008636405
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:
| 249-52091 | 10000 | MANEY AIRCRAFT, INC. | | 249-52091-11 | 10000 | MANEY AIRCRAFT, INC. | | 24952091-11 | 34411 | L AND E MACHINE EXPERIMENTAL LAB INC | | 249-52091-11 | 89332 | CHRYSLER CORP | | 249-52091-11 | 89372 | ROCKWELL INTERNATIONAL CORP NORTH AMERICAN AIRCRAFT OPNS |
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Techincal Specification:
| BORE DIAMETER | 1.250 INCHES NOMINAL | | BORE TYPE | PLAIN STRAIGHT | | BORE LENGTH | 0.506 INCHES NOMINAL | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 1.625 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.687 INCHES NOMINAL | | FEATURES PROVIDED | COUNTERBORE | | LINK END HOLE DIAMETER | 0.250 INCHES NOMINAL | | LINK END THICKNESS | 0.812 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-267, T4 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 0.096 INCHES MINIMUM AND 0.506 INCHES MAXIMUM | | SPECIAL FEATURES | OFFSET HEIGHT: 0.215 IN. NOMINAL | | STYLE DESIGNATOR | OFFSET, CLEVIS LINK END |
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