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National Stock Number:
3040-01-020-0570
Federal Supply Class:
3040
National Item Identification Number:
010200570
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:
| 69-31940-1 | 17765 | THE BOEING COMPANY | | 69-31940-1 | 81205 | THE BOEING COMPANY | | 69-31940-501 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
| BORE DIAMETER | 1.750 INCHES NOMINAL | | BORE LENGTH | 0.495 INCHES NOMINAL | | BORE TYPE | PLAIN STRAIGHT | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 4.000 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.500 INCHES NOMINAL | | FEATURES PROVIDED | COUNTERBORE | | LINK END HOLE DIAMETER | 0.250 INCHES NOMINAL | | LINK END THICKNESS | 0.940 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-268, T4 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 0.495 INCHES NOMINAL | | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
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