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National Stock Number:
1680-00-092-0396
Federal Supply Class:
1680
National Item Identification Number:
000920396
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:
| 338823L | 0A489 | LOCKHEED MARTIN AEROPARTS, INC. | | 338823L | 17772 | AERO ENGINEERING & MANUFACTURING COMPANY OF CALIFORNIA, LLC | | 338823L | 3H683 | INTERNATIONAL PRECISION, INC | | 338823L | 58730 | AIRBORNE TECHNOLOGIES, INC. | | 338823L | 8X044 | DERCO AEROSPACE, INC. | | 338823L | 98897 | LOCKHEED MARTIN CORP |
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Techincal Specification:
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 7.000 INCHES NOMINAL | | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.814 INCHES MINIMUM AND 0.819 INCHES MAXIMUM | | LINK END THICKNESS | 1.306 INCHES NOMINAL | | LINK END HOLE DIAMETER | 0.375 INCHES MINIMUM AND 0.377 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367, 2014-T6 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 1.800 INCHES NOMINAL | | STYLE DESIGNATOR | OFFSET, CLEVIS LINK END |
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