NSN 1680-00-906-8861
Part Details | REMOTE CONTROL LEVER
1680-00-906-8861 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.
Alternate Parts: 6540403419041, 65404-03419-041, 6540403419041, 65404-03419-041, 1680-00-906-8861, 00-906-8861, 1680009068861, 009068861
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JUN 17, 1966 | 00-906-8861 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
FLAT, ONE HOLE LINK END
Cross Reference | NSN 1680-00-906-8861
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 65404-03419-041 | D1081 | AIRBUS DEUTSCHLAND GMBH -WERKBREMEN- |
| 65404-03419-041 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
Technical Data | NSN 1680-00-906-8861
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-A-22771, COMP 7075-T73 MIL SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | 4 FLAT, ONE HOLE LINK END |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 5.911 INCHES NOMINAL |
| SHAFT END THICKNESS | 1.495 INCHES MINIMUM AND 1.500 INCHES MAXIMUM |
| LINK END THICKNESS | 1.480 INCHES NOMINAL |
| LINK END HOLE DIAMETER | 0.312 INCHES MINIMUM AND 0.313 INCHES MAXIMUM |
| DISTANCE BETWEEN FORK INSIDE SPREAD | 1.050 INCHES MINIMUM AND 1.060 INCHES MAXIMUM |
| BORE TYPE | PLAIN STRAIGHT |
| BORE DIAMETER | 1.814 INCHES MINIMUM AND 1.815 INCHES MAXIMUM |
| BORE LENGTH | 1.495 INCHES MINIMUM AND 1.500 INCHES MAXIMUM |