NSN 1680-00-768-3088
Part Details | REMOTE CONTROL LEVER
1680-00-768-3088 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: 3134375, 3-13437-5, 3134371, 3-13437-1, 3134375, 3-13437-5, 3134371, 3-13437-1, 1680-00-768-3088, 00-768-3088, 1680007683088, 007683088
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 01, 1962 | 00-768-3088 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
FLAT, ONE HOLE LINK END
Cross Reference | NSN 1680-00-768-3088
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3-13437-5 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 3-13437-1 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 3-13437-5 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
| 3-13437-1 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
Technical Data | NSN 1680-00-768-3088
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367, COMP 2014, T6 FED SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | 5 FLAT, ONE HOLE LINK END |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 3.000 INCHES NOMINAL |
| SHAFT END THICKNESS | 0.610 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
| LINK END THICKNESS | 0.793 INCHES NOMINAL |
| LINK END HOLE DIAMETER | 0.250 INCHES NOMINAL |
| DISTANCE BETWEEN FORK INSIDE SPREAD | 0.593 INCHES MINIMUM AND 0.598 INCHES MAXIMUM |
| BORE TYPE | SERRATED |
| SHAFT SECURING METHOD | SERRATIONS |
| SPECIAL FEATURES | THIS ITEM HAS BEEN DETERMINED TO BE A CRITICAL APPLICATION ITEM. IN-FLIGHT FAILURE OF THIS ITEM WOULD CREATE A HAZARDOUS CONDITION |
| CRITICALITY CODE JUSTIFICATION | FEAT |