NSN 1680-00-767-9572
Part Details | REMOTE CONTROL LEVER
1680-00-767-9572 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: 2138195, 2-13819-5, 2138191, 2-13819-1, 2138195, 2-13819-5, 1680-00-767-9572, 00-767-9572, 1680007679572, 007679572
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 01, 1962 | 00-767-9572 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
FLAT, ONE HOLE LINK END
Cross Reference | NSN 1680-00-767-9572
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-13819-5 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 2-13819-1 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 2-13819-5 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
Technical Data | NSN 1680-00-767-9572
| Characteristic | Specifications |
|---|---|
| MATERIAL | MAGNESIUM ALLOY |
| STYLE DESIGNATOR | 4 FLAT, ONE HOLE LINK END |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.000 INCHES NOMINAL |
| SHAFT END THICKNESS | 0.590 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
| LINK END THICKNESS | 0.640 INCHES MINIMUM AND 0.700 INCHES MAXIMUM |
| LINK END HOLE DIAMETER | 0.190 INCHES NOMINAL |
| DISTANCE BETWEEN FORK INSIDE SPREAD | 0.438 INCHES MINIMUM AND 0.443 INCHES MAXIMUM |
| BORE TYPE | SERRATED |
| MINOR DIAMETER | 0.583 INCHES MINIMUM AND 0.584 INCHES MAXIMUM |
| 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 |