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| Item Name | Lever Remote Contro |
| Federal Supply Group (FSG) | Aircraft Components and Accessories |
| Federal Supply Class (FSC) | 1680 Miscellaneous Aircraft Accessories Components |
| National Item Identification Number (NIIN) | 00-767-9572 (007679572) |
| NCB Code | USA (00) |
| Manufacturer | Northrop Grumman Technical Services Inc, Northrop Grumman Systems Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.000 INCHES NOMINAL |
| BFGY | LINK END THICKNESS | 0.640 INCHES MINIMUM AND 0.700 INCHES MAXIMUM |
| BFHA | LINK END HOLE DIAMETER | 0.190 INCHES NOMINAL |
| AGJR | MINOR DIAMETER | 0.583 INCHES MINIMUM AND 0.584 INCHES MAXIMUM |
| ASBP | BORE TYPE | SERRATED |
| BFGX | SHAFT END THICKNESS | 0.590 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
| BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.438 INCHES MINIMUM AND 0.443 INCHES MAXIMUM |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CZLP | SHAFT SECURING METHOD | SERRATIONS |
| FEAT | SPECIAL FEATURES | THIS ITEM HAS BEEN DETERMINED TO BE A CRITICAL APPLICATION ITEM. IN-FLIGHT FAILURE OF THIS ITEM WOULD CREATE A HAZARDOUS CONDITION |
| MATT | MATERIAL | MAGNESIUM ALLOY |
| STYL | STYLE DESIGNATOR | CLEVIS LINK END,SECURING HOLE(S) SHAFT END |
| Relevant Components for NSN - 1680-00-767-9572, 1680007679572 | ||||
| 1650-00-084-8670 (1650000848670) | 1650-00-880-3734 (1650008803734) | 1650-01-022-9496 (1650010229496) | 1650-00-840-5467 (1650008405467) | |
| 1660-01-336-7435 (1660013367435) | 1660-01-664-6031 (1660016646031) | 1680-01-152-9626 (1680011529626) | 1650-01-384-8665 (1650013848665) | |
| 1620-00-990-6198 (1620009906198) | 1680-01-569-9366 (1680015699366) | 1680-01-559-1098 (1680015591098) | 1670-00-089-5212 (1670000895212) | |
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