Maintenance Parts Pro is pleased to offer procurement options for Northrop Grumman Technical Services Inc part number 2-13819-5, a Lever Remote Contro product we carry that is listed with the NSN 1680-00-767-9572 for seamless identification. As this item is available for purchase today, be sure to fill out and submit the Request for Quote (RFQ) form on this page if you are interested in obtaining pricing information. All that we ask is that you share details like your budget, desired quantity, and expected fulfillment speed so that we can respond with the most fitting solutions for your comparisons.
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Alongside streamlined quotation processes, we aim to support our customers by providing as much relevant listing information and data with product offerings as possible. For example, part number 2-13819-5 specifically traces back to Northrop Grumman Technical Services Inc through CAGE Code 0JRC1, as well as belongs to the FSC [FSC] as per its NSN of 1680-00-767-9572. Referencing such details, you can locate and procure exact specifications with ease. With our various practices in mind, do not hesitate to request a quote on part number 2-13819-5 using our provided form.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1680-00-767-9572 Item PartTypeName: LEVER,REMOTE CONTROL | 1680 | 007679572 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
2-13819-5 | 2 | 9 | 3 |
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 |
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