Thank you for your interest in Northrop Grumman Systems Corporation part number 3-13437-5, a Lever Remote Contro item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 1680-00-768-3088, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.
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Besides part number 3-13437-5, you may browse our platform further for similar components produced by Northrop Grumman Systems Corporation under the CAGECode 76823, as well as additional products that are categorized under FSC 1680 Miscellaneous Aircraft Accessories Components. If you have any questions regarding our services or the NSN 1680-00-768-3088 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number 3-13437-5 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1680-00-768-3088 Item PartTypeName: LEVER,REMOTE CONTROL | 1680 | 007683088 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
3-13437-5 | 2 | 1 | C | 9 |
MRC | Criteria | Characteristic |
---|---|---|
BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.593 INCHES MINIMUM AND 0.598 INCHES MAXIMUM |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
MATT | MATERIAL | ALUMINUM ALLOY |
STYL | STYLE DESIGNATOR | OFFSET,CLEVIS LINK END |
ASBP | BORE TYPE | SERRATED |
BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 3.000 INCHES NOMINAL |
BFGX | SHAFT END THICKNESS | 0.610 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
BFGY | LINK END THICKNESS | 0.793 INCHES NOMINAL |
BFHA | LINK END HOLE DIAMETER | 0.250 INCHES NOMINAL |
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 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367,COMP 2014,T6 FED SPEC SINGLE MATERIAL RESPONSE |
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