To receive competitive purchasing options on part number 114R3123-1 by The Boeing Company, look no further than NSN Direct. For your reference, this item has the NSN 1615-00-875-9742 and is listed with the description “Retainer Rotary Wing.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other The Boeing Company parts produced under the CAGE Code 77272, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number 114R3123-1, you can glean from the first four digits of its NSN 1615-00-875-9742 that it belongs to the FSC 1615 Helicopter Rotor Blades Drive Mechanisms and Components. This being said, do not hesitate to request quotes on part number 114R3123-1 and any other NSN parts that we feature to experience unrivaled procurement.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1615-00-875-9742 Item PartTypeName: RETAINER,ROTARY WING | 1615 | 008759742 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
114R3123-1 | 5 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY AMS4260 COMP 356-T6,ANODIZED MIL-C-5541,DIM.,3.094 IN. NOM LG,2.250 IN. CENTER DIA,1.000 IN. RADIUS OF CURVATURE ON TOP AND BOTTOM 45.0 DEG LEFT AND RIGHT OF VERTICAL CENTERLINE,0.090 IN. NOM CENTER MATERIALTHK,0.340 IN. NOM |
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