To receive competitive purchasing options on part number 93572-01 by Barry Wright Corporation, look no further than NSN Direct. For your reference, this item has the NSN 1680-01-481-9577 and is listed with the description “Isolator Auxillary.” 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 Barry Wright Corporation parts produced under the CAGE Code 13636, 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 93572-01, you can glean from the first four digits of its NSN 1680-01-481-9577 that it belongs to the FSC 1680 Miscellaneous Aircraft Accessories Components. This being said, do not hesitate to request quotes on part number 93572-01 and any other NSN parts that we feature to experience unrivaled procurement.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1680-01-481-9577 Item PartTypeName: ISOLATOR,AUXILLARY | 1680 | 014819577 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
93572-01 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MRC | Decoded Requirement | Clear Text Reply |
TEXT | General Characteristics Item Description | METAL COMPONENTS MADE FROM 17-4PH OR 15-5PH STAINLESS STEEL WHICH IS HEAT TREATED TO 160,000 PSI; ELASTOMER IS MADE OF RUBBER; CONSISTS OF A MOLDED CORE, APU BRACKETS, COVER PLATE, AND OUTER HOUSING WHICH ATTACHES TO THE AFT FUSELAGE STRUCTURE THROUGH STRUTS; DESIGNED TO MINIMIZE NOISE TRANSMISSION FROM THE APU INTO THE PASSENGER CABIN, LIMIT SHOCK LOADS FROM THE AIRFRAME, AND LIMIT DEFLECTION OF THE APU; FORWARD LEFT ISOLATOR |
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