Thank you for choosing to partner with National Stock Number Shop for the Isolator Auxillary NSN parts you require. On this page, you can submit a quote request for Barry Wright Corporation part number 93572-01, a component that can also be found by inputting NSN 1680014819577 in our search engine. Apart from this item, we also have an array of other in-demand part numbers, all of which can be traced back to a conglomerate of well-known manufacturers that we trust. Explore our expansive part catalogs by scrolling over to our menu and locate products according to manufacturer, NIIN, NSN, and more.
National Stock Number Shop works with numerous government and defense agencies, so we use CAGE Codes like 13636 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find Barry Wright Corporation parts under the FSC 1680 Miscellaneous Aircraft Accessories Components with ease. With this in mind, we encourage you to complete the RFQ form below for NSN 1680014819577 or any others, and see how we can provide you with a customized sourcing solution. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock for customer inquiries!
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| 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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