We appreciate your interest in Barry Wright Corporation part number 93572-02, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 93572-02 is listed with the NSN 1680-01-481-9579 and description “Isolator Auxillary.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Barry Wright Corporation under the CAGE Code 13636 or that similarly fall under the FSC 1680 Miscellaneous Aircraft Accessories Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 1680-01-481-9579 parts and Isolator Auxillary items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1680-01-481-9579 Item PartTypeName: ISOLATOR,AUXILLARY | 1680 | 014819579 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 93572-02 | 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 RIGHT ISOLATOR |
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