Mfg Part Number: 93572-01 | Alternate P/N: 9357201 | NSN : 1680-01-481-9577 |
NIIN : 014819577 | CAGE Code : 13636 | Manufacturer: Barry Wright Corporation |
Item Name : Isolator Auxillary | FSC : 1680 Miscellaneous Aircraft Accessories and Components |
If you are in the market for NSN part like 93572-01 of Isolator Auxillary components with the NSN 1680-01-481-9577, we have you covered here on Single Source Spares. Listed alongside the part number 93572-01, this particular NSN component was originally manufactured by Barry Wright Corporation. All listings are ready for purchase from our website at any time, so you can easily request a quote for your comparisons on 93572-01 part through the completion and submission of the form provided on this page. To ensure a customized solution that meets your needs, please let us know information such as your target price and expected shipping time frame. Once we have received a completed form, a dedicated account representative will rapidly formulate a quote and present it to you in just 15 minutes or less.
To ensure that customers only procure the exact items that they need, we try to list our parts with all of their applicable information. For example, 93572-01 part of Barry Wright Corporation was specifically manufactured under FSC 1680 Miscellaneous Aircraft Accessories and Components and the CAGE Code 13636. Additionally, if you choose to purchase this item, it will ship with any applicable qualifying certifications or manufacturing trace documentation for your benefit. Kick-start the procurement process today and see how Single Sourcing Spares can serve as your strategic sourcing partner for all your operational needs!
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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