Thank you for taking an interest in the various Isolator Auxillary components that we offer here on ASAP Military Parts, such as those listed with NSN 1680014819577. The particular item that you have taken an interest in is listed alongside the part number 93572-01, having been manufactured by Barry Wright Corporation. With current availability for this product, we encourage you to utilize our online RFQ forms to quickly and easily request quotes for your comparisons. Within 15 minutes of us receiving a completed request and reviewing your provided details, a member of our staff will reach out to you to present a tailored solution.
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To make the part procurement process as simple as possible, we choose to list all offerings with as many details as we can to ensure that you find exactly what you require with ease. For example, with the NSN 1680-01-481-9577, one can determine that part number 93572-01 belongs to FSC 1680 Miscellaneous Aircraft Accessories Components. Furthermore, its manufacturer Barry Wright Corporation specifically produced this part under CAGE Code 13636, allowing you to know the exact facility it traces back to. If you are ready to begin procurement for part number 93572-01, send us a completed RFQ form today. You may also give us a call or email at any time, and we would be more than happy to assist you however we can as your strategic sourcing partner!
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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