Thank you for taking interest in United Technologies Corporation part number 503574, which is listed with the NSN 2840-00-063-4848 and a product description of “Pin Bearing Seal.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 503574, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Pin Bearing Seal part with the NSN 2840-00-063-4848. For example, you can browse other United Technologies Corporation components that were produced under CAGE Code 77445 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 503574 and other desired offerings on Aerospace Spare.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-063-4848 Item PartTypeName: PIN,BEARING SEAL | 2840 | 000634848 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
503574 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF-30 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STAINLESS STEEL AMS 5613,ROCKWELL C 19-25 HARDNESS,CHROMIUM PLATE PER AMS 2406,1.700 IN. LG,0.235 MIN IN. 0.245 MAX IN. DIA 1ST END,0.395 MIN IN. 0.405 MAX IN. DIA OF SHOULDER END,0.065 MIN IN. 0.075 MAX IN. DIA OF HOLE |
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