Thank you for your interest in United Technologies Corporation part number 854801, a Disk And Hub Compressor Aircraft item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 2840-00-088-0474, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.
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Besides part number 854801, you may browse our platform further for similar components produced by United Technologies Corporation under the CAGECode 77445, as well as additional products that are categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. If you have any questions regarding our services or the NSN 2840-00-088-0474 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number 854801 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-088-0474 Item Description: Disk And Hub Compressor Aircraft | 2840 | 000880474 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
854801 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | III END ITEM IDENTIFICATION | TF33-3/5/9/102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDES P/N 431001 |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 5, IND 2 OR TF-33-34, FIG 5, IND 1 |
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