Thank you for taking interest in United Technologies Corporation part number 4063801, which is listed with the NSN 2840-01-205-1280 and a product description of “Blade Turbine Rotor Aircraft Gas.” 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 4063801, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Blade Turbine Rotor Aircraft Gas part with the NSN 2840-01-205-1280. 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 4063801 and other desired offerings on Aerospace Spare.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-205-1280 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 012051280 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4063801 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | ACFT ENG F100 |
APGF | DESIGN TYPE | COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
CZCJ | STAGE NUMBER | 1 |
FEAT | SPECIAL FEATURES | THIS NSN IS AN F100 FRACTURE CRITICAL ITEM. T.O. 2J-F100-4,FIG 116,IND 47 |
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