Thank you for considering United Technologies Corporation part number 801239, an item we carry that is listed with the NSN 2840-01-471-7748 and product description “Hub Compressor Aircraft Gas Turb.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 801239 was specifically produced by United Technologies Corporation under CAGE Code 77445, and with the NSN 2840-01-471-7748, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 801239 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-471-7748 Item PartTypeName: HUB,COMPRESSOR,AIRCRAFT GAS TURB | 2840 | 014717748 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
822666 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | DIAMETER | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | TF33-P-7A ACFT ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-14 FIGURE 19 INDEX 5A |
ABMZ | DIAMETER | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | TF33-P-7A ACFT ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-14 FIGURE 19 INDEX 5A |
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