Thank you for taking interest in United Technologies Corporation part number 530082, which is listed with the NSN 2840-00-929-4378 and a product description of “Hub Compressor Aircraft Gas Turb.” 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 530082, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Hub Compressor Aircraft Gas Turb part with the NSN 2840-00-929-4378. 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 530082 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-929-4378 Item PartTypeName: HUB,COMPRESSOR,AIRCRAFT GAS TURB | 2840 | 009294378 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 710411 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 16.500 INCHES MINIMUM AND 16.570 INCHES MAXIMUM |
| ABMZ | DIAMETER | 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ENGINE MODEL TF33 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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