Thank you for taking interest in the United Technologies Corporation part number 530082, a Hub Compressor Aircraft Gas Turb product that we stock that is presented alongside the NSN 2840-00-929-4378 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 530082 specifically traces back to United Technologies Corporation through the CAGE Code 77445, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-00-929-4378, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 530082 here on Aero OEM Parts at your earliest convenience.
| 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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