We appreciate your interest in United Technologies Corporation part number 710411, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 710411 is listed with the NSN 2840-00-929-4378 and description “Hub Compressor Aircraft Gas Turb.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by United Technologies Corporation under the CAGE Code 77445 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-00-929-4378 parts and Hub Compressor Aircraft Gas Turb items your operations require, so request a quote today.
| 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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