| Mfg Part Number: 854231 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-161-1130 | NIIN : 011611130 |
| Item Name : disk and hub compre | CAGE Code : 77445 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in our available 854231 NSN part. This part number 854231 is a Disk And Hub Compre listed under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, and it is manufactured by United Technologies Corp. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 854231 NSN component, and we carry recently requested NSN components such as 2840011611130. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as United Technologies Corp. If you are interested in this particular item, we invite you to begin the purchasing process for 854231 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | DIAMETER | 5.1183 INCHES MINIMUM AND 5.1189 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF33PW-3/5/9/102/A&B AIRCRAFT GAS TURBINE ENGINES |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 4 |
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