| Mfg Part Number: 4082885 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-440-1697 | NIIN : 014401697 |
| Item Name : damper turbine blad | CAGE Code : 77445 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in our available 4082885 NSN part. This part number 4082885 is a Damper Turbine Blad 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 4082885 NSN component, and we carry recently requested NSN components such as 2840014401697. 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 4082885 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.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-440-1697 Item Description: Damper Turbine Blad | 2840 | 014401697 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4082885 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CQFM | HARDNESS RATING | 34.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL |
| AGAV | III END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| ABMZ | DIAMETER | 16.788 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| ABHP | OVERALL LENGTH | 0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 21; REPL P/N 4074864 ONCE TCTO HAS BEEN ACCOMPLISHED; RETAINING PLATE DAMPER IS SYMMETRICAL IN SHAPE AND HAS 6 RETENTION TABS FORWARD AND AFT TO PRECLUDE POSSIBLE REVERSE INSTALLATION AND RESULTING CUT-OFF OF COOLING AIR TO THE 2ND STAGE BLADES |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
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