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Quality guaranteed We sell only warrantied and traceable partsMfg Part Number: 4082885
NSN : 2840-01-440-1697
NIIN : 014401697
CAGE Code : 77445
Manufacturer: United Technologies Corporation
Item Name : Damper Turbine Blad
In our inventory, we have more than two billion new and obsolete NSN part like 4082885. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like 4082885 Damper Turbine Blad from manufacturer United Technologies Corporation and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like 4082885, you purchase from us is fully traceable or comes directly from its manufacturer.
Our website offers a number of parametric search capabilities, one of which allows you to search specifically for NSN part like 4082885. This means you can quickly sort through National Stock Numbers such as 2840014401697 and find parts from quality manufacturers like United Technologies Corporation and many others. To begin the purchasing process immediately, submit an RFQ today. Our team of dedicated account managers is standing by and will respond to all inquiries in 15 minutes or less.
| 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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