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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 Corp
Item Name : Damper Turbine Blade Aircraft Tu
Thank you for your interest in our available parts and components on NSN Target. Damper Turbine Blade Aircraft Tu is an item listed with the part number 4082885, and it is manufactured by United Technologies Corp. This particular item 4082885 is currently available for purchase through our website today, and our team of industry experts are on standby 24/7x365 to provide rapid lead-times and competitive pricing. To begin the purchasing process, we invite you to fill out and submit an Instant RFQ form as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to provide a quote that has been personalized to fit your individual needs.
NSN Parts is a website that is owned and operated by ASAP Semiconductor, and we serve as a leading independent distributor of NSN parts and components that serve many industries and applications. Throughout our extensive part and manufacturer catalogues, we carry a variety of top requested components that you may need, including 4082885 with NSN 2840014401697 and other parts manufactured by United Technologies Corp. Quality is of the utmost importance to us at NSN Parts, and we have established ourselves as an FAA AC 00-56B, AS9120B, and ISO 9001:2015 certified enterprise. Get started today with a personalized quote and experience how we are revolutionizing the parts procurement process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-440-1697 Item Description: Damper Turbine Blade Aircraft Tu | 2840 | 014401697 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4082885 | 2 | 2 | 5 |
| 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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