Thank you for taking interest in United Technologies Corporation part number 4084243CLM, which is listed with the NSN 2840-01-447-4909 and a product description of “Nozzle Assembly Turbine Aircraft.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 4084243CLM, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Nozzle Assembly Turbine Aircraft part with the NSN 2840-01-447-4909. For example, you can browse other United Technologies Corporation components that were produced under CAGE Code 77445 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 4084243CLM and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-447-4909 Item PartTypeName: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT | 2840 | 014474909 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | 0 | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4084243CLM | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| BGLW | Blade Attachment Method | SLOT |
| FEAT | Special Features | T.O. 2J-F100-24, FIG 109; FLOW AREA 4.615-4.639 SQUARE INCH AREA |
| CRTL | Criticality Code Justification | MATT AND ABKW AND ABMK AND ABHP AND FEAT |
| APGF | Design Type | AXIAL COMPRESSOR |
| ABHP | Overall Length | 2.820 INCHES NOMINAL |
| AGAV | End Item Identification | F100-PW-100/200/220E AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | Engine Section Location | LOW PRESSURE TURBINE |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | NICKEL ALLOY OVERALL |
| ABKW | Overall Height | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM |
| CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME VANE,TURBINE STATOR |
| ABMK | Overall Width | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM |
| CZCJ | Stage Number | 3 |
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