Thank you for taking interest in United Technologies Corporation part number 804351CL19, which is listed with the NSN 2840-01-394-5226 and a product description of “Nozzle Turbine Aircraft Gas Turb.” 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 804351CL19, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Nozzle Turbine Aircraft Gas Turb part with the NSN 2840-01-394-5226. 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 804351CL19 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5226 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945226 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351CL19 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR,1 STG |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
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