Thank you for taking interest in the United Technologies Corporation part number 804351CL17, a Nozzle Turbine Aircraft Gas Turb product that we stock that is presented alongside the NSN 2840-01-394-5230 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 804351CL17 specifically traces back to United Technologies Corporation through the CAGE Code 77445, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-01-394-5230, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 804351CL17 here on Aero OEM Parts at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5230 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945230 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351CL17 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
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