| Mfg Part Number: 804351CL19 | Manufacturer: Therm Incorporated |
| NSN : 2840-01-394-5226 | NIIN : 013945226 |
| Item Name : nozzle turbine airc | CAGE Code : 99160 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in our available 804351CL19 NSN part. This part number 804351CL19 is a Nozzle Turbine Airc listed under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, and it is manufactured by Therm Incorporated. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 804351CL19 NSN component, and we carry recently requested NSN components such as 2840013945226. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as Therm Incorporated. If you are interested in this particular item, we invite you to begin the purchasing process for 804351CL19 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5226 Item Description: Nozzle Turbine Airc | 2840 | 013945226 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351CL19 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR, 1 STG |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| AGAV | III END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
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