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| Part No. : 804351CL19 | Manufacturer : turbine airfoil designs inc | Item Name: nozzle turbine aircraft gas turb |
| NSN: 2840-01-394-5226 (2840013945226) | CAGE Code: 96965 | FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
If you require part number 804351CL19 from Turbine Airfoil Designs Inc which is described as a Nozzle Turbine Aircraft Gas Turb component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 804351CL19 which is listed under the Federal Supply Class 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 2840013945226 and was produced under the CAGE Code 96965. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 804351CL19 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs.
| 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 |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR,1 STG |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| 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 |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446 PITCH 34 DEG. 11 MIN. 28 SEC. 2ND END WIDTH 0.760-0.780 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
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