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| Part No. : 804351CL20 | Manufacturer : turbine airfoil designs inc | Item Name: nozzle turbine aircraft gas turb |
| NSN: 2840-01-394-5228 (2840013945228) | CAGE Code: 96965 |
If you require part number 804351CL20 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 804351CL20 which is listed under the Federal Supply Class . 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 2840013945228 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 804351CL20 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 |
|---|---|---|---|---|---|---|
| 2840-01-394-5228 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945228 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804351CL20 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.446-1.455 PITCH 34 DEG. 20 MIN. 28 SEC. 2ND END WIDTH 0.760-0.780 IN. |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT 1 STG |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| CZCJ | STAGE NUMBER | 1 |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
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