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| Part No. : 804351CL16 | Manufacturer : turbine airfoil designs inc | Item Name: nozzle turbine aircraft gas turb |
| NSN: 2840-01-394-5225 (2840013945225) | CAGE Code: 96965 | FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
If you require part number 804351CL16 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 804351CL16 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 2840013945225 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 804351CL16 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 |
|---|---|---|---|---|---|---|
| 2840-01-394-5225 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945225 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 804341 | 2 | 9 | D |
| MRC | Criteria | Characteristic |
|---|---|---|
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | FLOW AREA IS 1.409 MIN. TO 1.418 MAX. DIAMETER |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| ABHP | OVERALL LENGTH | 4.980 INCHES MINIMUM AND 5.030 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF33 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR,1 STG |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| MATT | MATERIAL | COBALT ALLOY VANE |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
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