| Mfg Part Number: 804351CL17 | Manufacturer: Turbine Airfoil Designs Inc | NSN : 2840-01-394-5230 |
| NIIN : 013945230 | Item Name : nozzle turbine airc | CAGE Code : 96965 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your continued interest in the 804351CL17 part currently available on National Stock Number Parts. Here, our customers will find our NSN RFQ Page for Nozzle Turbine Airc parts under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with the NSN 2840-01-394-5230, among others from the manufacturer Turbine Airfoil Designs Inc. For particular equipment, such as part number 804351CL17, the submission of a completed RFQ form will provide customers with a quote on any desired part in just 15 minutes or less. Upon receival, our expert market representatives will use your offered information to construct a quote paramount to your operations with rapid turnaround times and cost savings at our forefront.
As our robust supply chain stretches across the United States, Canada, and the United Kingdom, we are able to supply entities facing Aircraft on Ground (AOG) delays or other unique time constraints with expedited shipping on select NSN 2840-01-394-5230 items for immediate procurement. Operating as an AS9120B, ISO 9001:2015, and FAA AC 00-56B certified enterprise, products listed on our database are upheld to rigorous quality assurance testing, inspection, and cross-referencing before shipment. Functioning as the only independent distributor with a NO CHINA SOURCING pledge, you can depend on National Stock Number Parts for authentic 804351CL17 NSN part, which are listed alongside the CAGE Code 96965 by Turbine Airfoil Designs Inc.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5230 Item Description: Nozzle Turbine Airc | 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| 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 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
| MATT | III MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
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