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Upload| Part Number : 804351CL20 | NSN : 2840013945228 |
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| Manufacturer : Turbine Airfoil Designs Inc | CAGE Code : 96965 | FSC Details : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN : 013945228 | INC Code : 50585 | Country : USA |
| NCB Code : 01 |
Thank You for Submitting Your RFQ for Part Number 804351CL20 by Turbine Airfoil Designs Inc
We always put our customers’ needs first, and we are always just a click or call away from assisting you throughout the purchasing process whenever you need it. Please do not hesitate to call our toll-free number +1-714-705-4780 for any inquiries about part number 804351CL20, or send us an email listing your needs, and we will get back to you as soon as possible. Whatever your requirements may be, we will not rest until we have fulfilled all your operational needs with highly competitive options.
| 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 |
| 804351 | 2 | 9 | D |
| 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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