Thank you for your interest in part number 804351CL17, a component manufactured by Therm Incorporated that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-394-5230 and features the description “Nozzle Turbine Aircraft Gas Turb.” To request a quote for part number 804351CL17, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-01-394-5230 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Therm Incorporated, which is associated with the CAGECode 99160. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 804351CL17.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-394-5230 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.418-1.427; PITCH 33 DEG. 53 MIN. 28 SEC. |
| MATT | MATERIAL | COBALT ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | APWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| BGLW | BLADE ATTACHMENT METHOD | SLOT |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| 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 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 31 IND 50 |
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