Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number 804351CL20, which is a Nozzle Turbine Aircraft Gas Turb item from Therm Incorporated that is listed with the NSN 2840-01-394-5228 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
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To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number 804351CL20 was specifically produced by Therm Incorporated under the CAGE Code 99160, providing traceability. Furthermore, with the NSN 2840-01-394-5228, one can also determine that this listing falls under Federal Supply Class (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number 804351CL20, and we will be in touch.
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 |
---|---|---|
ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
MATT | MATERIAL | COBALT ALLOY OVERALL |
AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
CZCJ | STAGE NUMBER | 1 |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50 |
ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
BGLW | BLADE ATTACHMENT METHOD | SLOT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT 1 STG |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
FEAT | SPECIAL FEATURES | FLOW AREA 1.446-1.455; PITCH 34 DEG. 20 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 IN. |
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