Thank you for taking an interest in part number 804351CL17, a Therm Incorporated product we have in stock that is listed alongside the NSN 2840013945230 and the description “Nozzle Turbine Aircraft Gas Turb.” As part number 804351CL17 is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number 804351CL17 is listed alongside the NSN 2840-01-394-5230, meaning that it also belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Furthermore, this NSN part is specifically manufactured under CAGE Code 99160, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
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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