Thank you for your interest in part number 804351CL23, a component manufactured by Therm Incorporated that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-394-5885 and features the description “Nozzle Turbine Aircraft Gas Turb.” To request a quote for part number 804351CL23, 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 2840-01-394-5885 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 804351CL23.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-394-5885 Item PartTypeName: NOZZLE,TURBINE,AIRCRAFT GAS TURB | 2840 | 013945885 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
804351CL23 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMK | OVERALL WIDTH | 2.045 INCHES NOMINAL |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,HPT,1 STG |
CZCJ | STAGE NUMBER | 1 |
FEAT | SPECIAL FEATURES | FLOW AREA 1.473-1.483.PITCH IS 34DEG 47MIN 28SEC |
ABKW | OVERALL HEIGHT | 4.153 INCHES NOMINAL |
MATT | MATERIAL | COBALT ALLOY VANE |
AGAV | END ITEM IDENTIFICATION | TF-33 |
BGLW | BLADE ATTACHMENT METHOD | SLOT |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
ABHP | OVERALL LENGTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
CRTL | CRITICALITY CODE JUSTIFICATION | ABMK |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31,IND50 |
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