Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 804351, a United Technologies Corporation item that is listed alongside the description “Nozzle Turbine Aircraft Gas Turb” and the NSN 2840013945885. To guarantee a swift procurement process for NSN part number 804351, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 804351 is manufactured by United Technologies Corporation, it is specifically done so under CAGE Code 77445, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 2840-01-394-5885, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
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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