NSN 2840-01-394-5226 of Nozzle Turbine Aircraft Gas Turb - Parts Details
| Alternative NSN: 2840013945226 |
| Item Name: Nozzle Turbine Aircraft Gas Turb |
| FSG: 28 Engines Turbines and Components |
| Federal Supply Class (FSC): 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN: 013945226 |
| NCB Code: USA (01) |
| Manufacturers: Therm Incorporated , Turbine Airfoil Designs Inc , United Technologies Corporation |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 804351CL19, 804351 under NSN 2840-01-394-5226 of Nozzle Turbine Aircraft Gas Turb manufactured by Therm Incorporated, Turbine Airfoil Designs Inc, United Technologies Corporation.
Federal Supply Class of NSN 2840-01-394-5226 is FSC 2840 contains part details of Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Quote for your desired part numbers.
Part Number's List for NSN 2840-01-394-5226, 2840013945226
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Part No Manufacturer Item Name QTY RFQ 804351CL19 Therm Incorporated nozzle turbine aircraft gas turb Avl RFQ 804351CL19 Turbine Airfoil Designs Inc nozzle turbine aircraft gas turb Avl RFQ 804351CL19 United Technologies Corporation nozzle turbine aircraft gas turb Avl RFQ 804351 United Technologies Corporation nozzle turbine aircraft gas turb Avl RFQ
Characteristics Data of NSN 2840013945226MRC Criteria Characteristic ABHP OVERALL LENGTH 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" ABKW OVERALL HEIGHT 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" ABMK OVERALL WIDTH 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" AGAV END ITEM IDENTIFICATION TF-33 AIRCRAFT ENGINE" APGF DESIGN TYPE AXIAL COMPRESSOR" BGLW BLADE ATTACHMENT METHOD SLOT" CRTL CRITICALITY CODE JUSTIFICATION APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY VANE-TURB STTR, 1 STG" CZBJ ENGINE SECTION LOCATION HIGH PRESSURE TURBINE" CZCJ STAGE NUMBER 1" FEAT SPECIAL FEATURES FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780" MATT III MATERIAL COBALT ALLOY OVERALL" MDCL MATERIAL DOCUMENT AND CLASSIFICATION PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" RDAL REFERENCE DATA AND LITERATURE T.O. 2J-TF33-4 FIG31 IND50" ABHP OVERALL LENGTH 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" ABKW OVERALL HEIGHT 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" ABMK OVERALL WIDTH 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" AGAV END ITEM IDENTIFICATION TF-33 AIRCRAFT ENGINE" APGF DESIGN TYPE AXIAL COMPRESSOR" BGLW BLADE ATTACHMENT METHOD SLOT" CRTL CRITICALITY CODE JUSTIFICATION APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY VANE-TURB STTR, 1 STG" CZBJ ENGINE SECTION LOCATION HIGH PRESSURE TURBINE" CZCJ STAGE NUMBER 1" FEAT SPECIAL FEATURES FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780" MATT III MATERIAL COBALT ALLOY OVERALL" MDCL MATERIAL DOCUMENT AND CLASSIFICATION PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" RDAL REFERENCE DATA AND LITERATURE T.O. 2J-TF33-4 FIG31 IND50"
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| BGLW | BLADE ATTACHMENT METHOD | SLOT" |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR, 1 STG" |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE" |
| CZCJ | STAGE NUMBER | 1" |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780" |
| MATT | III MATERIAL | COBALT ALLOY OVERALL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50" |
| ABHP | OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM" |
| ABKW | OVERALL HEIGHT | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM" |
| ABMK | OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM" |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE" |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR" |
| BGLW | BLADE ATTACHMENT METHOD | SLOT" |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE-TURB STTR, 1 STG" |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE" |
| CZCJ | STAGE NUMBER | 1" |
| FEAT | SPECIAL FEATURES | FLOW AREA 1.436-1.446; PITCH 34 DEG. 11 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780" |
| MATT | III MATERIAL | COBALT ALLOY OVERALL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL" |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG31 IND50" |