NSN 2840-01-394-5231 of Nozzle Turbine Aircraft Gas Turb - Parts Details
| Alternative NSN: 2840013945231 |
| 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: 013945231 |
| NCB Code: USA (01) |
| Manufacturers: United Technologies Corporation , Therm Incorporated , Turbine Airfoil Designs Inc |
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 804351CL18, 804351 under NSN 2840-01-394-5231 of Nozzle Turbine Aircraft Gas Turb manufactured by United Technologies Corporation, Therm Incorporated, Turbine Airfoil Designs Inc.
Federal Supply Class of NSN 2840-01-394-5231 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 2840-01-394-5231, 2840013945231
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Part No Manufacturer Item Name QTY RFQ 804351CL18 United Technologies Corporation nozzle turbine aircraft gas turb Avl RFQ 804351CL18 Therm Incorporated nozzle turbine aircraft gas turb Avl RFQ 804351CL18 Turbine Airfoil Designs Inc nozzle turbine aircraft gas turb Avl RFQ 804351 United Technologies Corporation nozzle turbine aircraft gas turb Avl RFQ
Characteristics Data of NSN 2840013945231MRC Criteria Characteristic RDAL Reference Data And Literature T.O. 2J-TF33-4 FIG31 IND50 BGLW Blade Attachment Method SLOT CRTL Criticality Code Justification APGF AND CZBJ AND CZCJ AND BGLW AND FEAT APGF Design Type AXIAL COMPRESSOR ABHP Overall Length 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM AGAV End Item Identification TF-33 AIRCRAFT ENGINE MATT Material COBALT ALLOY OVERALL CZBJ Engine Section Location HIGH PRESSURE TURBINE MRC Decoded Requirement Clear Text Reply MDCL Material Document And Classification PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL FEAT Special Features FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 ABKW Overall Height 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM CXCY Part Name Assigned By Controlling Agency VANE,HPT,1 STG ABMK Overall Width 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM CZCJ Stage Number 1
| MRC | Criteria | Characteristic |
|---|---|---|
| RDAL | Reference Data And Literature | T.O. 2J-TF33-4 FIG31 IND50 |
| BGLW | Blade Attachment Method | SLOT |
| CRTL | Criticality Code Justification | APGF AND CZBJ AND CZCJ AND BGLW AND FEAT |
| APGF | Design Type | AXIAL COMPRESSOR |
| ABHP | Overall Length | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| AGAV | End Item Identification | TF-33 AIRCRAFT ENGINE |
| MATT | Material | COBALT ALLOY OVERALL |
| CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
| MRC | Decoded Requirement | Clear Text Reply |
| MDCL | Material Document And Classification | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| FEAT | Special Features | FLOW AREA 1.427-1.436; PITCH 34 DEG. 2 MIN. 28 SEC.; 2ND END WIDTH 0.760-0.780 |
| ABKW | Overall Height | 4.270 INCHES MINIMUM AND 4.300 INCHES MAXIMUM |
| CXCY | Part Name Assigned By Controlling Agency | VANE,HPT,1 STG |
| ABMK | Overall Width | 1.110 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| CZCJ | Stage Number | 1 |