NSN 2840-01-394-5231 Nozzle Turbine Aircraft Gas Turb manufactured by Turbine Airfoil Designs Inc, United Technologies Corporation, Therm Incorporated is available within ASAP Part Service’s ready-to-ship inventory. Owned and operated by ASAP Semiconductor, ASAP Part Services has over 6 billion parts within its inventory including 804351, 804351CL18. ASAP is committed to streamlining the parts procurement process for our customers. We make it easy for our customers to search through billions of parts to find the exact part they are looking for.
A dedicated ASAP account manager is ready to help solve any procurement issues or needs that a customer may have. As a company we are quick and responsive meaning we can deliver a part within an AOG timeframe. Quality control is at the center of all that we do. Each and every NSN 2840-01-394-5231 part is subject to numerous quality checks that are designed to screen out any part imperfections or validity issues. Subject a request for quote for NSN 2840-01-394-5231 part today and allow us to simplify your procurement process.
Alternative NSN: 2840-01-394-5231 |
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 |
NCB Code: USA (01) |
Manufacturers: Turbine Airfoil Designs Inc , United Technologies Corporation , Therm Incorporated |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
804351 | Turbine Airfoil Designs Inc | nozzle turbine aircraft gas turb | Avl | RFQ |
804351 | United Technologies Corporation | nozzle turbine aircraft gas turb | Avl | RFQ |
804351 | Therm Incorporated | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL18 | United Technologies Corporation | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL18 | Turbine Airfoil Designs Inc | nozzle turbine aircraft gas turb | Avl | RFQ |
804351CL18 | Therm Incorporated | nozzle turbine aircraft gas turb | Avl | RFQ |
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 |
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