NSN 2840-00-927-2618 Blade Compressor Aircraft Gas Tu manufactured by United Technologies Corporation, Turbine Engine Components Textron, Airfoil Textron Inc 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 576712. 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 2840-00-927-2618 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 2840-00-927-2618 part today and allow us to simplify your procurement process.
Alternative NSN: 2840-00-927-2618 |
Item Name:Blade Compressor Aircraft Gas Tu |
FSG: 28 Engines Turbines and Components |
Federal Supply Class (FSC): 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
NCB Code: USA (00) |
Manufacturers: United Technologies Corporation , Turbine Engine Components Textron , Airfoil Textron Inc |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
576712 | United Technologies Corporation | blade compressor aircraft gas tu | Avl | RFQ |
576712 | Turbine Engine Components Textron | blade compressor aircraft gas tu | Avl | RFQ |
576712 | Airfoil Textron Inc | blade compressor aircraft gas tu | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.944 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 0.834 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.415 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
APGF | DESIGN TYPE | COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
MATT | III MATERIAL | NICKEL ALLOY BLADE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1003 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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