NSN 2840-01-076-5887 Rotor Turbine Aircraft Gas Turbi manufactured by Rolls Royce Corp, Mtu Detroit Diesel Australia Pty Ltd, Allison Transmission Holdings 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 6898782. 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 2840-01-076-5887 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 2840-01-076-5887 part today and allow us to simplify your procurement process.
Alternative NSN: 2840-01-076-5887 |
Item Name:Rotor Turbine Aircraft Gas Turbi |
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: Rolls Royce Corp , Mtu Detroit Diesel Australia Pty Ltd , Allison Transmission Holdings Inc |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
6898782 | Rolls Royce Corp | rotor turbine aircraft gas turbi | Avl | RFQ |
6898782 | Mtu Detroit Diesel Australia Pty Ltd | rotor turbine aircraft gas turbi | Avl | RFQ |
6898782 | Allison Transmission Holdings Inc | rotor turbine aircraft gas turbi | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | T63-A-700 AND T63-A-720 ENGINES |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | CRES EMS73649-2,FSCM 73342,48 BLADES EQUALLY SPACED ON OUTER PERIPHERY,6.409 IN. MIN,6.411 IN. MAX OD,EXTERNAL SPLINE,17 TEETH,0.562 IN. MIN,0.567 IN. MAX OD,0.5313 IN. NOM PITCH DIA,30 DEG PRESSURE ANGLE,EXTERNAL THD,0.8438 IN.-32 UNJS CLA |
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