Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-425-7589 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 4082504, 4081904, 2840-01-425-7589, 01-425-7589, 2840014257589, 014257589
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 27, 1996 | 01-425-7589 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-425-7589
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082504 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4081904 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-425-7589
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 4 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.929 INCHES NOMINAL |
| SPECIAL FEATURES | NOT TO BE PROCURED; NSN REQUIRED; THIS IS A SINGLE ROBUST BLADE |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$ACZCJ$$ABGLW$$AABHP |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |