Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-205-0574 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: 4059422, 2840-01-205-0574, 01-205-0574, 2840012050574, 012050574
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 14, 1997 | 01-205-0574 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-205-0574
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4059422 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-205-0574
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 3.842 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 121, IND 44; F100 FRACTURE CRITICAL PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FSC APPLICATION DATA | F-15 AIRCRAFT |