Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-371-5783 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: 3054159080, 305-415-908-0, 3054159070, 305-415-907-0, 3054159080, 305-415-908-0, 3054159070, 305-415-907-0, 2840-01-371-5783, 01-371-5783, 2840013715783, 013715783
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 19, 1993 | 01-371-5783 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-371-5783
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 305-415-908-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-907-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-908-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 305-415-907-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-371-5783
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 5.500 INCHES NOMINAL |
| SPECIAL FEATURES | MATERIAL RENE 77 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14, FIG 72-54-00-9A, IND 54A |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE ASSY-LPT RTR STG 2 |