Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-371-5782 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: 3054158040, 305-415-804-0, 3054158040, 305-415-804-0, 2840-01-371-5782, 01-371-5782, 2840013715782, 013715782
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 19, 1993 | 01-371-5782 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-371-5782
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 305-415-804-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-804-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-371-5782
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 4.000 INCHES NOMINAL |
| SPECIAL FEATURES | MATERIAL INCONEL 100 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14,FIG FIN 72-54-00-9 IND 525 |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE ASSY-LPT RTR STG 1 |