Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-187-8240 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: 3054158030, 305-415-803-0, 3054158020, 305-415-802-0, 3054158010, 305-415-801-0, 3054158030, 305-415-803-0, 3054158020, 305-415-802-0, 3054158010, 305-415-801-0, 2840-01-187-8240, 01-187-8240, 2840011878240, 011878240
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 25, 1984 | 01-187-8240 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-187-8240
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 305-415-803-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-802-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-801-0 | 58828 | CFM INTERNATIONAL, INC. |
| 305-415-803-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 305-415-802-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 305-415-801-0 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-187-8240
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | LOCK |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,TURBINE ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |