Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-147-2670 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: 1276M41G02, 1276M31P03, 1276M31P02, 1276M41G02, 2840-01-147-2670, 01-147-2670, 2840011472670, 011472670
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 15, 1983 | 01-147-2670 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-147-2670
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1276M41G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1276M31P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1276M31P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1276M41G02 | 8W315 | TURBINE ENGINE COMPONENTSTECHNOLOGIES CORPORATION |
Technical Data | NSN 2840-01-147-2670
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | BLADE PLUS SEAL,SOLVENT WASH WITMETHYL-ETHYL-KETONE,VAPOR BLAST TO 63-90 MICROINCH SURFACE,SILICONE BONDING PRIMER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F101 |
