Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-192-0856 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: 9530M95P13, 9530M95P09, 1441M54P01, 2840-01-192-0856, 01-192-0856, 2840011920856, 011920856
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 16, 1984 | 01-192-0856 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-192-0856
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9530M95P13 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9530M95P09 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1441M54P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-192-0856
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 2.767 INCHES MINIMUM AND 2.777 INCHES MAXIMUM |
| DIAMETER | 28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM |
| SPECIAL FEATURES | BLADE ATTACHMENT METHOD IS DOVETAIL |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABHP$$AABMZ |
| END ITEM IDENTIFICATION | ACFT ENG F110 |