Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-452-0524 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: 6078T11P05, 6078T11, 2840-01-452-0524, 01-452-0524, 2840014520524, 014520524
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 13, 1998 | 01-452-0524 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-452-0524
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6078T11P05 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 6078T11 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-452-0524
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 2.603 INCHES NOMINAL |
| SPECIAL FEATURES | DOVETAIL BLADE ATTACHMENT METHOD;MAKE FROM CASTING P/N 6078T10P02; DCN INTRODUCES 97-066, COMMERCIAL STG 1 AND 2 HPT TURBINE BLADES AND ASSOCIATED BAFFLES AS SETS TO THE ENGINE PARTS LIST; SUPERSEDES P/N 6036T94P08 |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABHP$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF34-4, FIG 15A, IND 26 |
| END ITEM IDENTIFICATION | TF34-GE-100A AIRCRAFT GAS TURBINE ENGINE |