NSN 2840-00-456-0447
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-456-0447 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 37D401329G013, 2840-00-456-0447, 00-456-0447, 2840004560447, 004560447
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 21, 1969 | 00-456-0447 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-456-0447
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37D401329G013 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-456-0447
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 18.000 INCHES NOMINAL |
| OVERALL WIDTH | 12.000 INCHES NOMINAL |
| OVERALL HEIGHT | 12.000 INCHES NOMINAL |
| SPECIAL FEATURES | FSCAP |
| CRITICALITY CODE JUSTIFICATION | AAGAV$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-J85-64 |
| END ITEM IDENTIFICATION | J-85 AIRCRAFT ENGINE |
