NSN 2840-00-906-5303
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-906-5303 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: 37D401329G007, 37D401329G007, 2840-00-906-5303, 00-906-5303, 2840009065303, 009065303
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-906-5303 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-906-5303
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37D401329G007 | 24446 | GENERAL ELECTRIC COMPANY |
| 37D401329G007 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-906-5303
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AAGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-J85-64 |
| END ITEM IDENTIFICATION | J-85 AIRCRAFT ENGINE |
| FSC APPLICATION DATA | C-135 AIRCRAFT SERIES |