Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-031-8758 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: 110088012, 1-100-880-12, 2840-01-031-8758, 01-031-8758, 2840010318758, 010318758
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 02, 1976 | 01-031-8758 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-031-8758
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-100-880-12 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-031-8758
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 66 BLADES,11.686 IN. MIN,11.689 IN. MAX OD. FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | T-53 SERIES ENGINES |