NSN 2840-00-890-2768
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-890-2768 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: 212109015, 2-121-090-15, 2840-00-890-2768, 00-890-2768, 2840008902768, 008902768
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 05, 1968 | 00-890-2768 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-890-2768
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-121-090-15 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-890-2768
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 80 BLADES,14.505 IN. MIN,14.507 IN. MAX TIP DIA |
| END ITEM IDENTIFICATION | ENG T-55 |