Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-187-8723 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: 111019214, 1-110-192-14, 2840-01-187-8723, 01-187-8723, 2840011878723, 011878723
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 27, 1984 | 01-187-8723 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-187-8723
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-110-192-14 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-187-8723
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | AN ITEM THAT IS DESIGNED TO RECEIVE THE LATENT ENERGY OF COMBUSTION GAS. THE ITEM CONSISTS OF A DISK OR DISKS |
| END ITEM IDENTIFICATION | UH-1 SERIES TURBINE ENGINES |