Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-00-927-5766 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: 114020025, 1-140-200-25, 114020022, 1-140-200-22, 114020014, 1-140-200-14, 2840-00-927-5766, 00-927-5766, 2840009275766, 009275766
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 15, 1966 | 00-927-5766 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-927-5766
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-140-200-25 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-140-200-22 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-140-200-14 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-927-5766
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 62 BLADES,13.139 IN. MIN,13.141 IN. MAX OD |