Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-481-0833 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: 110136007, 1-101-360-07, 2840-01-481-0833, 01-481-0833, 2840014810833, 014810833
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 16, 2000 | 01-481-0833 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-481-0833
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-101-360-07 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-481-0833
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | FORM, FIT AND FUNCTION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | AH-1, UH-1, OV-1 TURBINE ENGINE |