Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-185-9320 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: 114704200, 114704-200, 2840-01-185-9320, 01-185-9320, 2840011859320, 011859320
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 05, 1984 | 01-185-9320 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-185-9320
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114704-200 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2840-01-185-9320
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | AN ITEM THEAT IS DESIGNED TO RECEIVE THE LATENT ENERGY OF COMBUSTION GAS. THE ITEM CONSIST OF A DISK OR DISKS |
| END ITEM IDENTIFICATION | UH-60 SERIES HELICOPTER |