Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-475-2851 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: 8141674, 814167-4, 814167, 2840-01-475-2851, 01-475-2851, 2840014752851, 014752851
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 30, 2000 | 01-475-2851 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-475-2851
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 814167-4 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
| 814167 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
Technical Data | NSN 2840-01-475-2851
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 3.740 INCHES NOMINAL |
| OVERALL WIDTH | 1.887 INCHES NOMINAL |
| SPECIFICATION/STANDARD DATA | MIL-L-9047 GOVERNMENT SPECIFICATION |
| END ITEM IDENTIFICATION | GOES ON AIR CONDITIONING SYSTEM ASSEMBLIES INSTALLED IN THE BOEING F/A-18 E/F MODEL AIRCRAFT-AIR CIRCLE MACHINE |