NSN 2840-00-076-4208
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-00-076-4208 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 701092, 576753, 2840-00-076-4208, 00-076-4208, 2840000764208, 000764208
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-076-4208 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-076-4208
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701092 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
| 576753 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
Technical Data | NSN 2840-00-076-4208
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 7.152 INCHES NOMINAL |
| DIAMETER | 13.582 INCHES MINIMUM AND 13.587 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J69 |