Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-010-4048 An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6841212, 6829932, 6841212, 6829932, 6841212, 6829932, 2840-00-010-4048, 00-010-4048, 2840000104048, 000104048
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-010-4048 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-010-4048
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6841212 | 73342 | ALLISON TRANSMISSION, INC. |
| 6829932 | 73342 | ALLISON TRANSMISSION, INC. |
| 6841212 | 24617 | GENERAL MOTORS CORP |
| 6829932 | 24617 | GENERAL MOTORS CORP |
| 6841212 | 63005 | ROLLS-ROYCE CORPORATION |
| 6829932 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-010-4048
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 2.534 INCHES MINIMUM AND 2.538 INCHES MAXIMUM |
| DIAMETER | 8.861 INCHES MINIMUM AND 8.871 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY |
| CRITICALITY CODE JUSTIFICATION | CZCJ |
| END ITEM IDENTIFICATION | T56 ENG |