Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-011-0678 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: 6841214, 6841214, 6841214, 2840-00-011-0678, 00-011-0678, 2840000110678, 000110678
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-011-0678 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-011-0678
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6841214 | 73342 | ALLISON TRANSMISSION, INC. |
| 6841214 | 24617 | GENERAL MOTORS CORP |
| 6841214 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-011-0678
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 4 |
| OVERALL LENGTH | 2.494 INCHES MINIMUM AND 2.498 INCHES MAXIMUM |
| DIAMETER | 10.361 INCHES MINIMUM AND 10.371 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY |
| CRITICALITY CODE JUSTIFICATION | CZCJ |
| END ITEM IDENTIFICATION | T56 ENG |