Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-443-2108 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: 23055554, 23008864, 2840-01-443-2108, 01-443-2108, 2840014432108, 014432108
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 03, 1997 | 01-443-2108 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-2108
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23055554 | 63005 | ROLLS-ROYCE CORPORATION |
| 23008864 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-443-2108
| 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 | COATED WITH IVADIZED ALUMINUM IAW AMS2427 AND MCDONNELL DOUGLAS PROCESS SPECIFICATION (PS) 13143 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG T56 (T.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY) |