Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-519-2631 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: 2411M21G012A, 2411M21G01-2A, 1589M66G032A, 1589M66G03-2A, 1589M66G022A, 1589M66G02-2A, 2840-01-519-2631, 01-519-2631, 2840015192631, 015192631
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 12, 2004 | 01-519-2631 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-519-2631
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2411M21G01-2A | 58828 | CFM INTERNATIONAL, INC. |
| 1589M66G03-2A | 58828 | CFM INTERNATIONAL, INC. |
| 1589M66G02-2A | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 2840-01-519-2631
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL-CENTRIFUGAL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | LIFE LIMITED PART |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O.2J-F108-14 FIG 72-31-00-1 IND140D |
| END ITEM IDENTIFICATION | CFM56 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SPOOL-STAGE 1AND 2 |