NSN 2840-00-440-2129
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-440-2129 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 108R815P3, 111R112P21, 111R112P12, 108R815P3, 2840-00-440-2129, 00-440-2129, 2840004402129, 004402129
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-440-2129 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-440-2129
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 108R815P3 | 24446 | GENERAL ELECTRIC COMPANY |
| 111R112P21 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R112P12 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 108R815P3 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-440-2129
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 9 |
| BLADE ATTACHMENT METHOD | SLOT |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-47,J-79,T-58 AND T-64 AIRCRAFT ENGINE |
