Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-183-0135 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: P104P45, P104P41, P104P09, P104P45, P104P41, P104P09, 2840-01-183-0135, 01-183-0135, 2840011830135, 011830135
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 01, 1984 | 01-183-0135 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-183-0135
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P104P45 | 58828 | CFM INTERNATIONAL, INC. |
| P104P41 | 58828 | CFM INTERNATIONAL, INC. |
| P104P09 | 58828 | CFM INTERNATIONAL, INC. |
| P104P45 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P104P41 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P104P09 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-183-0135
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 4 |
| BLADE ATTACHMENT METHOD | LOCK |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |