Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-212-4051 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: P104P42, P104P38, P104P06, P104P42, P104P38, P104P06, 2840-01-212-4051, 01-212-4051, 2840012124051, 012124051
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 11, 1985 | 01-212-4051 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-212-4051
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P104P42 | 58828 | CFM INTERNATIONAL, INC. |
| P104P38 | 58828 | CFM INTERNATIONAL, INC. |
| P104P06 | 58828 | CFM INTERNATIONAL, INC. |
| P104P42 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P104P38 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P104P06 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-212-4051
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 4 |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |