Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-212-4059 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: P106P40, P106P20, P106P08, P106P40, P106P20, P106P08, 2840-01-212-4059, 01-212-4059, 2840012124059, 012124059
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 11, 1985 | 01-212-4059 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-212-4059
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P106P40 | 58828 | CFM INTERNATIONAL, INC. |
| P106P20 | 58828 | CFM INTERNATIONAL, INC. |
| P106P08 | 58828 | CFM INTERNATIONAL, INC. |
| P106P40 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P106P20 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P106P08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-212-4059
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 6 |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |