Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-212-4060 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: P106P41, P106P21, P106P09, P106P41, P106P21, 2840-01-212-4060, 01-212-4060, 2840012124060, 012124060
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 11, 1985 | 01-212-4060 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-212-4060
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P106P41 | 58828 | CFM INTERNATIONAL, INC. |
| P106P21 | 58828 | CFM INTERNATIONAL, INC. |
| P106P09 | 58828 | CFM INTERNATIONAL, INC. |
| P106P41 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P106P21 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-212-4060
| 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 |