Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-267-7689 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: P111P16, P111P10, P111P16, P111P10, 2840-01-267-7689, 01-267-7689, 2840012677689, 012677689
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 18, 1987 | 01-267-7689 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-267-7689
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P111P16 | 58828 | CFM INTERNATIONAL, INC. |
| P111P10 | 58828 | CFM INTERNATIONAL, INC. |
| P111P16 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P111P10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-267-7689
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. F108 |