Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-146-5691 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: P108P03, P108P03, 2840-01-146-5691, 01-146-5691, 2840011465691, 011465691
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 02, 1983 | 01-146-5691 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-146-5691
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P108P03 | 58828 | CFM INTERNATIONAL, INC. |
| P108P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-146-5691
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 8 |
| OVERALL LENGTH | 1.089 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-100,F108-CF-100,AND F110-GE-100 |