Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-339-6769 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: P103P12, P103P03, 2840-01-339-6769, 01-339-6769, 2840013396769, 013396769
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 28, 1991 | 01-339-6769 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-339-6769
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P103P12 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P103P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-339-6769
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.518 INCHES NOMINAL |
| OVERALL WIDTH | 1.115 INCHES MINIMUM AND 1.119 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110 AIRCRAFT ENG |