Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-368-3958 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: 408221202, 4082212-02, 408221202, 4082212-02, 408221202, 4082212-02, 407941202, 4079412-02, 2840-01-368-3958, 01-368-3958, 2840013683958, 013683958
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 01, 1992 | 01-368-3958 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-368-3958
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082212-02 | 1645F | HANWHA TECHWIN CO.,LTDDIV PS BUSINESS UNIT |
| 4082212-02 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4082212-02 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079412-02 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-368-3958
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 12 |
| OVERALL LENGTH | 1.471 INCHES NOMINAL |
| OVERALL WIDTH | 0.803 INCHES MINIMUM AND 0.811 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |