Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-370-9805 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: 408221001, 4082210-01, 408221001, 4082210-01, 408221001, 4082210-01, 407931001, 4079310-01, 2840-01-370-9805, 01-370-9805, 2840013709805, 013709805
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 04, 1993 | 01-370-9805 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-370-9805
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082210-01 | 1645F | HANWHA TECHWIN CO.,LTDDIV PS BUSINESS UNIT |
| 4082210-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4082210-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079310-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-370-9805
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 10 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.671 INCHES NOMINAL |
| OVERALL WIDTH | 0.843 INCHES MINIMUM AND 0.851 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE CORE |