Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-318-7549 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: 407561102, 4075611-02, 2840-01-318-7549, 01-318-7549, 2840013187549, 013187549
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 25, 1990 | 01-318-7549 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-7549
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4075611-02 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-318-7549
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 11 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.528 INCHES NOMINAL |
| OVERALL WIDTH | 0.914 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/CORE MOD |