Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-318-4798 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: 407561304, 4075613-04, 2840-01-318-4798, 01-318-4798, 2840013184798, 013184798
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 19, 1990 | 01-318-4798 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-4798
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4075613-04 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-318-4798
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 13 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.269 INCHES NOMINAL |
| OVERALL WIDTH | 0.726 INCHES NOMINAL |
| SPECIAL FEATURES | USE ONLY ON P/N 4079598-06, -07, -09 AND 4080302-02, -04 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/CORE MOD |