Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-323-4295 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: 407751201, 4077512-01, 2840-01-323-4295, 01-323-4295, 2840013234295, 013234295
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 27, 1990 | 01-323-4295 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-323-4295
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4077512-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-323-4295
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 12 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 1.467 INCHES NOMINAL |
| OVERALL WIDTH | 0.811 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ACFT ENGINE |