Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-423-8133 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: 4081506, 2840-01-423-8133, 01-423-8133, 2840014238133, 014238133
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 11, 1996 | 01-423-8133 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-423-8133
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4081506 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-423-8133
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 6 |
| OVERALL LENGTH | 2.919 INCHES MINIMUM AND 2.929 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AFEAT$$AAGAV |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |