Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-374-0730 An item used to maintain the position of a BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 408078702, 4080787-02, 408078702, 4080787-02, 2840-01-374-0730, 01-374-0730, 2840013740730, 013740730
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 14, 1993 | 01-374-0730 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-374-0730
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4080787-02 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4080787-02 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-374-0730
| Characteristic | Specifications |
|---|---|
| STAGE NUMBER | 9 |
| REFERENCE DATA AND LITERATURE | 2J-F100-54 |
| SPECIAL FEATURES | GOES ON THE AXIAL COMPRESSOR ROTOR; 2 UNITS PER ASSEMBLY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT ENGINE,CORE |