Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-00-767-5190 An item used to maintain the position of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 364506, 364506, 364506, 364506, 2840-00-767-5190, 00-767-5190, 2840007675190, 007675190
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-767-5190 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-767-5190
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 364506 | 81753 | CONNECTICUT SPRING & STAMPINGCORPORATION THE |
| 364506 | 55694 | UNITED HYDROFORMING CO INC |
| 364506 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 364506 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-767-5190
| Characteristic | Specifications |
|---|---|
| STAGE NUMBER | 5 |
| REFERENCE DATA AND LITERATURE | 2J-TF33-4 |
| SPECIAL FEATURES | GOES ON THE COMPRESSOR ROTOR-FRONT |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |