Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-00-759-6320 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: 494421, 2840-00-759-6320, 00-759-6320, 2840007596320, 007596320
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-759-6320 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-759-6320
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 494421 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-759-6320
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1038 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 15 |
| MATERIAL THICKNESS | 0.049 INCHES NOMINAL |
| OVERALL WIDTH | 0.045 INCHES NOMINAL |
| OVERALL LENGTH | 0.765 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-J57-14; GOES ON THE ROTOR-REAR COMPRESSOR |
| END ITEM IDENTIFICATION | J-57 AIRCRAFT ENG |