NSN 2840-00-883-6002
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-00-883-6002 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: 674943, 674943, 2840-00-883-6002, 00-883-6002, 2840008836002, 008836002
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 05, 1972 | 00-883-6002 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-883-6002
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 674943 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 674943 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-883-6002
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1038 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 16 |
| MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.025 INCHES MAXIMUM |
| OVERALL WIDTH | 0.342 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
| OVERALL LENGTH | 0.710 INCHES MINIMUM AND 0.720 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J57-14; GOES ON THE ROTOR-REAR COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-57 AIRCRAFT ENGINE |