Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-00-883-6001 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: 674942, 2840-00-883-6001, 00-883-6001, 2840008836001, 008836001
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 05, 1972 | 00-883-6001 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-883-6001
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 674942 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-883-6001
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1038 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 15 |
| MATERIAL THICKNESS | 0.046 INCHES MINIMUM AND 0.051 INCHES MAXIMUM |
| OVERALL WIDTH | 0.040 INCHES MINIMUM AND 0.050 INCHES MAXIMUM |
| OVERALL LENGTH | 0.760 INCHES MINIMUM AND 0.770 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | 2J-J57-14 |
| SPECIAL FEATURES | GOES ON THE REAR-ROTOR COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J57 ACFT ENGINE |