Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-947-7114 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 753011, 711311, 506511, 2840-00-947-7114, 00-947-7114, 2840009477114, 009477114
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 25, 1966 | 00-947-7114 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-947-7114
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 753011 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 711311 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 506511 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-947-7114
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM |
| OVERALL WIDTH | 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE MODEL J57 |