Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-822-4834 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: 753014, 753014, 753014, 711514, 464214, 2840-00-822-4834, 00-822-4834, 2840008224834, 008224834
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-822-4834 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-822-4834
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 753014 | 33755 | AIRFOIL TEXTRON INCSUB OF TEXTRON INC |
| 753014 | 8W315 | TURBINE ENGINE COMPONENTSTECHNOLOGIES CORPORATION |
| 753014 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 711514 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 464214 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-822-4834
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 2.269 INCHES MINIMUM AND 2.274 INCHES MAXIMUM |
| OVERALL WIDTH | 1.017 INCHES MINIMUM AND 1.027 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE MODEL J57 |