NSN 2840-00-821-6301
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-821-6301 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: 711515, 464215, 753015, 2840-00-821-6301, 00-821-6301, 2840008216301, 008216301
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-821-6301 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-821-6301
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 711515 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 464215 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 753015 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-821-6301
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 2.084 INCHES MINIMUM AND 2.093 INCHES MAXIMUM |
| OVERALL WIDTH | 0.972 INCHES MINIMUM AND 0.982 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 | CZBJ |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |