Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-064-8521 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: 6895382, 6895382, 2840-01-064-8521, 01-064-8521, 2840010648521, 010648521
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 02, 1978 | 01-064-8521 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-064-8521
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6895382 | 73342 | ALLISON TRANSMISSION, INC. |
| 6895382 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-064-8521
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 7.030 INCHES MINIMUM AND 7.040 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF41 ENG |