Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-109-8529 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: 9658M56P03, 2840-00-109-8529, 00-109-8529, 2840001098529, 001098529
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 02, 1968 | 00-109-8529 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-109-8529
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9658M56P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-109-8529
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.837 INCHES MINIMUM AND 6.857 INCHES MAXIMUM |
| OVERALL WIDTH | 2.461 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |