Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-084-0262 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: 6009T97P03, 2840-01-084-0262, 01-084-0262, 2840010840262, 010840262
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 06, 1979 | 01-084-0262 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-084-0262
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6009T97P03 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-084-0262
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 3.373 INCHES MINIMUM AND 3.376 INCHES MAXIMUM |
| OVERALL WIDTH | 0.744 INCHES MINIMUM AND 0.748 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J85-94 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85 |