Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-192-0855 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: 9531M23P04, 9531M23P02, 9531M23, 2840-01-192-0855, 01-192-0855, 2840011920855, 011920855
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 16, 1984 | 01-192-0855 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-192-0855
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9531M23P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9531M23P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9531M23 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-192-0855
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 5.547 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| REFERENCE DATA AND LITERATURE | T.O. 2J-110-4 |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,FAN ROTOR-STG 3 |