Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-200-5347 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: 9531M23P05, 2840-01-200-5347, 01-200-5347, 2840012005347, 012005347
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 05, 1985 | 01-200-5347 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-200-5347
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9531M23P05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-200-5347
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 3.011 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 |