Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-191-1896 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 9531M22P03, 9531M22P02, 9531M22, 2840-01-191-1896, 01-191-1896, 2840011911896, 011911896
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 06, 1984 | 01-191-1896 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-191-1896
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9531M22P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9531M22P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9531M22 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-191-1896
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 7.284 INCHES MINIMUM AND 7.294 INCHES MAXIMUM |
| OVERALL WIDTH | 2.810 INCHES MINIMUM AND 2.814 INCHES MAXIMUM |
| SPECIAL FEATURES | REWORK AND REIDENTIFY TO P/N 9531M22P04 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-110-4 |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,STAGE 2 |