Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-00-953-0874 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: 643E111P5262, 643E111P5-262, 643E111P5260, 643E111P5-260, 643E111P5258, 643E111P5-258, 643E111P5256, 643E111P5-256, 643E111P5254, 643E111P5-254, 643E111P5252, 643E111P5-252, 643E111P5250, 643E111P5-250, 643E111P5248, 643E111P5-248, 643E111P5246, 643E111P5-246, 643E111P5244, 643E111P5-244, 643E111P5242, 643E111P5-242, 643E111P5240, 643E111P5-240, 643E111P5238, 643E111P5-238, 643E111P5236, 643E111P5-236, 643E111P5234, 643E111P5-234, 643E111P5232, 643E111P5-232, 2840-00-953-0874, 00-953-0874, 2840009530874, 009530874
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-953-0874 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-953-0874
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 643E111P5-262 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-260 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-258 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-256 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-254 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-252 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-250 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-248 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-246 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-244 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-242 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-240 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-238 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-236 | 24446 | GENERAL ELECTRIC COMPANY |
| 643E111P5-234 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 643E111P5-232 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-953-0874
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,TURBINE ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J47/J73/J79/J85/J93/T58 AND T64 AIRCRAFT ENGINES |
