Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-125-3841 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: 6897060, 6897060, 6897060, 2840-01-125-3841, 01-125-3841, 2840011253841, 011253841
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 26, 1982 | 01-125-3841 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-125-3841
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6897060 | 73342 | ALLISON TRANSMISSION, INC. |
| 6897060 | 3V257 | HOWMET CORPORATIONDIV HOWMET MACHINING |
| 6897060 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-125-3841
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 11.343 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.158 INCHES MINIMUM AND 0.184 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF 41 |