Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-008-8800 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: 111R303P01, 111R303P01, 111R303P01, 111R303P01, 111R303P01, 111R303P01, 111R303P01, 2840-01-008-8800, 01-008-8800, 2840010088800, 010088800
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 31, 1975 | 01-008-8800 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-008-8800
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R303P01 | 3204A | BLADES TECHNOLOGY LTD |
| 111R303P01 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 111R303P01 | 1WZW9 | BLUE AEROSPACE LLC |
| 111R303P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R303P01 | 3V257 | HOWMET CORPORATIONDIV HOWMET MACHINING |
| 111R303P01 | 99160 | THERM, INCORPORATED |
| 111R303P01 | 58556 | WALBAR INC.DIV TURBOMACHINERY PRODUCTS |
Technical Data | NSN 2840-01-008-8800
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 5.850 INCHES MINIMUM AND 5.868 INCHES MAXIMUM |
| OVERALL WIDTH | 1.530 INCHES MINIMUM AND 1.570 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.661 INCHES MINIMUM AND 0.676 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J79 ENGINE |