Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-007-5442 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: 111R304P01, 111R304P01, 111R304P01, 111R304P01, 2840-01-007-5442, 01-007-5442, 2840010075442, 010075442
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 05, 1975 | 01-007-5442 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-007-5442
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R304P01 | 3204A | BLADES TECHNOLOGY LTD |
| 111R304P01 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 111R304P01 | 1WZW9 | BLUE AEROSPACE LLC |
| 111R304P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-007-5442
| 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 | 0.668 INCHES MINIMUM AND 0.683 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J79 ENGINE |