Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-443-4087 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: 4084503, 2840-01-443-4087, 01-443-4087, 2840014434087, 014434087
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 09, 1997 | 01-443-4087 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-4087
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084503 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-443-4087
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 0.796 INCHES NOMINAL |
| OVERALL HEIGHT | 5.077 INCHES MINIMUM AND 5.089 INCHES MAXIMUM |
| SPECIAL FEATURES | SURFACE TREATMENT PWA 694 COBALT ALLOY; IT TAKES OF THESE TO MAKE UP BLADE SET P/N 4084283 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AABKW$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |