Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-443-3613 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: 4088604, 4084804, 2840-01-443-3613, 01-443-3613, 2840014433613, 014433613
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 09, 1997 | 01-443-3613 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-3613
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4088604 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084804 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-443-3613
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 4 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.809 INCHES NOMINAL |
| OVERALL WIDTH | 0.832 INCHES NOMINAL |
| DIAMETER | 14.497 INCHES MINIMUM AND 14.697 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 130, IND 9; REPLACES P/N 4067004; TAKES 2 OF THIS ITEM TO MAKE UP BLADE SET P/N 4084194 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AABMZ$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |