Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-308-6139 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: 4070292, 2840-01-308-6139, 01-308-6139, 2840013086139, 013086139
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 01, 1989 | 01-308-6139 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-308-6139
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4070292 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-308-6139
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 14/15; 72 UNITS PER ASSY; 2 OF THE BLADES MAKE UP P/N 4080342; USED ON THE REAR COMPRESSOR DRIVE TURBINE ROTOR |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE SET,COMPRESSOR,ACFT GAS TURBINE ENGINE |