Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-445-2811 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: 4085104, 2840-01-445-2811, 01-445-2811, 2840014452811, 014452811
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 28, 1997 | 01-445-2811 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-445-2811
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4085104 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-445-2811
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 4 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 6.771 INCHES MINIMUM AND 6.781 INCHES MAXIMUM |
| DIAMETER | 29.004 INCHES MINIMUM AND 29.404 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 130, IND 9; INTERIM BLADE REPLACES P/N 4067004 AND IS REPLACED BY P/N 4084804 PER ECP 95-NA027 |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$AABMZ$$AABHP$$ACZBJ |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |