Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-01-443-4088 An item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 408411301, 4084113-01, 2840-01-443-4088, 01-443-4088, 2840014434088, 014434088
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 09, 1997 | 01-443-4088 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-4088
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084113-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-443-4088
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 3.156 INCHES MINIMUM AND 3.166 INCHES MAXIMUM |
| DIAMETER | 17.311 INCHES NOMINAL |
| SPECIAL FEATURES | BLADE SLOTS ARE FIR TREE DESIGN |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |