Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-966-5067 An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 785208, 474808, 2840-00-966-5067, 00-966-5067, 2840009665067, 009665067
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-966-5067 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-966-5067
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 785208 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 474808 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-966-5067
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 8 |
| SPECIAL FEATURES | T.O. 2J-TF33-53-1, SWP 019 06 PROVIDES IMPROVED REPAIR DURABILITY FEATURING SHOTPEENING OF SPACER MATING AND OUTER WEB SURFACES AND COATING CONTACT AREAS WITH PWA 474 ANTIGALLANT COMPOUNT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 6, IND 42 |
| END ITEM IDENTIFICATION | TF33-P-3/5/7A/9 AIRCRAFT GAS TURBINE ENGINES |