Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-451-0692 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: 4085003, 2840-01-451-0692, 01-451-0692, 2840014510692, 014510692
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 04, 1997 | 01-451-0692 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-451-0692
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4085003 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-451-0692
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| SPECIAL FEATURES | ECP95NA047; INCREASED DISK LUG THICKNESS, REVISED SLOT RADII AND BLADE SHROUDS; REPLACES P/N 4059503; 3000 TAC |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AAGAV$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-14, FIG 139, IND 51 |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |