NSN 2840-00-006-2791
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-00-006-2791 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: 701608, 701608, 2840-00-006-2791, 00-006-2791, 2840000062791, 000062791
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 23, 1972 | 00-006-2791 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-006-2791
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701608 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 701608 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-006-2791
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ROCKWELL C35-40 HARDNESS; 1.482-1.493 INCH THICKNESS; 19.825-19.835 INCH OD; 101 BLADE SLOTS EQUALLY SPACED AROUND OD; 16 0.4205-0.4235 INCH HOLES EQUALLY SPACED ON 8 INCH CENTERLINE RADIUS; 16 0.437-0.440 INCH HOLES EQUALLY SPACED ON 8.0 INCH CENTERLINE RADIUS |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |