NSN 2840-00-005-6777
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-00-005-6777 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: 702609, 740809, 702609, 2840-00-005-6777, 00-005-6777, 2840000056777, 000056777
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 19, 1972 | 00-005-6777 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-005-6777
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 702609 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 740809 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 702609 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-005-6777
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | STEEL,AMS 6415,ROCKWELL C35-40 HARDNESS,1.354-1.365 IN. THK,20.017-20.027 IN. OD,11.995-12.005 IN. ID,103 BLADE SLOTS EQUALLYSPACED AROUND OD,SIXTEEN 0.437-0.440 IN. HOLES EQUALLY SPACED ON 8.000IN. CENTERLINE RADIUS,32 SCALLOPS EQUALLY SPACED ON 7.260 IN.CENTERLINE RADIUS,THIRTY-TWO 0.108-0.113 IN. HOLES EQUALLY SPACED ON7.260 IN. CENTERLINE RADIUS |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |
