NSN 2840-00-006-5308
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-00-006-5308 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: 754901, 701701, 2840-00-006-5308, 00-006-5308, 2840000065308, 000065308
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 16, 1972 | 00-006-5308 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-006-5308
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 754901 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 701701 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-006-5308
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | STEEL,AMS 6415,ROCKWELL C35-40 HARDNESS,3.210-3.221 IN. THK,19.825-19.835 IN. OD,6.995-7.005 IN. ID,27 BLADE SLOTS EQUALLY SPACEDAROUND OD,SIXTEEN 0.437-0.440 IN. HOLES EQUALLY SPACED ON 8.000 IN.CENTERLINE RADIUS,THIRTY-TWO 0.101-0.113 IN. HOLES EQUALLY SPACED ON7.260 IN. CENTERLINE RADIUS,THIRTY-TWO SCALLOPS EQUALLY SPACED ON 7.260IN. CENTERLINE RADIUS |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |