Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-00-006-5309 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: 701604, 2840-00-006-5309, 00-006-5309, 2840000065309, 000065309
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JUL 16, 1972 | 00-006-5309 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-006-5309
Part Number | Cage Code | Manufacturer |
---|---|---|
701604 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-006-5309
Characteristic | Specifications |
---|---|
DESIGN TYPE | AXIAL COMPRESSOR |
ENGINE SECTION LOCATION | COMPRESSOR |
SPECIAL FEATURES | STEEL,AMS 6415,ROCKWELL C35-40 HARDNESS,2.028-2.039 IN. THK,19.825-19.835 IN. OD,7.995-8.005 IN. ID,51 BLADE SLOTS EQUALLY SPACEDAROUND OD,SIXTEEN 0.4205-0.4235 IN. HOLES EQUALLY SPACED ON 9.000 IN.CENTERLINE RADIUS,SIXTEEN 0.437-0.440 IN. HOLES EQUALLY SPACED ON 9.000IN.CENTERLINE RADIUS |
FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |