Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-006-5305 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: 701708, 2840-00-006-5305, 00-006-5305, 2840000065305, 000065305
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 16, 1972 | 00-006-5305 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-006-5305
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701708 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-006-5305
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 1.482 INCHES MINIMUM AND 1.493 INCHES MAXIMUM |
| DIAMETER | 19.825 INCHES MINIMUM AND 19.835 INCHES MAXIMUM |
| SPECIAL FEATURES | 10.995-11.005 IN. ID.;101 BLADE S LOTS EQ SP AROUND OD; 16 0.420-0.423 HOLES EQ SP ON 8.000 IN. C/L RAD.;16 0.433-0.440 IN. HOLES EQ SP ON 8.000 IN. C/L RAD. |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |