Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-005-6753 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: 701802, 2840-00-005-6753, 00-005-6753, 2840000056753, 000056753
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 19, 1972 | 00-005-6753 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-005-6753
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701802 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-005-6753
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 2.882 INCHES MINIMUM AND 2.893 INCHES MAXIMUM |
| DIAMETER | 19.825 INCHES MINIMUM AND 19.835 INCHES MAXIMUM |
| SPECIAL FEATURES | 6.995-7.005 IN ID.; 28 BLADE SLOTS EQ SP AROUND OD,16 0.420-0.423 IN. DIA. HOLES EQ SP ON 8.0000 IN CENTERLINE RAD.; 16 0.437-0.440 IN. DIA. HOLES EQ SP ON 8.000 CENTERLINE RAD. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J57 |