Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-005-6766 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: 701415, 2840-00-005-6766, 00-005-6766, 2840000056766, 000056766
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 19, 1972 | 00-005-6766 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-005-6766
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701415 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-005-6766
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 0.971 INCHES MINIMUM AND 0.982 INCHES MAXIMUM |
| DIAMETER | 23.491 INCHES MINIMUM AND 23.501 INCHES MAXIMUM |
| SPECIAL FEATURES | 5.995-6.005 IN. ID; 16 0.437-0.440 IN. HOLES EQ SP ON 9.000 IN. CENTERLINE RAD.; 16 0.498-0.501 IN. HOLES EQ SP ON 9.000 IN. CENTERLINE RAD. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |