NSN 2840-00-005-6755
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-005-6755 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: 701304, 2840-00-005-6755, 00-005-6755, 2840000056755, 000056755
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 19, 1972 | 00-005-6755 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-005-6755
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701304 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-005-6755
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 2.039 INCHES MINIMUM AND 2.302 INCHES MAXIMUM |
| DIAMETER | 19.825 INCHES MINIMUM AND 19.835 INCHES MAXIMUM |
| SPECIAL FEATURES | 7.995-8.005 IN. ID.; 51 BLADE SLOTS EQ SP AROUND OD; 16 0.420 IN. DIA HOLES EQ SP ON 8.000 IN. CENTERLINE RAD.; 16 0.437-0.440 IN. DIA HOLES EQ SP ON 8.000 IN. CENTERLINE RAD. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |