NSN 2840-00-185-6252
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-00-185-6252 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: 701106, 2840-00-185-6252, 00-185-6252, 2840001856252, 001856252
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 10, 1971 | 00-185-6252 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-185-6252
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 701106 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-185-6252
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 1.172 INCHES MINIMUM AND 1.192 INCHES MAXIMUM |
| DIAMETER | 12.274 INCHES MINIMUM AND 12.576 INCHES MAXIMUM |
| SPECIAL FEATURES | SPECIAL FEATURES AT TAPERED OD; 2ND END OD 12.264-12.274; WAS DISK,AXIAL COMPRESSOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-60 AIRCRAFT ENGINE |
