Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-313-4567 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: 9992M60G07108, 9992M60G07-108, 2840-01-313-4567, 01-313-4567, 2840013134567, 013134567
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 09, 1990 | 01-313-4567 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-313-4567
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9992M60G07-108 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
Technical Data | NSN 2840-01-313-4567
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL-CENTRIFUGAL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 6.287 INCHES NOMINAL |
| DIAMETER | 17.200 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$AAPGF$$ACZBJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-4 FIG 72-31-00-01 IND 140B |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SPOOL COMPRESSOR ROTOR STAGES 1&2 |