Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-01-343-3768 An item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 23031176, 2840-01-343-3768, 01-343-3768, 2840013433768, 013433768
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 12, 1991 | 01-343-3768 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-343-3768
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23031176 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-343-3768
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 6 |
| OVERALL LENGTH | 11.445 INCHES NOMINAL |
| SPECIAL FEATURES | INTERNAL INVOLUTE SPLINE DATA; NO. OF TEETH 364,PITCH 32/64,PRESSURE ANGLE 30 DEGREES,BASE CIRCLE DIA. 9.851 IN.,MINOR DIA. 11.344/11.347 IN.,PITCH DIA. 11.375 IN. BASIC,FORM DIA. 11.412 IN.,MAJOR DIA. 11.433 IN. MAX.,SPLINES IN ACCORDANCE WITH ANSI B92.1,DIMENSION BTWN TWO 0.054 DIA. PINS = 11.2945/11.2980 IN.,EXTERNAL INVOLUTE SPLINE DATA; NO. OF TEETH 374,PITCH 32/64,PRESSURE ANGLE 30 DEGREES,BASE CIRCLE DIA. 10.121 IN.,MINOR DIA.11.636 IN. MIN.,PITCH DIA. 11.6875 IN. BASIC,FORM DIA. 11.652 IN.,MAJOR DIA. 11.716/11.719 IN.,SPLINES IN ACCORDANCE WITH ANSI B92.1,DIMENSION OVER TWO 0.0540 DIA. PINS = 11.7696/11.7730 IN. |
| FSC APPLICATION DATA | TURBINE COMPRESSOR ROTOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DISK,GAS TURBINE ENGINE |