NSN 2840-00-779-3970
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-00-779-3970 An item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals.
Alternate Parts: 210123801, 2-101-238-01, 2840-00-779-3970, 00-779-3970, 2840007793970, 007793970
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 15, 1968 | 00-779-3970 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-779-3970
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-101-238-01 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-779-3970
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 23.709 INCHES NOMINAL |
| SPECIAL FEATURES | FIRST END OD THD; 2.5625 IN.-16NS 3A THD; 0.286 IN. NOM THD LG; SECOND END OD THD; 3.2812 IN.-16NS 3A THD; 0.39 IN. NOM THD LG; 3.0937 IN.-12NS 3A THD ON OD 2.123 MIN 2.127 MAX IN. FROM FIRST END; EXTERNAL SPLINES ON OD; 65 SPLINES; 30 DEG PRESSURE ANGLE; 2.7083 IN. NOM PITCH DIA; 0.576 MIN 0.588 MAX IN. LG SPLINES; 0.762 MIN 0.774 MAX IN. FROM FIRST END TO SPLINES; 79 SPLINES; 30 DEG PRESSURE ANGLE; 3.2917 IN. NOM PITCH DIA; 0.58 MIN 0.66 MAX IN. LG SPLINES; 2.846 MIN 2.89 MAX IN. FROM SECOND END TO SPLINES; 106 SPLINES; 30 DEG PRESSURE ANGLE; 3.3125 IN. NOM PITCH DIA; 0.081 MIN 0.085 MAX IN. LG SPLINES; 0.36 MIN 0.37 MAX IN. FROM SECOND END TO SPLINES |