Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-134-2691 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: 23001903, 2840-01-134-2691, 01-134-2691, 2840011342691, 011342691
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 02, 1982 | 01-134-2691 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-134-2691
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23001903 | 73342 | ALLISON TRANSMISSION, INC. |
Technical Data | NSN 2840-01-134-2691
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 3.700 INCHES NOMINAL |
| SPECIAL FEATURES | ROCKWELL C SCALE 41 MIN 45 MAX CORE HARDNESS; ONE END 1.475 MIN 1.485 MAX IN. OD; 1.156 MIN 1.161 MAX IN. ID; OTHER END; 1.88 MIN 1.89 MAX IN. OD; 1.555 MIN 1.56 MAX IN. ID; INTERNAL SPLINE DATA; 38 TEETH 30 DEG PRESSURE ANGLE |