Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-397-4774 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: 9687M80G37, 9687M80G37, 2840-01-397-4774, 01-397-4774, 2840013974774, 013974774
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 12, 1994 | 01-397-4774 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-397-4774
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9687M80G37 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9687M80G37 | T0545 | TEI TUSAS MOTOR SAN.A.S. |
Technical Data | NSN 2840-01-397-4774
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 18.372 INCHES MINIMUM AND 18.390 INCHES MAXIMUM |
| DIAMETER | 23.400 INCHES NOMINAL |
| SPECIAL FEATURES | MATL IS MADE FROM A NEW TRIPLE MELT INCONEL ALLOY; INVOLUTE SPLINE DATA: NO. OF TEETH 65; PITCH 10; PRESSURE ANGLE 14 DEG. 30 MIN. |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |