Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-447-8978 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: 1359M21P02118, 1359M21P02-118, 1359M21P01118, 1359M21P01-118, 1359M20G01118, 1359M20G01-118, 1275M25P02118, 1275M25P02-118, 2840-01-447-8978, 01-447-8978, 2840014478978, 014478978
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 15, 1997 | 01-447-8978 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-8978
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1359M21P02-118 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1359M21P01-118 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1359M20G01-118 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1275M25P02-118 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-8978
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-4, FIG 58, IND 38; THIS ITEM IS TO BE USED STRICTLY ON THE F118 ENGINE |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |