Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-00-110-8019 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: 638E259P6, 2840-00-110-8019, 00-110-8019, 2840001108019, 001108019
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 09, 1968 | 00-110-8019 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-110-8019
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 638E259P6 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-110-8019
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 4.843 INCHES MINIMUM AND 4.845 INCHES MAXIMUM |
| DIAMETER | 8.461 INCHES MINIMUM AND 8.469 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHAFT STUB, COMPRESSOR ROTOR, FRONT |