Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-103-5057 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: 3017T94P04, 3017T94P04, 3017T94P04, 3017T94P04, 3017T94P04, 2840-01-103-5057, 01-103-5057, 2840011035057, 011035057
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 13, 1980 | 01-103-5057 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-103-5057
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3017T94P04 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 3017T94P04 | 08244 | MOELLER MFG. COMPANY, INC.DIV AIRCRAFT |
| 3017T94P04 | 03983 | STERLING MACHINE COMPANY, INC. |
| 3017T94P04 | 31340 | THE BIRKEN MANUFACTURING COMPANY |
| 3017T94P04 | 2M223 | WHITE ENGINEERING SURFACESCORPORATION |
Technical Data | NSN 2840-01-103-5057
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 1.465 INCHES MINIMUM AND 1.470 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85 |