Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-511-0612 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: 1863M32P02101, 1863M32P02-101, 1863M32P01101, 1863M32P01-101, 2840-01-511-0612, 01-511-0612, 2840015110612, 015110612
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 31, 2003 | 01-511-0612 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-511-0612
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1863M32P02-101 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1863M32P01-101 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-511-0612
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 10.371 INCHES MINIMUM AND 10.381 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F101-4 FIG 56 IND 3 |
| END ITEM IDENTIFICATION | F101 ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHAFT,FWD HPT ROTOR |