Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-444-2930 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: 1864M72P01, 2840-01-444-2930, 01-444-2930, 2840014442930, 014442930
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 02, 1997 | 01-444-2930 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-2930
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1864M72P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-2930
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | THIS ITEM HAS 2 KNIVE EDGE SEALS WHICH CUT A GROOVE INTO THE HONEYCOMB SEAL IN THE LPT TO CONTROL THE COOLING AIR FOR THE AFT FACE OF THE HPT DISK |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F11-GE129 |