Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-349-5758 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: 30970312, 3097031-2, 2840-01-349-5758, 01-349-5758, 2840013495758, 013495758
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 29, 1991 | 01-349-5758 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-349-5758
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3097031-2 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-349-5758
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | FAN |
| OVERALL LENGTH | 11.450 INCHES MINIMUM AND 11.500 INCHES MAXIMUM |
| OVERALL WIDTH | 3.380 INCHES MINIMUM AND 3.520 INCHES MAXIMUM |
| SPECIAL FEATURES | Y-SHAPED END WIDTH 6.540-6.550; DIA. OF CENTER THRU SHAFT HOLE 1.660-1.690 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | PACER DAWN |