Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-475-3392 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: 9940M50P03110B, 9940M50P03-110B, 2840-01-475-3392, 01-475-3392, 2840014753392, 014753392
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 31, 2000 | 01-475-3392 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-475-3392
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9940M50P03-110B | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-475-3392
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| OVERALL LENGTH | 11.714 INCHES MINIMUM AND 11.724 INCHES MAXIMUM |
| SPECIAL FEATURES | FRONT END STEPPED FROM 5.008 IN MIN AND 5.009 IN MAX O.D. SPLINED TEETH4.538 IN MIN AND 4.548 IN MAX I.D. AND5.2707 IN MIN AND 5.2712 IN MAX O.D.SECOND END 15.914 IN MIN 14.917 IN MAX.OD.SIX HOLES 0.262 IN MIN 0.269 IN MAX,DIA. 60 HOLES 0.251 IN MIN 0.252 IN MAX. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100-100B 2J-F100-4 |