Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-298-4534 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 214114038, 2-141-140-38, 2840-01-298-4534, 01-298-4534, 2840012984534, 012984534
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 16, 1989 | 01-298-4534 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-298-4534
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-141-140-38 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-298-4534
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MATERIAL METAL; O/L 19.04; SHIM TO OBTAIN MIN DIA 0.003 IN. MAX DIA 0.006 IN., FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | 2840-01-030-4890 |