NSN 2835-01-114-8612
Part Details | NONAIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2835-01-114-8612 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, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 38420134, 3842013-4, 10106415, 2835-01-114-8612, 01-114-8612, 2835011148612, 011148612
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 24, 1981 | 01-114-8612 | 50592 ( ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-114-8612
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3842013-4 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 10106415 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
Technical Data | NSN 2835-01-114-8612
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | ROTOR MATERIAL NICKEL ALLOY PER AIRESEARCH ENS 55445,IN738LC; 7.080 MIN 7.110 MAX IN. O/A DIA ROTOR; 16.78 MIN 16.84 MAX IN. O/A LG SHAFT AND ROTOR |