Turbine Parts for PG9171E

 Turbine combustion chamber liners GE code: 117E3639G055/G056 - 14 pcs.;

- Primary nozzles of the turbine combustion chamber GE code: 116Е1640G020- 14 pcs.;

- Secondary nozzles of the turbine combustion chamber code according to GE: 119E1856G039 - 14 pcs.;

- Transit parts of the turbine combustion chamber GE code: 101E2571G105 - 14 pcs.;

  - A set of turbine blades 1,2,3 stages GE codes: 314B7168G013, 121E2509G004; 119E9603P001, respectively, one set of each stage;

- A set of turbine nozzle vanes 1,2,3 stages GE codes: 109E3736G017, 119E2064G042, 112E6651G007, respectively, one set of each stage;

- Set of shroud seals 1,2,3 steps, GE codes: 109B4316G008, 329A3247G006; 329A3248G004 one set of each stage;

- A set of bushings for the support bearing GT No. 1,2,3 codes for GE: 193D2284G001, 112E1523G001; 112E1293G001, respectively, one set;

Thrust bearing shell set GT No. 1 code under GE: 287A1162P001 one set.