Special Features:

1st stage gas producer turbine rotor assembly; includes disc p/n 1-103-035-01 and retaining ring 1-103-120-01; from honeywell service bulletin engines and systems t53-l-13b-0113 page 5, jan 25/01 revision 1, july 26/01 authorisation date 05.06.08; illustrated parts breakdown nzap 6112.002-4 fig 30 page 150 sep 30/08 assembly item number 210

Properties:

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.