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.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 7035-01-607-0415
NSN 5920-00-201-4914
NSN 5960-00-167-7875
NSN 7035-00-215-3272
NSN 5965-00-682-3567
NSN 6610-01-442-3509
NSN 6105-01-401-5361
NSN 5895-01-214-9145
NSN 5950-01-258-3474
NSN 5996-00-224-1987
NSN 4140-01-571-7913
NSN 6650-01-056-7508