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 4140-00-435-0436
NSN 5930-00-702-5536
NSN 5996-01-471-9519
NSN 5998-01-449-0882
NSN 6145-00-728-4026
NSN 5950-00-655-1416
NSN 6150-01-096-2400
NSN 5945-00-729-1358
NSN 5985-00-072-7177
NSN 5930-01-171-4943
NSN 5920-00-192-1723
NSN 5905-00-164-8000