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 5996-00-757-7742
NSN 5999-00-415-1766
NSN 5835-00-021-5913
NSN 5935-01-416-7352
NSN 6145-00-144-0918
NSN 6320-01-125-3361
NSN 5935-01-170-0501
NSN 5915-01-592-3355
NSN 5960-00-987-1897
NSN 5935-01-473-7554
NSN 4140-01-122-4050
NSN 6610-01-323-7045