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 6645-01-596-6077
NSN 6150-01-456-5912
NSN 6145-01-602-9331
NSN 5835-01-328-6626
NSN 5975-01-362-4177
NSN 6145-00-506-4989
NSN 5990-00-424-8872
NSN 2925-00-656-3224
NSN 6150-01-422-4686
NSN 6110-01-220-1660
NSN 6620-01-213-8772
NSN 5999-01-445-5668