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 6650-00-701-8081
NSN 6620-01-580-4327
NSN 5835-00-196-9771
NSN 6320-00-295-2854
NSN 6105-01-035-7197
NSN 5950-01-038-6578
NSN 2925-01-484-5066
NSN 5905-01-075-9813
NSN 5998-01-444-4241
NSN 6145-00-181-9622
NSN 4140-01-552-6158
NSN 4140-00-580-8508