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 6320-01-532-7491
NSN 6650-01-265-2672
NSN 5950-01-067-5893
NSN 4140-00-879-0862
NSN 5920-00-940-2912
NSN 6135-01-461-2915
NSN 2925-01-115-0306
NSN 5990-00-754-2842
NSN 2925-01-514-6301
NSN 6240-01-352-0882
NSN 5960-01-560-8461
NSN 6105-01-069-2911