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 5965-00-261-8086
NSN 6150-00-220-9382
NSN 7035-00-283-3112
NSN 5855-00-916-2236
NSN 5960-00-297-7099
NSN 6650-01-516-3631
NSN 6645-00-451-6462
NSN 5990-01-493-4039
NSN 5975-01-645-4974
NSN 5945-01-470-0691
NSN 6110-01-239-9319
NSN 5920-01-150-1706