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 6130-01-574-2837
NSN 5920-01-370-5521
NSN 6620-00-838-6954
NSN 5930-01-400-6126
NSN 6130-00-778-4442
NSN 5895-01-122-3108
NSN 6685-00-740-7256
NSN 6105-00-900-4143
NSN 6650-00-754-2276
NSN 5965-00-652-5661
NSN 5935-01-066-9504
NSN 6240-00-372-4841