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 5985-00-982-6242
NSN 6650-00-527-7451
NSN 5985-00-563-0883
NSN 5998-01-015-5042
NSN 5975-01-499-9148
NSN 6105-01-214-4554
NSN 5935-00-806-3269
NSN 5999-01-506-5731
NSN 6135-01-336-3115
NSN 6685-00-534-9056
NSN 5855-00-791-5000
NSN 6620-01-498-4780