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 5998-01-449-8809
NSN 5975-00-965-9217
NSN 6645-01-368-1508
NSN 6620-01-415-5803
NSN 6145-00-495-7391
NSN 5925-01-421-4473
NSN 5990-00-015-3907
NSN 5996-01-025-5683
NSN 5925-01-406-8605
NSN 6135-00-152-8729
NSN 5965-01-202-1007
NSN 5999-00-264-4970