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 5975-00-480-7902
NSN 5965-01-315-5764
NSN 5925-00-549-5366
NSN 5985-01-008-3578
NSN 6620-00-072-8602
NSN 5990-00-490-5250
NSN 5975-01-607-6129
NSN 6105-01-030-9266
NSN 6645-01-055-9423
NSN 6145-01-573-5891
NSN 6145-01-483-6567
NSN 6145-00-377-0971