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 6220-01-227-1917
NSN 6650-01-446-1160
NSN 4140-00-878-1222
NSN 6135-01-176-2206
NSN 5855-01-053-9684
NSN 6320-01-171-3238
NSN 5998-00-287-6355
NSN 5935-00-777-0511
NSN 6685-01-141-6130
NSN 5965-01-532-1198
NSN 6240-01-158-5664
NSN 5855-00-991-0096