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 2925-01-550-0177
NSN 5930-01-617-6193
NSN 5855-01-508-1707
NSN 5920-00-391-6252
NSN 5835-01-398-3859
NSN 4140-01-400-3610
NSN 5950-00-678-0238
NSN 6685-00-856-4109
NSN 6645-01-487-2052
NSN 6620-01-369-4627
NSN 5985-01-576-9593
NSN 5998-01-392-3335