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 5895-01-379-8611
NSN 6145-01-417-2988
NSN 5950-00-364-8162
NSN 5895-00-967-1933
NSN 6220-00-371-7589
NSN 5855-01-570-8816
NSN 5996-00-995-3222
NSN 6620-01-037-4631
NSN 6150-01-562-0495
NSN 6130-01-476-6865
NSN 5920-00-369-0923
NSN 6130-01-448-8713