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 5985-01-592-3035
NSN 5950-01-202-1340
NSN 5990-01-101-7602
NSN 5905-01-311-9213
NSN 6320-01-305-5881
NSN 5950-00-138-9701
NSN 5996-01-446-8198
NSN 5915-00-193-6850
NSN 5990-01-159-5988
NSN 6110-01-170-4263
NSN 6650-00-544-5497
NSN 6685-00-815-0305