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 6110-00-353-0139
NSN 6685-01-397-8694
NSN 5999-01-434-7877
NSN 7035-01-063-8753
NSN 5960-01-543-0235
NSN 6610-00-869-8685
NSN 6240-01-578-7913
NSN 5985-01-629-6048
NSN 5996-01-122-8288
NSN 6620-00-526-8996
NSN 6150-01-538-4407
NSN 6240-00-115-8575