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 7035-01-106-3476
NSN 6620-01-131-9620
NSN 5960-01-438-0245
NSN 5985-00-179-4449
NSN 6145-01-595-9139
NSN 5996-01-398-4755
NSN 5985-01-556-4421
NSN 7035-01-383-6549
NSN 5895-00-081-7836
NSN 5950-01-396-3072
NSN 5910-01-599-9338
NSN 5930-00-246-5599