No other part numbers with same form, fit, and function found.
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 7035-01-044-0136
NSN 6620-01-065-8265
NSN 2925-01-581-3273
NSN 6685-01-495-5692
NSN 5835-00-461-3342
NSN 6150-01-575-3209
NSN 5975-00-794-8769
NSN 6150-01-437-8666
NSN 6685-00-759-9801
NSN 5985-00-581-2820
NSN 5925-00-845-3168
NSN 6685-01-548-9274