T.O. 2j-f107-14, fig 14, index 2; used on the 3rd stage turbine nozzle
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 5930-01-447-7516
NSN 5975-01-293-5742
NSN 5950-01-479-6595
NSN 6620-01-417-3314
NSN 5965-01-501-5638
NSN 5985-00-652-1631
NSN 5985-01-013-6209
NSN 2925-01-442-7812
NSN 6145-01-196-5211
NSN 5975-00-893-5443
NSN 6105-01-197-7081
NSN 5935-01-418-5354