Original name compressor rotor, axial, turbine engine
No other part numbers with same form, fit, and function found.
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, 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 5855-00-821-7512
NSN 6105-00-043-0550
NSN 6130-00-959-2117
NSN 5965-01-210-7784
NSN 4140-01-122-9163
NSN 6240-01-373-6417
NSN 6135-01-561-5945
NSN 6320-01-607-0347
NSN 5895-01-138-4694
NSN 5920-00-820-0791
NSN 5855-00-151-3853
NSN 5996-01-272-5685