Original name hub, compressor rotor, turbine engine
A component of a rotor, compressor, aircraft gas turbine engine. it is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a shaft, turbine, aircraft gas turbine engine. it may have provisions for installing bearings, and/or oil and air seals. see also disk and hub, compressor, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5925-01-050-8410
NSN 2925-00-233-5644
NSN 5895-00-199-4964
NSN 6150-01-250-2772
NSN 5915-01-485-0222
NSN 5999-01-175-8730
NSN 6110-00-393-1212
NSN 5905-01-108-5140
NSN 6130-01-271-5653
NSN 6320-01-088-1109
NSN 5990-01-037-1704
NSN 5998-01-346-3229