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 6685-01-229-9844
NSN 5835-00-995-0277
NSN 5960-00-407-1728
NSN 6240-01-608-1030
NSN 6610-01-151-1540
NSN 6645-01-603-6716
NSN 6130-01-369-4970
NSN 5935-01-396-2033
NSN 6620-00-842-9224
NSN 5999-01-272-4285
NSN 6110-01-565-1293
NSN 6240-00-489-8531