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 6620-00-383-8740
NSN 5999-00-290-5898
NSN 6240-00-393-1161
NSN 6220-01-067-8142
NSN 6220-01-081-7631
NSN 5855-01-589-7273
NSN 5975-01-492-8362
NSN 6645-00-369-4410
NSN 5996-01-409-1860
NSN 4140-01-464-4445
NSN 6220-01-204-7429
NSN 6135-00-948-7061