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 5835-01-319-4636
NSN 5998-00-538-0690
NSN 5920-00-924-7348
NSN 6645-01-231-9891
NSN 5855-01-392-3734
NSN 5996-00-978-0408
NSN 2925-01-565-6410
NSN 5998-01-607-6721
NSN 6610-01-423-5889
NSN 5998-01-104-4783
NSN 5835-00-484-1529
NSN 7035-01-146-7096