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 6150-01-487-5376
NSN 6645-01-468-4990
NSN 5950-00-828-6989
NSN 5835-01-529-3050
NSN 4140-01-106-2559
NSN 6105-01-587-8522
NSN 6110-01-179-7024
NSN 5920-01-468-0186
NSN 5990-00-810-9562
NSN 5835-01-286-6499
NSN 6685-01-245-8952
NSN 6130-01-418-7787