5998-01-159-6845
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A component of a rotor, turbine, 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, turbine, aircraft gas turbine engine.
5998-01-159-6845, no name available
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