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.
NSN: 2840-01-304-3018
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What are the manufacturers of nsn 2840013043018? |
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Does this nsn 2840013043018 have a shelf life? No. This NSN does not have an applicable shelf life. |
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What is the formal definition of nsn 2840013043018 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. |
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Does nsn 2840013043018 contain any precious metals? No precious metal content. |
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Does nsn 2840013043018 contain any hazardous materials? No MSDS. No hazardous material. |
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What is the ESD classification of nsn 2840013043018? No known electrostatic discharge. |
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