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Standards Development
This document applies to the design and production of eVTOL aircraft used for passenger-carrying, cargo, inspection, etc., and have a maximum take-off weight of more than 150 kg and less than 5,7 tons.
It specifies the product-level safety design requirements for the eVTOL aircraft itself, including its system and functions, airframe strength, electric propulsion system, and design and construction, but does not cover the entire UAS system; therefore, it neither specifies how to obtain type certification nor operational approval.
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