Standard Specification for Structures for Light Sport Category Aircraft
1.1 This specification covers minimum requirements for primary aircraft structures critical to the safety of flight and is applicable to aircraft capable of wing-borne flight, semi-thrust-borne flight, thrust-borne flight or autorotation-borne flight. Specifically, this version of the specification is focused on airplanes, helicopters, gyroplanes, gliders and powered lift types. Many of the requirements specified likely apply to other aircraft types as well, but the applicability to other types shall be assessed on a case-by-case basis.
Note 1: The subcommittee is actively developing this specification so that future versions apply to a wider range of aircraft types and capabilities.
1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.
1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
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