1.1 以下要求适用于包括滑翔机在内的固定翼飞机的制造。本规程包括生产验收测试要求。 1.2 本惯例适用于以飞行证书、飞行许可证或其他类似文件的形式寻求民航局批准的飞机。 1.3 本标准并非旨在解决与其使用相关的所有安全问题（如有）。本标准的用户有责任在使用前制定适当的安全、健康和环境实践，并确定监管限制的适用性。 1.4 本国际标准是根据世界贸易组织技术性贸易壁垒（TBT）委员会发布的《关于制定国际标准、指南和建议的原则的决定》中确立的国际公认标准化原则制定的。 ====意义和用途====== 4.1 本规程旨在为轻型运动飞机制造商制定生产验收计划提供最低要求。 4.2 本规范的目的是提供建立地面和飞行测试计划的最低要求，以验证初始生产的飞机符合制造商在其飞行员操作手册（POH）中规定的某些操作性能要求。 4.3 此外，本规范提供了最低要求，以验证每架后续生产的飞机是否没有会妨碍飞机安全运行的明显缺陷。 4.4 本规范中给出的所有要求均应按照制造商规范执行 F2972 -符合质量保证体系要求。 4.5 以下标准不应解释为LSA中包含的特定功能的要求。 当需求指定LSA上不存在的功能时，该需求不适用。

1.1 The following requirements apply for the manufacture of fixed wing aircraft, including gliders. This practice includes the production acceptance test requirements. 1.2 This practice applies to aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. 1.3 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. 1.4 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. ====== Significance And Use ====== 4.1 The purpose of this practice is to provide the minimum requirements necessary for the establishment of a production acceptance program for a manufacturer of light sport aircraft. 4.2 The purpose of this specification is to provide the minimum requirements for the establishment of a ground and flight test program for verifying the initial production aircraft meets certain operational performance requirements that have been set forth by the manufacturer in its Pilot’s Operating Handbook (POH). 4.3 In addition, this specification provides minimum requirements to verify that each subsequent production airplane has no obvious defects that would prevent the safe operation of the airplane. 4.4 All requirements given in this specification are to be performed in accordance with the manufacturer’s Specification F2972 -compliant quality assurance system requirements. 4.5 The following criteria should not be construed as requirements for specific features to be included on a LSA. When a requirement specifies a feature that does not exist on a LSA, the requirement does not apply.