1.1 本规程提供了一种可接受的方法，以满足小型正常类别1级和2级飞机飞行设计载荷和条件的适航要求。该材料是通过通用航空领域国际专家的公开协商制定的。这些信息是通过关注普通类飞机而创建的。内容可能适用范围更广；申请人有责任证明更广泛的适用性作为一种具体的遵守手段。本规程涵盖的主题包括:简化设计荷载标准、控制面荷载计算的可接受方法、主控制系统荷载计算的可用方法和控制面荷载（一级飞机）。 1.2 本规程适用于正常类别、低速、1级和2级飞机。除非另有说明，本规范中使用的术语“飞机”将指“正常类别、低速、1级或2级飞机”。 1.3 打算提出这些信息作为设计批准合规性手段的申请人必须向其各自的监督机构寻求有关其可接受用途和应用的指导（例如，适用CAA发布的指导）。有关监督机构已接受本标准（全部或部分）作为符合其监管要求的可接受手段（以下简称“规则”）的信息，请参阅ASTM委员会F44网页（www。 astm.org/COMMITTEE/F44.htm）。 1.4 本文件可能以国际单位制、英语工程单位或两者兼有的形式提供信息。每个系统中规定的值不一定是完全相等的；因此，为了确保符合标准，每个系统应独立使用，并且两个系统的值不得组合。 1.5 本标准并非旨在解决与其使用相关的所有安全问题（如有）。本标准的使用者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。 1.6 本国际标准是根据世界贸易组织技术性贸易壁垒委员会发布的《关于制定国际标准、指南和建议的原则的决定》中确立的国际公认的标准化原则制定的。 ===意义和用途====== 4.1 该实践提供了一种用于确定飞行、控制表面和控制系统的飞机结构载荷的方法。本规程满足规范中规定的简化荷载要求 F3116/F3116米 适用于普通类别飞机。

1.1 This practice provides an acceptable means of meeting the airworthiness requirements for the flight design loads and conditions of small normal category level 1 and 2 aeroplanes. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this practice are: Simplified Design Load Criteria, Acceptable Methods for Control Surface Loads Calculations, Acceptable Methods for Primary Control System Loads Calculations, and Control Surface Loading (Level 1 Aeroplanes). 1.2 This practice is applicable to normal category, low-speed, level 1 and 2 aeroplanes. Use of the term aeroplane used throughout this practice will mean “normal category, low-speed, level 1 or 2 aeroplane,” unless otherwise stated. 1.3 An applicant intending to propose this information as means of compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable means of compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.4 This document may present information in either SI units, English Engineering units, or both. The values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined. 1.5 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. 1.6 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 This practice provides one means for determining the aeroplane structural loads for flight, control surfaces, and control systems. This practice satisfies the simplified loads requirements set forth in Specification F3116/F3116M for Normal Category Aeroplanes.