本文件规定了航空货物托盘、网和集装箱（通常指定为航空货物单元装载装置（ULD））适航性批准的最低要求。 本文件旨在为航空货运单元装载装置的批准提供统一的技术参考。作为先决条件，前提是遵守适用的通用民用航空要求和飞机制造商批准的重量和平衡手册。 本文件定义了需要适航性批准的航空货运单元负载装置的最低性能要求和测试参数，以安装在符合EASA CS货物约束和乘客保护要求的经批准的飞机货舱和约束系统中- 25或14 CFR第25部分，除了§25.561（b）（3）（ii）中的9,0 g向前极限惯性力。 本文件适用于根据EASA CS-25或14 CFR第25部分或同等标准认证的民用运输类飞机上的适航性批准的航空货物单元装载装置。 本文件仅适用于单元负载设备适航性批准和测试参数。它不适用于飞机设计或飞机运行要求，这些要求由批准的重量和平衡手册为每种飞机类型提供。 本文件未涵盖与航空货运单元装载设备适航性批准和测试不直接相关的其他方面，其他国际标准（见参考文献）也对这些方面进行了定义。 g、 : -ULD设计规范， -ULD在役损坏限值， -ULD约束故障限制， -ULD测试方法， -ULD负载分配模型， -ULD最大允许轮廓， -ULD CG（重心）位置控制装置， -ULD压力均衡方法， -ULD使用指南。 根据ISO 8097:2001的要求，在本文件发布之前经过鉴定的空运货物单元装载装置已获得批准。本文件旨在作为TSO批准参考，以取代ISO 8097，适用于其所涵盖尺寸和类型的所有新型单元负载装置。 对于本文件中未涉及尺寸或类型的空运货物单元装载装置，如果其尺寸或类型包含在本文件中，请参见ISO 8097:2001的要求，如果没有，请参见其他等效标准。 注1:ISO 8097基于美国国家航空航天标准NAS 3610修订版10:1990《货物单元负载装置规范》。 注2:本文件中未定义货物保护层的要求，除非其中包含净约束。

This document specifies the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices (ULD). This document is intended to provide a uniform technical reference for air cargo unit load devices approval. As a prerequisite, it is presupposed that the applicable general civil aviation requirements and the aircraft manufacturer's approved Weight and Balance Manual are followed. This document defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of EASA CS-25 or 14 CFR Part 25, except for the 9,0 g forward ultimate inertia force of § 25.561(b) (3) (ii). This document applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes type certificated under EASA CS-25 or 14 CFR Part 25, or equivalent. This document exclusively applies to unit load devices airworthiness approval and testing parameters. It does not apply to aircraft design or aircraft operating requirements, which are provided by the approved Weight and Balance Manual for each aircraft type. Other aspects that do not directly pertain to air cargo unit load devices airworthiness approval and testing are not covered by this document and are defined in other International Standards (see Bibliography), e.g.: — ULD design specifications, — ULD in service damage limits, — ULD restraint malfunction limitations, — ULD test methods, — ULD load distribution models, — ULD maximum allowable contours, — ULD CG (centre for gravity) location control means, — ULD pressure equalization methods, — ULD utilization guidelines. Air cargo unit load devices qualified prior to publication of this document were approved in accordance with the requirements of ISO 8097:2001. This document is intended as a TSO approval reference for all new models of unit load devices in the sizes and types it covers, in replacement of ISO 8097. For air cargo unit load devices the size or type of which is not covered in this document, see the requirements of ISO 8097:2001, if their size or type is contained therein, or other equivalent criteria, if not. NOTE 1 ISO 8097 is based on USA National Aerospace Standard NAS 3610 revision 10:1990, Specification for Cargo Unit Load Devices. NOTE 2 The requirements for cargo covers are not defined in this document, except insofar as net restraint is incorporated therein.