本SAE航空航天推荐规程（ARP）旨在为验证飞机车轮/轮胎组件充气压力密封系统的完整性提供指导。只有当由轮胎、车轮、充气阀、过压释放装置、压力监测系统、阀盖、仪表、保险丝塞、O形圈、密封压盖和这些部件之间的接口/边界组成的整个密封系统成功地包含轮胎充气气体时，飞机机轮/轮胎组件才能保持充气完整性。当使用未经验证的新设计概念时，本文件将用作密封系统验证指南。它还可用于评估替代设计方法、材料变更和故障排除服务问题。 密封系统的设计和验证测试的需要由车轮制造商以及认可的车轮设计和配置控制器自行决定。本文件无意成为新的资格/认证标准。

This SAE Aerospace Recommended Practice (ARP) is intended to provide guidance on verifying the integrity of inflation pressure sealing systems of aircraft wheel/tire assemblies.Aircraft wheel/tire assemblies can maintain inflation integrity only if the entire sealing system, consisting of the tire, wheel, inflation valve, over pressure relief devices, pressure monitoring systems, valve caps, gauges, fuse plugs, O-rings, seal glands and interfaces/boundaries between these components, successfully contains the tire inflation gas.This document is to be used as a guide for sealing system validation when new design concepts not proven in service are being employed. It may also be used for evaluating alternate design approaches, material changes and trouble shooting service problems. The design of the sealing system and the need for verification testing are left to the discretion of the wheel manufacturer, and the cognizant wheel design and configuration controller.This document is not intended to be a new qualification/certification standard.