本SAE航空航天标准（AS）建立了振动和传递性试验程序，比较了各种环式和鞍式支撑夹具的相对强度。本程序旨在进行疲劳试验，这是整个航空航天行业的标准，从而建立可用于评估过程的夹具强度比较。本文件要求的测试确保夹具仅满足足够的疲劳要求。这并不意味着夹具安装技术的合格性，也不意味着其满足以下要求的能力:- 服务环境或操作条件。应进行单独的鉴定测试，以确保所安装夹具的使用符合要求。

This SAE Aerospace Standard (AS) establishes vibration and transmissibility test procedures which compare the relative strengths of various loop and saddle type support clamps.This procedure is intended for conducting fatigue testing which is standard throughout the aerospace industry thereby establishing a clamp strength comparison that can be used in an evaluation process.The testing required by this document ensures that clamps will meet adequate fatigue requirements only. It does not infer qualification of the clamp installation techniques or its ability to meet in-service environments or operating conditions. Separate qualifications testing should be performed to ensure satisfactory service of the installed clamp.