本试验程序适用于将接收器飞机燃料箱连接到加油源燃料泵的加油歧管系统，用于地面和空中加油。本试验程序旨在验证从符合AS1284（参考文献2）要求的加油源加油时，不超过接收器燃油系统规定的喘振压力限值。本推荐规程不直接适用于飞机燃油系统运行期间产生的喘振压力，如启动或停止飞机内的发动机燃油供给或燃油输送，或当燃油泵首次启动以填充空的燃油歧管时产生的压力喘振。

The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value for surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.