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尾吊布局的民用飞机动力装置大侧风试验,是考核发动机在装机环境下进气道与发动机之间工作兼容性的适航试验,涉及对CCAR§25.939(a)(c)、§25.1091(a)(1)、§25.903(d)(2)和§25.1309(c)条款符合性验证,通过侧风地面试验制定出发动机在装机环境下的地面侧风运行包线,由侧风下的滑跑起飞和着陆试验验证发动机装机条件下的滑跑起飞侧风范围,并在飞行手册中给出飞机侧风飞行的要求和程序。
Airworthiness test of civil aircraft power plant with tail suspension layout for airworthiness test of engine operating compatibility with engine in installed environment involves airworthiness test to CCAR §25.939 (a) (c), §25.1091 ( Compliance verification of a) (1), §25.903 (d) (2) and §25.1309 (c) shall be made by the crosswind ground test to determine the ground crosswind running envelope of the engine under installed conditions, Skid-off take-off and landing tests validate the range of the roll-off crosswind under engine loading conditions and give the requirements and procedures for the cross -wind flight of the aircraft in the flight manual.