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ON THE RECORD

机译：记录下来

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摘要

During the supervised solo flight, the student pilot had completed three previous circuits in the traffic pattern, with two of the three landing attempts aborted. On the fourth landing attempt, a 70-degree right crosswind "blew" the airplane off the left side of the runway. The student pilot then applied full engine power to conduct a go-around, and the airplane "veered left and banked 45 degrees to the left." The student pilot stated that the airplane continued left "no matter how hard I pushed the control stick to the right." The student pilot also reported that there were no. mechanical deficiencies with the airplane that would have prevented normal operation. According to FAA Advisory Circular AC-61-23C, Pilot's Handbook of Aeronautical Knowledge: "The effect of torque increases in direct proportion to engine power, airspeed, and airplane attitude. If the power setting is high, the airspeed slow, and the angle of attack high, the effect of torque is greater. During takeoffs and climbs, when the effect of torque is most pronounced, the pilot must apply sufficient right rudder pressure to counteract the left-turning tendency and maintain a straight takeoff path."
机译：在有监督的单人飞行中，学生飞行员已按照交通模式完成了之前的三个巡回赛，其中三次着陆尝试中的两次中止。在第四次着陆尝试中，一架70度右旋风将飞机吹离跑道左侧。然后，学生飞行员施加全部发动机动力进行复飞，飞机“向左转弯并向左倾斜45度”。学生飞行员说，飞机“无论我将操纵杆向右推得多么努力，都继续向左行驶”。学生飞行员还报告说没有。飞机的机械缺陷会阻止正常运行。根据美国联邦航空局（FAA）咨询通告AC-61-23C，《飞行员航空知识手册》：“扭矩的影响与发动机功率，空速和飞机姿态成正比增加。如果功率设置高，则空速变慢，并且角度在起飞和爬升过程中，当扭矩影响最明显时，飞行员必须施加足够的右舵压力来抵消左转趋势并保持直线起飞路径。”

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    《Flying》 |2014年第11期|42-42|共1页
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