A、 You can get the corrected velocity by dividing the aircraft velocity by the crosswind component.
B、 Divide the crosswind component by the aircraft speed to get the correction.
C、 Divide the aircraft speed by the crosswind component to get the correction.
答案:B
A、 You can get the corrected velocity by dividing the aircraft velocity by the crosswind component.
B、 Divide the crosswind component by the aircraft speed to get the correction.
C、 Divide the aircraft speed by the crosswind component to get the correction.
答案:B
A. 人工超控起动顺序。
B. 按手册重写起动顺序。
C. 手动覆盖起动序列。
A. 使用听筒侧面的按钮来调节音量。
B. 使用手机旁边的按键来适应体积。
C. 为了加大容量,使用手机侧面的旋钮。
A. 如果产品的简单性允许,制造商也可以选择将相关系统进行组合。
B. 当产品允许简单组合,制造商还可能对其选择的相关系统进行分组。
C. 当产品可以组合在一起,制造商还可以选择对系统关联进行简要说明。
A. Completely retract the rod slowly and ensure not to touch other components.
B. Slowly protect the bar and guarantee not touching other parts.
C. Slowly extend the rod fully and make sure that it does not touch other parts.
A. If one or more blades are broken, make an entry in the engine logbook.
B. If one or more blades are in place , make an entry in the engine logbook.
C. If one or more blades are absent, make an entry in the engine logbook.
A. 你可以在检查完成后操作车辆。
B. 测试完成后可以操作机器。
C. 检查完成后可以停止车辆。
A. When you move the alternate nose wheel steering switch to the alternate position, the landing gear transfer valve moves to the alternate position. The landing gear transfer valve moves the pressure source for the landing gear retraction and the nose wheel
B. When move the alternate switch to steer the nose wheel to the alternate position, the landing gear transfer valve moves to the alternate position. The landing gear transfer valve moves the pressure source from hydraulic system A to hydraulic system B duri
C. When moving the alternate nose wheel steering switch to the alternate position, the landing gear transfer valve moves to the alternate position. The landing gear transfer valve removes the pressure source from the landing gear retraction and the nose whe
A. 本部分必须确定每个(部件的)指导更换时间,结构检查间隔以及型号合格证要求的相关结构检查程序。
B. 本部分必须确定每个强制的型号合格证要求的(部件)更换时间、结构检查间隔以及结构检查对应的检查程序。
C. 本部分必须明确型号合格证要求的每个(部件的)强制更换时间,结构检查间隔以及相应的结构检查程序。
A. 通过持续适航程序,实际上组成飞机的每个部件都涉及到某种形式的保养、检查、预防性维修、翻修、修理和/或更换活动。
B. 通过持续适航程序,组成飞机的几乎每个部件都涉及到某种形式的保护、检查、预测性维修、翻修、维修和/或更换活动。
C. 通过持续适航活动,组成飞机的每个部件基本上都涉及到某种形式的保护、检查、预测性维修、翻修、修理和/或更换活动。
A. 对于增压飞机和涡轮增压或涡轮螺旋桨飞机,应规定最大高度限制
B. 增压飞机、涡轮增压飞机或涡轮螺旋桨动力飞机,对于最高飞行高度有陈述。
C. 对于涡轮增压或涡轮螺旋桨飞机,可以提供最大高度限制。