A、 If your decision is not to change the unit, monitor its temperature at least 15 rotations.
B、 If you decide not to renew the unit, supervise its temperature at least 15 periods.
C、 If your decision is not to replace the unit, monitor its temperature for a minimum of 15 cycles.
答案:C
A、 If your decision is not to change the unit, monitor its temperature at least 15 rotations.
B、 If you decide not to renew the unit, supervise its temperature at least 15 periods.
C、 If your decision is not to replace the unit, monitor its temperature for a minimum of 15 cycles.
答案:C
A. 在提供给客户的所有技术资料中,规则应保持一致。
B. 在提供给客户的所有技术数据中,文化词汇应保持一致。
C. 在提供给客户的所有技术资料中,术语应保持一致。
A. Operate the dimmer switch and make sure that the intensity of the light changes.
B. Control the light knob to ensure that the light strength changes.
C. Turn the light regulator on to adjust the luminous intensity.
A. 缠紧卷轴上的发条。
B. 将胶带缠绕在卷筒上。
C. 将胶带粘贴在线圈上。
A. 描述飞机电力转向系统时,如安装前轮电力转向,应包括以下相关信息: (a)系统 (b)如何使用 (c)限制讨论。
B. 描述飞机动力转向系统时,如安装前轮动力转向,应包括以下相关信息: (a)系统描述 (b)如何使用 (c)相关限制。
C. 描述飞机功率转向系统时,如果安装前轮功率转向,应包括以下相关信息: (a)应描述系统。 (b)应说明如何使用。 (c)应阐述限制。
A. 引擎多的飞机改出螺旋程序可由代理商分别编写。
B. 多发飞机的改出螺旋程序可由制造商选择。
C. 多台发动机的改出螺旋程序可以包含在飞机制造商的操作手册中。
A. 在此推荐清单中,更换部件对于起落架收放系统和其相关的指示系统来讲是不合理的。
B. 在此推荐清单中,起落架收放系统和适用的指示系统没有可更换的部件。
C. 此推荐清单不能用于起落架放下系统部件更换但适用于指示系统。
A. The rudder can be used in case of thrust asymmetry.
B. The vertical stabilizer can be used in case of throttle symmetry.
C. The rudder can be used in situations where thrust is symmetric.
A. Remove the caps from the hoses.
B. Remove the caps from the tubes.
C. Remove the caps from the manifolds.
A. 此时不要拆解弹簧筒组件。如果弹簧负载没有正确释放,会造成人员受伤或零件损伤。
B. 此时不要错装弹簧筒组件。不正确的操作,弹簧负载会造成人员受伤或零件损伤。
C. 不要在这个时候拆下弹簧筒组件。如果不小心释放,弹簧负载会造成人员受伤或零件损伤。
A. Necessary information by manufacturer should be provided in this chapter to maintain, overhaul or major repair the aircraft so as to properly level it during the life of the aircraft.
B. In order to properly level the aircraft when performing repair, overhaul or major repairs during the life of the aircraft, this chapter should provide all considered information by manufacturer.
C. This chapter shall provide that information considered necessary by the manufacturer to properly level the aircraft for any of the various maintenance, overhaul or major repairs which might become necessary during the life of the aircraft.