A、 Turn the knob clockwise to decrease the intensity of the light.
B、 Turn the knob counterclockwise to decrease the Intensity of the light.
C、 In order to turn the knob clockwise, decrease the intensity of the light.
答案：B
A、 Turn the knob clockwise to decrease the intensity of the light.
B、 Turn the knob counterclockwise to decrease the Intensity of the light.
C、 In order to turn the knob clockwise, decrease the intensity of the light.
答案：B
A. 飞机燃油系统从中央或主油箱提供增压的燃油。
B. 飞机燃油供应系统给来自中央或主油箱的燃油增压
C. 飞机燃油系统提供燃油,这些燃油是从中央或主油箱增压的。
A. 发行人栏目,出版物名称,飞机型号和发行或修订日期都应该出现在活页文件页面中。
B. 制造商的刊头,出版物标,飞机型号和发行或修订日期必须出现在活页文件的所有页面。
C. 生产商发行人栏目,出版物名称,飞机类型和发布或修订日期都应该出现在活页文件所有页面中。
A. Only when the engine is at idle speed and has active communication with the flight cabin, can you enter and exit the corridor.
B. Only when the engine is running at idle speed and you have good contact with the cockpit, can you enter the access corridor.
C. Enter/exit the corridor only when the engine is at idle state and in good contact with the cabin.
A. 轮毂
B. 轮轴
C. 轮胎
A. With the aid of the component manufacturer, all components in this chapter can be overhauled in any workshops with different qualifications.
B. Without the data supplied by the component manufacturer, it is possible for the most qualified shop to overhaul any components included in this chapter.
C. You must overhaul any or all components in this chapter in an eligible shop on the basis of data provided by the component manufacturer.
A. Maneuvering Speed is the maximum speed what required of full uncommitted aerodynamic control will not exceed the airplane.
B. Maneuvering Speed is the largest speed that the aerodynamic application by the full available control will not cause the aircraft overexert.
C. Maneuvering Speed is the maximum speed at which application of full available aerodynamic control will not overstress the airplane.
A. 如果逐字包含此类数据,则将使用飞机制造商的标头将数据识别为部件制造商的数据,如第7.1.4节所述。
B. 如果逐字包含此类数据,则将使用该制造商的标头将数据识别为部件制造商的数据,如第7.1.4节所述。
C. 如果包含此类数据,则将使用该制造商的标头将数据识别为部件制造商的数据,如第7.1.4节所述。
A. The fuselage is a semi-monocoque structure
B. The fuselage is a demi-plate.
C. The airframe is of half-shell structure.
A. Troubleshoot the VHF Communication system per FIM
B. Do the troubleshooting procedure on the VHF navigation system.
C. Do the fault isolation procedure for the ADIRU system.
A. That portion of the system that automatically controls the position of the lever to properly blend power plant with slat position and aircraft pitch attitude during landing/approach and go around procedures. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices such as amplifiers, computers, servos, limit switches, clutches, gear boxes, warning lights, etc.
B. That portion of the system that automatically controls the position of the throttles to properly mix engine power with flap position and aircraft pitch altitude during landing/approach and takeoff procedures. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices such as amplifiers, computers, servos, limit switches, clutches, gear boxes, warning lights, etc.
C. That portion of the system that automatically controls the position of the throttles to properly blend engine power with flap position and aircraft pitch attitude during landing/approach and go around procedures. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices such as amplifiers, computers, servos, limit switches, clutches, gear boxes, warning lights, etc.
