如果机长侧大气数据计算机出现故障，可通过 In case of the failure of the pilot‘s side Air Data computer （ADC）, We can:

A. 仅出现故障或非正常/不安全状况出现时会显示EICAS信息。EICAS messages appear only in case of malfunction or abnormal/unsafe condition

B. 舱门或出口的状态信息显示。Status messages for the door or exit appears

C. 舱门或出口的咨询信息显示。Advisory message for the door or exit would appear

D. 后设备舱门和应急出口不被PSEU监控，所以没有指示显示。Aft equipment bay door and emergency exits are not monitored by the PSEU, therefore no indications appear

A. 不能

B. 能

C. 由机长最终决策

A. 轻雾、微风2 米／秒

B. 风向不定、风速2 米／秒

C. 轻雾，能见度200 米

A. 逆温层

B. 等温层

C. 不稳定气层

A. 内侧防滞系统发现故障。 Fault found in the anti-skid INBD system.

B. 外侧防滞系统发现故障。 Fault found in the anti-skid OUTBD system.

C. 转弯控制组件探测到故障。 Steering control unit has detected a fault.

D. 防滞-BTMS控制组件失去裕度，可能失去接地保护。 Loss of redundancy in anti-skid - BTMS control unit with a possible loss of touch-down protection.

A. 安装在机身右侧的堵塞型舱门。A plug type door installed on the right side of the fuselage

B. 安装在机身左侧的堵塞型舱门。A plug type door installed on the left side of the fuselage

C. 安装在机身右侧地液压操作舱门。A hydraulically operated door installed on the right side of the fuselage

D. 安装在机身左侧的液压操作舱门。A hydraulically operated door installed on the left side of the fuselage

A. 打开 open

B. 关闭 closed

A. 电风扇通过热交换器从客舱引气。An electric fan draws air from the cabin across the heat exchanger

B. 冲压空气自然地流过热交换器。Ram air naturally flows across the heat exchanger

C. 电风扇从冲压空气管道引气以及通过热交换器排出。An electric fan draws air from the ram air duct and discharges it across the heat exchanger

D. 液压油不需要冷却。Hydraulic fluid does not require cooling

A. 外侧机翼区域 In the outer wing section

B. 内侧机翼区域 In the inner wing section

C. 在中央油箱 In the center tank

D. 在供油箱内 Within the feeder tanks