飞行操纵系统信息显示在 EICAS 主页和状态页上。＇CONFIG SPLRS＇ 警告信息指示：The flight controls system messages are shown on the EICAS primary and status pages. ＇CONFIG SPLRS＇ Warning message indicates:
A. 副翼配平不在起飞范围之内(配平＞ ±1 度) 且两台发动机 ＞70% N1。Aileron trim is outside of the takeoff range (trim ＞ ±1 degree) and both engines ＞70% N1.
B. 飞行扰流板没有收起，飞机为起飞构型。Flight spoilers are not retracted with the aircraft configured for takeoff.
C. 水平安定面配平不在起飞范围之内。Horizontal stab trim is outside of the takeoff range.
D. 停留刹车设置, 飞机为起飞构型且两台发动机＞70% N1。Parking brake is set with the aircraft configured for takeoff and both engines ＞70% N1.
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使用中国民航高低空图进行航路飞行时，航路最低安全高度是如何规定的（分别阐述沿航路或航路中心线两侧25km以内飞行、偏离航路中心线25km以外飞行）？When performing a flight by using China Civil, Aviation’s high and low altitude charts, how is the minimum safe altitude specified? (From the perspective of the flight along the route or within 25 km on both sides of the route center line or that deviating by 25 km from the route center line)
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判断正误：CONT IGNITION 状态信息（白色）表明相对应的发动机的双套点火系统都接通。True or False:CONT IGNITION status (white) Indicates that all ignitors have been selected on.
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发动机的最大额定功率为在海平面的 ISA+15°C(86°F)情况下The engine performance is flat rated at 59°F (15°C) at sea level as follows:
A. 正常起飞推力额定功率Normal take-off thrust – 13360 lb (59.43 kN)
B. 最大起飞推力（APR）额定功率Max take-off thrust (with APR) – 13360 lb (59.43 kN)
C. 最大连续推力额定功率Max continuous thrust – 13360 lb (59.43 kN)
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只要机组决定备降，可以飞抵任何一个机场降落。As long as the flight crew decides to make an alternate landing, they can fly to any airport for the landing.
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左和右风挡雨刷分别由直流汇流条1和2供电The left and right windshield wipers are supplied by DC bus 1 and 2
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判断正误True or False: 有两个扰流板安定面控制组件（SSCUs），它们可以自动控制扰流板、水平安定面配平、俯仰杆力控制和方向舵行程限制的操作。There are two spoiler stabilizer control units (SSCUs) that automatically control operation of the spoilers, horizontal stabilizer trim, pitch feel control and rudder travel limiting.
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在日常航空天气报告中，电码“VCTS”表示的意思是
A. 机场上有雨
B. 机场附近有雨，但机场上无雨
C. 机场附近有雷暴，但机场上无雷暴
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盲降进近高于下滑道时，截获航向道并建立着陆形态后，可以使用不大于（ ）尺/分钟的下降率从上方切入下滑道，场高（ ）尺（AGL）前，必须截获下滑道。如无法满足以上条件，立即执行复飞。When ILS approach is above the glideslope, after capturing localizer and establishing landing configuration, the glideslope can be intercepted from the above by using not more than 1500ft/min descent rate, the glideslope must be captured before （ ）ft AGL. If the above condition cannot be satisfied, go-around must be carried out.
A. 1500，1300
B. 1500,1000
C. 1400,1300
D. 1400,1000
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CABIN ALT座舱高度警告信息和＇CABIN PRESSURE＇（座舱压力）语音警告在座舱高度大于或等于（ ）出现。The CABIN ALT warning message and ＇CABIN PRESSURE＇ aural will be shown when the cabin altitude greater than or equal to（ ）.
A. 8,000 feet
B. 8,500 feet
C. 10,000 feet
D. 14,000 feet
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