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.
答案:B
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.
答案:B
A. 8,000 ft
B. 8,500 ft
C. 10,000 ft
D. 14,000ft
A. 不行,目测值只能用于替代能见度
B. 可以,接地区的RVR可以由驾驶员目测估算
C. 机长可视实际情况自行决断
A. 30
B. 15
C. 25
D. 35
A. 一旦出现35节机轮转动信号或机轮承重信号在5秒延迟后显示。Once a 35 knot wheel spin-up signal is present or a WOW signal after a 5 second delay.
B. 接地时。 At touchdown.
C. 一旦机轮承重信号在15秒延迟后显示。 Once a WOW signal is present after a 15 second delay.
D. 一旦出现25节机轮转动信号。Once a 25 knot wheel spin-up signal is present.
A. FMS, GPS, LOC
B. LOC, VOR, FMS
C. GPS, LOC, VOR
D. GPS, FMS, VOR/DME
A. 16.6
B. 11.6
C. 7.6
D. 没有APU危险区域。There is no APU danger area
A. "150 米,1000 百帕(750 毫米水银柱)
B. 100 米,1000 百帕(750 毫米水银柱)
C. 100 米,1013 百帕(760 毫米水银柱)"
A. 1
B. 2
C. 3
D. 4
A. 在 APU 舱内探测到火警或超温。Fire or overheat detected in APU enclosure.
B. APU 转速超过 106%。 APU RPM >106%.
C. APU 排气温度超过自动停车限制值。APU EGT over temperature shutdown limit exceeded.
A. FQGC的一个通道处于激活状态 one channel of the FQGC is active.
B. FQGC持续地进行通电自测 the FQGC continuously preforms a built-in test
C. FQGC的一号通道计算燃油重量和密度,二号通道计算燃油温度 channel one of the FQGC calculates fuel weight and density and channel two calculates fuel temperature.
D. FQGC使燃油转移实现自动化the FQGC enables fuel transfer to be automatic