A、 左集油箱left collector tank
B、 右集油箱right collector tank
C、 左机翼油箱left wing tank.
D、 右机翼油箱right wing tank.
答案:A
A、 左集油箱left collector tank
B、 右集油箱right collector tank
C、 左机翼油箱left wing tank.
D、 右机翼油箱right wing tank.
答案:A
A. 10
B. 15
C. 20
D. 25
A. 进气门位置 intake door position
B. EGT-排气温度 EGT-exhaust gas temperature
C. 燃油温度 fuel temperature
D. ITT-内部涡轮温度 ITT- inter turbine temperature
A. FADEC(全权数字电子发动机控制)交流发电机FADEC alternator
B. 液压泵(EDP 1 或 EDP 2) Hydraulic pump
C. 燃油控制组件Fuel control Unit
D. 以上全部All of above
A. 方向舵脚蹬和操纵盘Rudder pedals and control wheel
B. 横滚选择电门Roll SEL switchlight
C. 横滚脱开手柄Roll DISC handle
D. 俯仰脱开手柄PITCH DISC handle
A. 针对选定的故障,在降落后30秒关闭APU Shutdown the APU 30 seconds after landing for selected faults
B. 针对所有检测到的故障,关闭LCV Close the LCV for all detected faults
C. 针对选定的故障,在着陆后60秒关闭APU Shutdown the APU 60 seconds after landing for selected faults
D. 针对所有检测到的故障立即关闭APUShutdown immediately for all detected faults
A. 机身前顶部;the forward top of the fuselage
B. 机身前机腹;the forward belly of the fuselage
C. 机身后顶部;the backward top of the fuselage
D. 垂直安定面两侧;bothside of the vertical stabilizer
A. 两个湿翼设计燃油箱和一个集油箱用耐油密封条密封 two wet wing design fuel tanks and one collector tank sealed with fuel resistant sealant
B. 两个湿翼设计燃油箱和可选的用于拓展航程的翼尖油箱two wet wing design tanks with optional wing tip tanks for extended ranges
C. 三个整体式燃油箱位于机翼和中央机身机翼箱型结构内three integral-type fuel tanks located in the wings and center fuselage wing box structure
D. 四个燃油箱其中两个是湿翼设计油箱两个是集油箱four fuel tanks of which two are wet wing designed tanks and two are collector tanks
A. 37,000ft
B. 41,000ft
C. 25,000ft
D. 21,000ft
A. GPWS语音告警 GPWS voice alerts
B. TCAS语音告警 TCAS voice alerts
C. 高音响告警度Altitude aural alerts
D. 以上全部All of the above