A、 3
B、 6
C、 12
D、 24
答案:B
A、 3
B、 6
C、 12
D、 24
答案:B
A. 外侧多功能扰流板、起落架、外侧刹车 Outboard multifunction spoiler panels、landing gear、Outboard brakes
B. 外侧刹车、升降舵、内侧多功能扰流板Outboard brakes、elevators、Inboard multifunction spoiler panels
C. 右发反推、外侧多功能扰流板、外侧地面扰流板 Right thrust reverser、Outboard multifunction spoiler panels、Outboard ground spoilers
D. 方向舵、前轮转弯、起落架 Rudder、nosewheel steering、landing gear
A. 风速
B. 气压
C. 气温
A. 状态页和环控简图页 status and ECS synoptic pages
B. 只有环控简图页 ECS synoptic page only
C. 状态页和主页 status and primary pages
D. 主页和环控简图页 primary and ECS synoptic pages
A. 外流活门关闭、地面活门打开 the outflow valve closed、ground valve open
B. 外流活门打开、地面活门打开 the outflow valve open、ground valve open
C. 外流活门打开、地面活门关闭 the outflow valve open、ground valve closed
D. 外流活门关闭、地面活门关闭 the outflow valve closed、ground valve closed
A. 人工模式下,不正确的引气构型(包括APU)。(APU LCV 打开,发动机引气关闭)。人工选择APU作为引气源时,任意一个机翼或整流罩防冰电门选择接通。 Incorrect bleed configuration (including APU) when in manual mode. (APU LCV open, engine bleeds closed).APU is manually selected as the bleed source and either wing or cowl anti-ice switches selected on.
B. 隔离活门失效在开位或关位。 Isolation valve failed open or closed.
C. 引气泄露后引气关闭且系统未选择关闭。Bleed shutdown after bleed leak and system not selected off.
D. 在通电自检测试中(PBIT),左引气管路的漏气双探测环路失效。 Loss of both leak detection loops in left bleed ducting during PBIT.
A. 机轮不承重的同时Simultaneously with weight off wheels
B. 飞机通电时CVR开始记录,信标灯接通,或频闪灯接通或机轮不承重FDR开始记录。CVR with electrical power applied to aircraft and the FDR: beacon ON, or strobe ON, or WOW
C. 两个都是在遭遇撞击,减速和/或失去电源时。Both upon impact, deceleration and or loss of electrical power
D. 飞机通电的同时。Simultaneously with electrical power supplied to aircraft
A. 4m
B. 5m
C. 7m
D. 10m
A. 30秒30 sec
B. 60秒60 sec
C. 90秒90 sec
D. 120秒120 sec
A. 机长captain
B. 副驾驶co-pilot
C. PF
D. 观察员 observer
A. 失速、风切变、地形 stall, wind shear, and terrain
B. 失速、地形、风切变stall,terrain and wind shear
C. 地形、风切变、失速terrain, wind shear and stall
D. 风切变、失速、地形wind shear, stall and terrain