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(Markings for the Hydraulic Ground Connection)

A、 气源地面接口标识

B、 液压地面接口标识

C、 气源地面接口污滓

D、 液压地面接口污滓

答案:B

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The exact content of the Normal Procedures Section shall be determined by the applicable regulations of the certificating authority and by the operating and design features of each particular airplane.
https://www.shititong.cn/cha-kan/shiti/00017884-808f-d11c-c0a6-5ac6b1259100.html
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(Airflows between Mach 0.8 and Mach 1.5)
https://www.shititong.cn/cha-kan/shiti/00017884-808f-121f-c0a6-5ac6b1259100.html
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troubleshooting
https://www.shititong.cn/cha-kan/shiti/00017884-808e-67cc-c0a6-5ac6b1259100.html
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When you select the attitude mode, the ALIGN light comes on for 30 seconds. During this time, the ADIRU calibrates to 0 degrees in pitch and roll.
https://www.shititong.cn/cha-kan/shiti/00017884-8090-3ac7-c0a6-5ac6b1259100.html
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float
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The fuel dump system is used to dump fuel overboard during flight. It includes items such as plumbing, valves, chutes, controls, etc.
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Do external walk around check, check static ports for no damage and obstruction, check radome latches and angle of attack sensors for no damage.
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The main frame of the fuselage includes frames, bulkheads, longerons, stringers, keel, frames around openings, etc.
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(Shoring) is necessary to give a support to the wing in order to release the loads on the structure when you do major work or modifications.
https://www.shititong.cn/cha-kan/shiti/00017884-808f-325e-c0a6-5ac6b1259100.html
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Climb gradient is the demonstrated ratio of the change in height during a portion of a climb, to the horizontal distance traversed in the same time interval.
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(Markings for the Hydraulic Ground Connection)

A、 气源地面接口标识

B、 液压地面接口标识

C、 气源地面接口污滓

D、 液压地面接口污滓

答案:B

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相关题目
The exact content of the Normal Procedures Section shall be determined by the applicable regulations of the certificating authority and by the operating and design features of each particular airplane.

A. 正常程序部分的具体内容应根据认证机构的适用规定以及每架飞机的操作和设计特点确定。

B. 正常程序部分的具体内容应根据监管机构的有效规定以及每架飞机的操作和设计特点确定。

C. 正常程序部分的具体内容应根据认证机构的强制规定以及每架飞机的操作和设计特点确定。

https://www.shititong.cn/cha-kan/shiti/00017884-808f-d11c-c0a6-5ac6b1259100.html
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(Airflows between Mach 0.8 and Mach 1.5)

A. Hypersonic flow

B. Subsonic flow

C. Transonic flow

D. Supersonic flow

解析:这道题考察的是空气流速的范围,介于马赫数0.8和1.5之间。根据马赫数的定义,当空气流速等于音速时,为马赫数1,小于音速为亚音速,大于音速为超音速。因此,当空气流速介于亚音速和超音速之间时,我们称之为跨音速流动。

举个生动的例子来帮助理解:想象一下一架飞机正在加速飞行,当它的速度接近音速时,空气流动的情况就会发生变化,从亚音速到超音速的过渡阶段就是跨音速流动。在这个阶段,飞机会遇到一些特殊的气动性能问题,需要特殊设计来应对这种复杂的流动情况。

因此,答案是C: Transonic flow(跨音速流动)。

https://www.shititong.cn/cha-kan/shiti/00017884-808f-121f-c0a6-5ac6b1259100.html
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troubleshooting

A. 射击

B. 故障

C. 排故

D. 阻尼

https://www.shititong.cn/cha-kan/shiti/00017884-808e-67cc-c0a6-5ac6b1259100.html
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When you select the attitude mode, the ALIGN light comes on for 30 seconds. During this time, the ADIRU calibrates to 0 degrees in pitch and roll.

A. 选择高度模式时,ALIGN灯亮30秒。在此期间,ADIRU的俯仰和滚转计算为0度。

B. 选择姿态模式30秒后,ALIGN灯亮。在此期间,ADIRU的俯仰和滚转校准为0度。

C. 选择姿态模式时,ALIGN灯亮30秒。在此期间,ADIRU的俯仰和滚转校准为0度。

https://www.shititong.cn/cha-kan/shiti/00017884-8090-3ac7-c0a6-5ac6b1259100.html
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float

A. 飞行

B. 地板

C. 浮子

D. 簧片

https://www.shititong.cn/cha-kan/shiti/00017884-808e-ddab-c0a6-5ac6b1259100.html
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The fuel dump system is used to dump fuel overboard during flight. It includes items such as plumbing, valves, chutes, controls, etc.

A. 放油系统用于在飞行过程中向机外排放燃油,包括管道、活门、滑道、控制器等。

B. 放油系统用于在飞行过程中向机外排放燃油,包括接头、活门、滑道、控制器等。

C. 加油系统用于在飞行过程中为飞机紧急加油,包括管道、活门、滑道、控制器等。

https://www.shititong.cn/cha-kan/shiti/00017884-8090-53e1-c0a6-5ac6b1259100.html
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Do external walk around check, check static ports for no damage and obstruction, check radome latches and angle of attack sensors for no damage.

A. 执行绕机检查,清除静压孔的损坏和堵塞,检查整流罩锁和迎角传感器没有损坏。

B. 执行绕机检查,确保静压孔没有损坏和堵塞,检查雷达罩锁和迎角传感器没有损坏。

C. 执行目视检查,确保静压孔没有损坏和堵塞,检查雷达罩锁和迎角传感器没有损坏。

https://www.shititong.cn/cha-kan/shiti/00017884-808f-616d-c0a6-5ac6b1259100.html
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The main frame of the fuselage includes frames, bulkheads, longerons, stringers, keel, frames around openings, etc.

A. 机身主框架包括隔框、蒙皮、横梁、桁梁、龙骨、开口周围的隔框等。

B. 机身主框架包括隔框、特殊隔框、长梁、桁梁、龙骨、开口周围的隔框等。

C. 机身主框架包括隔框、特殊隔框、翼肋、桁梁、龙骨、开口周围的隔框等。

https://www.shititong.cn/cha-kan/shiti/00017884-808f-c2a4-c0a6-5ac6b1259100.html
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(Shoring) is necessary to give a support to the wing in order to release the loads on the structure when you do major work or modifications.

A. 顶升

B. 支撑

C. 系留

D. 拖曳

https://www.shititong.cn/cha-kan/shiti/00017884-808f-325e-c0a6-5ac6b1259100.html
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Climb gradient is the demonstrated ratio of the change in height during a portion of a climb, to the horizontal distance traversed in the same time interval.

A. 爬升梯度是指爬升过程中高度变化与同一时间内所通过的水平距离之比。

B. 爬升角度是指爬升过程中高度变化与同一时间内所通过的水平距离之比。

C. 爬升梯度是指爬升过程中,高度的变化与同一时间内所通过的水平距离成正比。

https://www.shititong.cn/cha-kan/shiti/00017884-8090-4600-c0a6-5ac6b1259100.html
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