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2222.In the description of the airplane's Control Locks,how to engage control locks or secure control surfaces shall be explained.

A、 描述飞机控制锁时,应说明如何连接控制锁或固定操纵面。

B、 描述飞机阵风锁时,应描述如何使用阵风锁或锁住操纵面。

C、 描述飞机舵面锁时,应说明如何参与舵面锁和操纵装置的固定。

答案:A

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3048.该构型具有所有惯性和空气数据功能的三重冗余数据。
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368.The protective paint will prevent corrosion for six months.
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2790.The yaw damper works by sensing any yaw motion and then applying corrective inputs to the aircraft's rudder to reduce or eliminate any unwanted yawing.It is particularly useful in minimizing the effects of turbulence or other external disturbances that can cause yawing and make the aircraft harder to control.The yaw damper is an important safety feature that helps to improve the overall stability and control of the aircraft,especially during critical phases of flight such as takeoff and landing.
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3024.两个活门上的旋转螺母都与内部阀杆上的螺纹啮合,从而使阀杆松开或拉紧到金属阀座。
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2925.不要操作刹车来降低蓄压器中的压力。
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2536.评估所需要的数量。
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1746.The slow moving,high pressure air from the compressor is fed into the combuster where it is mixed with a highly flammable fuel and ignited.
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1889.They include the tail assembly ,the structures at the rear of the airplane that serve to control and maneuver the aircraft and structures forming part of and attached to the wing.
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100 要求的情况下将使用第 19 段格式。
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305.The system to be tested operated abnormally during last flight leg.
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2222.In the description of the airplane's Control Locks,how to engage control locks or secure control surfaces shall be explained.

A、 描述飞机控制锁时,应说明如何连接控制锁或固定操纵面。

B、 描述飞机阵风锁时,应描述如何使用阵风锁或锁住操纵面。

C、 描述飞机舵面锁时,应说明如何参与舵面锁和操纵装置的固定。

答案:A

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相关题目
3048.该构型具有所有惯性和空气数据功能的三重冗余数据。

A. This configuration has three rest data for all the inertial and air data functions.

B. This configuration has triple redundant data for all the inertial and air data functions.

C. This configuration has three rest data for all the interface and air data functions.

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368.The protective paint will prevent corrosion for six months.

A. 保护漆将防止腐蚀达 6 个月。

B. 保护涂层将防止锈蚀达 6 个月。

C. 保护漆将保护腐蚀达 6 个月。

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2790.The yaw damper works by sensing any yaw motion and then applying corrective inputs to the aircraft's rudder to reduce or eliminate any unwanted yawing.It is particularly useful in minimizing the effects of turbulence or other external disturbances that can cause yawing and make the aircraft harder to control.The yaw damper is an important safety feature that helps to improve the overall stability and control of the aircraft,especially during critical phases of flight such as takeoff and landing.

A. 偏航阻尼器通过感受偏航动作然后将正确的信号输给方向舵来减轻和消除不希望出现的偏航。它在减少尾流和其他外部干扰的影响中很有用,气流和外部干扰使飞机难以操控。偏航阻尼器也是一个改进飞机稳定性和操作性的重要安全特征尤其是在起飞和着陆等关键阶段。

B. 偏航减震器通过感受偏航动作然后将正确的信号输给方向舵来减轻和消除不希望出现的偏航。它在减少气流和其他外部干扰的影响中很有用,气流和外部干扰使飞机难以操控。偏航减震器也是一个改进飞机稳定性和操作性的重要安全装置尤其是在起飞和着陆等关键阶段。

C. 偏航阻尼器通过感受偏航动作然后将修正的信号输给方向舵来减轻和消除不希望出现的偏航。它在减少湍流和其他外部干扰的影响中很有用,气流和外部干扰使飞机难以操控。偏航阻尼器也是一个改进飞机稳定性和操作性的重要安全装置尤其是在起飞和着陆等关键阶段。

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3024.两个活门上的旋转螺母都与内部阀杆上的螺纹啮合,从而使阀杆松开或拉紧到金属阀座。

A. The swivel nuts on both valves engage threads on an internal stem that loosens or draws tight the valve stem to a metal seat.

B. The rotating nuts on both valves are meshed with the threads on the inner valve stud,so that the valve stud is loosened or tightened to a metal valve base.

C. The swing nuts on both valves engage with the threads on the internal spool,allowing the spool to loosen or tighten to the metal seat.

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2925.不要操作刹车来降低蓄压器中的压力。

A. Do not operate the brakes to decrease the pressure in the accumulators.

B. Do not control the brakes to increase the pressure in the accumulators.

C. Do not maneuver the brakes for augmentation of the pressure in the reservoir.

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2536.评估所需要的数量。

A. Make an estimate of the necessary quantity.

B. Evaluate on the quantity available.

C. Approximate the scale of the quality.

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1746.The slow moving,high pressure air from the compressor is fed into the combuster where it is mixed with a highly flammable fuel and ignited.

A. 来自压气机的高压气体进入燃烧室并缓慢移动,并与被点燃的燃料混合。

B. 来自压气机的高压气体进入燃烧室并缓慢移动,并与易燃的燃料混合并点燃。

C. 来自压气机的缓慢移动的高压气体进入燃烧室,与易燃燃料混合并点燃。

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1889.They include the tail assembly ,the structures at the rear of the airplane that serve to control and maneuver the aircraft and structures forming part of and attached to the wing.

A. They comprise the three parts as follows:tail assembly,the structures at the rear of the airplane ,structures forming part of and attached to the wing.

B. They include three parts,one of them is tail assembly,one of them is the structures part at the rear of the airplane,one of them is structures part that forming part of and attached to the wing.

C. They include two parts,one of them is tail assembly at the rear of the airplane that serve to control and maneuver the aircraft,another of them is structures part that forming part of and attached to the wing.

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100 要求的情况下将使用第 19 段格式。

A. TA-100 要求的情况下,将使用第 19 段格式。

B. 任何以 ATA No.100 格式发布的技术数据将满足本规范的要求,但在没有预见 ATA-100要求的情况下,将使用第 19 段格式。

C. 任何以 ATA No.100 格式发布的技术数据将满足本规范的要求,但在预见不需要满足

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305.The system to be tested operated abnormally during last flight leg.

A. 将要测试的这个系统在上个航段运转不正常。

B. 该系统要测试上一航段的不正常运行。

C. 在上一航段里该系统被测试为运行不正常。

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