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2421. Excessive trim, however, has the effect of reducing not only aerodynamic efficiency but also primary control travel distance in the direction the trim is applied

A、 然而,过度的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

B、 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平应用方向上的主控制舵面的偏转行程。

C、 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

答案:B

设备系统操作理论翻译
2763. 机身是半硬壳结构。
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225. This Section shall contain a legible statement in a prominent location to the effect that the Airworthiness Limitations Section is FAA approved
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921. Engine Failure Procedures shall be provided for all airplanes for all cases of engine failure, including partial failure, during takeoff and in flight
https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b43-4cb3-c0b8-ef8d402da900.html
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118. 在燃油泄漏区域涂抹滑石粉
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2385. Be careful with easily damaged parts
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1836. 737NG Wing Span is 11258 feet
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2494. The values must not be more than the approved differences
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2532. Apply grease to the fasteners
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2017. Non destructive testing, NDT is a preventative maintenance test procedure that can detect hidden defects without damage to the part being inspected
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1511. If fumes come through, do the emergency procedure
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设备系统操作理论翻译

2421. Excessive trim, however, has the effect of reducing not only aerodynamic efficiency but also primary control travel distance in the direction the trim is applied

A、 然而,过度的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

B、 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平应用方向上的主控制舵面的偏转行程。

C、 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

答案:B

设备系统操作理论翻译
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2763. 机身是半硬壳结构。

A. The fuselage is a semi-monocoque structure

B. The fuselage is a demi-plate.

C. The airframe is of half-shell structure.

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225. This Section shall contain a legible statement in a prominent location to the effect that the Airworthiness Limitations Section is FAA approved

A. 在本节显著的位置应包括一个清楚的声明,内容是适航限制部分由FAA批准

B. 当本节很显著标示出适航限制部分,这说明FAA批准了其影响。

C. 本节应在显著位置包括一份清晰的声明,说明适航限制部分的影响是FAA批准的。

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921. Engine Failure Procedures shall be provided for all airplanes for all cases of engine failure, including partial failure, during takeoff and in flight

A. 发动机失效程序应该提供给所有的飞机,飞机起飞和飞行中出现的所有失效,包括部分失效都应包括。

B. 发动机失效程序应提供所有飞机在起飞和飞行中发生的所有发动机失效,包括部分失效。

C. 发动机失效程序应提供给所有飞机和所有发生的情况,包括在起飞和飞行中的部分失效。

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118. 在燃油泄漏区域涂抹滑石粉

A. Apply the talcum powder in fuel leak area.

B. Apply the kathon in fuel leak area.

C. Apply the bubble solution in fuel leak area.

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2385. Be careful with easily damaged parts

A. 小心修理损伤的零件。

B. 小心易损伤的零件。

C. 对于损伤的零件要小心。

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1836. 737NG Wing Span is 11258 feet

A. 737NG翼展是112.58英尺。

B. 737NG翼尖小翼尺寸为112.58英尺。

C. 737NG停放时大翼间距至少为112.58英尺。

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2494. The values must not be more than the approved differences

A. The values doesn't have to be more than the approved differences.

B. The values must be less than the approved differences.

C. The values must not be less than the approved differences.

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2532. Apply grease to the fasteners

A. 在快速齿轮上涂抹润滑脂。

B. 按照紧固件来申请润滑脂。

C. 给紧固件涂上油脂。

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2017. Non destructive testing, NDT is a preventative maintenance test procedure that can detect hidden defects without damage to the part being inspected

A. the NDT detect part’s defects and no damage caused by to the part.

B. the NDT can detect the defects on the surface of the part only.

C. Non destructive testing, NDT is a preventative maintenance test procedure that can detect hidden defects, but damage may cause to the part being inspected.

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1511. If fumes come through, do the emergency procedure

A. 如果有烟雾冒出,执行紧急程序。

B. 如果有气体产生,执行紧急程序。

C. 如果液体流出,执行紧急程序。

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