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2169. 轮胎磨损随速度的增加而增加。

A、 Tire wear increases with high speed.

B、 The higher the speed is, the more fragile the tire becomes.

C、 The tire blows out as the speed increases.

答案:A

设备系统操作理论翻译
1305. The technique or procedure necessary to duplicate the performance presented shall be included for those items of performance where the attainment of the predicted airplane performance requires a special sequence of actions
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2689. Install the sealing ring in the groove of the spherical bearing
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1147. The diagram shall be arranged so that the flow of the system dan be traced with a minimum of effort
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856. Water displacing corrosion inhibiting compound has been applied during construction on certain airplanes Ain the locations shown in this figure Periodic reapplication in these, and other locations, is required to maintain effectiveness of this protection
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590. Some cases, cleaning the connectors or replacing the IDG appears to correct the problem, but the messages recur after some time
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815. The operational test for the HFS-900D transceivers is a BITE test which does a check of the internal functions of the HF transceiver
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743. Do not apply solvents, grease, or oil to stainless steel control cables These materials can collect contamination that can cause damage to the internal surfaces of the CRES cable strands
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3021. Engine fire detection system is system of dual loop
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759. This Specification was developed by the General Aviation Manufacturers Association as guidance for airplane, engine and component manufacturers in preparing Continuing Airworthiness Program Inspection Documents ( ) CAPs may be prepared for all types of general aviation airplanes and components certificated under the applicable Federal Aviation Regulations
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2722. Inspection and modification per this bulletin will reduce the possibility of stress corrosion cracks which would require replacement of the stabilizer center section front spar
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设备系统操作理论翻译

2169. 轮胎磨损随速度的增加而增加。

A、 Tire wear increases with high speed.

B、 The higher the speed is, the more fragile the tire becomes.

C、 The tire blows out as the speed increases.

答案:A

设备系统操作理论翻译
相关题目
1305. The technique or procedure necessary to duplicate the performance presented shall be included for those items of performance where the attainment of the predicted airplane performance requires a special sequence of actions

A. 技术和程序是复制性能所需的,并应包括性能项目,其在达到预期飞机性能时需要特殊动作序列

B. 复制性能所需的技术和程序应包括那些达到预期飞机性能需要特殊动作序列的性能项目。

C. 对于那些达到飞机预期性能需要特殊动作顺序的性能项目,应包括复制所述性能所需的技术或程序

https://www.shititong.cn/cha-kan/shiti/0009ffaa-70d5-5ed4-c0b8-ef8d402da900.html
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2689. Install the sealing ring in the groove of the spherical bearing

A. 将封圈安装在锥形轴承的凹槽里

B. 将封圈安装在圆形轴承的凹槽里

C. 将封圈安装在球形轴承的凹槽里

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1147. The diagram shall be arranged so that the flow of the system dan be traced with a minimum of effort

A. The flow of the system can be traced as easily as possible through the arrangement of the diagram.

B. A reasonable distribution of the diagram helps to duplicate the flow of the system with least difficulties.

C. The diagram shall be arranged in order to draw a minimum flow of the system without effort.

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856. Water displacing corrosion inhibiting compound has been applied during construction on certain airplanes Ain the locations shown in this figure Periodic reapplication in these, and other locations, is required to maintain effectiveness of this protection

A. At the location shown in the figure, waterproof corrosion inhibiting compound has been used on certain aircraft construction. To keep the effectiveness of this protection, reapply the compound in these or other locations periodically.

B. Water displacing corrosion inhibiting compound has applied on certain airplanes structure in the locations in this figure. Periodic reapplication must be applied in these and other locations, so as to maintain effectiveness of this protection.

C. Water displacing anti-seize compound has been applied on certain airplanes construction in the locations in this figure. Periodic reapplication should be utilized in these and other locations, in order to keep effectiveness of the protection

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590. Some cases, cleaning the connectors or replacing the IDG appears to correct the problem, but the messages recur after some time

A. In certain circumstances, cleaning the connector or replacing the IDG seems to solve the problem, but the messages will appear again later.

B. Sometimes, cleaning the connector or replacing the IDG seems to settle the problem, but the message will reappear occasionally.

C. Sometimes, sterilizing the connector or renewing the IDG seems to resolve the problem, but the message will occur later.

https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b3e-ebf6-c0b8-ef8d402da900.html
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815. The operational test for the HFS-900D transceivers is a BITE test which does a check of the internal functions of the HF transceiver

A. The operational test of HFS-900D transceivers is internal functions check of the HF transceiver and it is a BITE test.

B. The BITE test for the HFS-900D transceivers is the operation test that does the inner check of the HF transceiver.

C. The check of the internal functions of the HF transceiver is a BITE test related to HFS-900D transceivers.

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743. Do not apply solvents, grease, or oil to stainless steel control cables These materials can collect contamination that can cause damage to the internal surfaces of the CRES cable strands

A. 请勿在不锈钢控制电缆上涂抹溶剂、油脂或油。 这些材料可能会积聚污染,从而对CRES电缆绞线的内表面造成损坏。

B. 请勿在不锈钢控制电缆上涂抹溶剂、油脂或油。 这些材料可能会积聚污染,从而对CRES电缆线束的内表面造成损坏。

C. 请勿在不锈钢控制电缆上涂抹溶剂、油脂或油。 这些材料可能会导电,从而对CRES电缆线束的内表面造成损坏。

https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b40-ffb4-c0b8-ef8d402da900.html
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3021. Engine fire detection system is system of dual loop

A. 发动机火警探测系统是一个双环路系统

B. 发动机火警探测系统是一个全循环系统

C. 发动机火警探测系统是一个重复回路系统

https://www.shititong.cn/cha-kan/shiti/0009ffba-8e34-22f1-c0b8-ef8d402da900.html
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759. This Specification was developed by the General Aviation Manufacturers Association as guidance for airplane, engine and component manufacturers in preparing Continuing Airworthiness Program Inspection Documents ( ) CAPs may be prepared for all types of general aviation airplanes and components certificated under the applicable Federal Aviation Regulations

A. When the airplane, engine and component manufacturers prepare Continuing Airworthiness Program Inspection Documents(which may also be called Continuing Airworthiness Programs or CAPs),they can consult this Specification as a guidance.

B. General Aviation Manufacturers Association Built up this Specification to guide the airplane, engine and component manufacturers to prepare Continuing Airworthiness Program Inspection Documents(which may also be called Continuing Airworthiness Programs or CAPs). All types of general aviation airplanes and components certified under the applicable Federal Aviation Regulations may be utilized to CAPs

C. General Aviation Manufacturers Association Built up this Specification to guide the airplane, engine and component manufacturers to prepare Continuing Airworthiness Program Inspection Documents(which may also be called Continuing Airworthiness Programs or CAPs). All types of general aviation airplanes and components certified under the applicable Federal Aviation Regulations may prepare CAPs

https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b41-342f-c0b8-ef8d402da900.html
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2722. Inspection and modification per this bulletin will reduce the possibility of stress corrosion cracks which would require replacement of the stabilizer center section front spar

A. This bulletin should be followed to inspect and modify the stress corrosion cracks which is caused by replacing the stabilizer center section front spar.

B. The stabilizer center section front spar would be replaced due to the stress corrosion cracks. However, if the spar is inspected and modified per this bulletin, the cracks will be reduced.

C. During inspection and modification per this bulletin, the stress corrosion cracks are found after replacement of the stabilizer center section front spar.

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