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236.Perform preliminary inspection of all articles that are maintained.

A、 对所有维修过的产品进行全面检查。

B、 对所有维修过的产品进行仔细检查。

C、 对所有维修过的产品进行初始检查。

答案:C

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2390.The following weights shall be presented if applicable: (a) Maximum Ramp Weight; (b) Maximum Takeoff Weight; (c) Maximum Landing Weight; (d) Maximum Zero Weight; (e) Maximum Weight in Baggage Compartment(s).
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320.The ventilation system uses differential pressure to pull air out of the airplane.
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967.将螺纹线连接到新电缆上。
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2310.Limitations associated with optional systems or equipment may be included in this Section or in Section 9,Supplements.
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2725.易燃物品与工作区域保持至少 50 英尺的距离。
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1187.The values must not be more than the approved differences.
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2329.That portion of the system provides the major support for the aircraft while on the ground,including items such as shock struts,bogie axles,drag struts,doors,linkages,attach bolts,etc.
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1134.The manufacturer supplies the safety procedures.
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2662.在动力装置表面或其周围安装有阻热隔板或封严层。
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1831.操作测试:这个过程仅需要确定系统或单元是可工作的。这些测试不应需要除已安装在飞机上外的任何特殊设备或设施,应该与机组人员执行的测试相当。操作测试不要求满足针对翻修或重大修理制定的规范和容错要求。
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236.Perform preliminary inspection of all articles that are maintained.

A、 对所有维修过的产品进行全面检查。

B、 对所有维修过的产品进行仔细检查。

C、 对所有维修过的产品进行初始检查。

答案:C

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2390.The following weights shall be presented if applicable: (a) Maximum Ramp Weight; (b) Maximum Takeoff Weight; (c) Maximum Landing Weight; (d) Maximum Zero Weight; (e) Maximum Weight in Baggage Compartment(s).

A. 如适用,还应提供以下重量:(a)最大停机坪重量;(b)最大起飞重量;(c)最大着陆重量;(d)最大零燃油重量;(e)最大行李舱重量。

B. 如可以,还应提供以下重量:(a)最大坡道重量;(b)最大起飞重量;(c)最大着陆重量;(d)最大无油重量;(e)最大行李舱重量。

C. 如适用,还应提供以下数据:(a)最大停机坪重量;(b)最大着陆重量;(c)最大起飞重量;(d)最大零重量;(e)最大行李重量。

D. B.如可以,还应提供以下重量:(a)最大坡道重量;(b)最大起飞重量;(c)最大着陆重量;(d)最大无油重量;(e)最大行李舱重量。

E. C.如适用,还应提供以下数据:(a)最大停机坪重量;(b)最大着陆重量;(c)最大起飞重量;

F. C.如适用,还应提供以下数据:(a)最大停机坪重量;(b)最大着陆重量;(c)最大起飞重量;(d)最大零重量;(e)最大行李重量。

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320.The ventilation system uses differential pressure to pull air out of the airplane.

A. 通风系统使飞机产生不同的压力从而将废气排出。

B. 飞机利用通风系统将空气排出机外。

C. 通风系统利用压差将空气排出飞机。

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967.将螺纹线连接到新电缆上。

A. Attach the threading cord to the new cable.

B. Attach the screw's cord to the new cable.

C. Attach the screw's wire to the new cable.

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2310.Limitations associated with optional systems or equipment may be included in this Section or in Section 9,Supplements.

A. 限制因素与可选系统和设备都是相关的,它们可以包括在这部分或者第 9 部 “附录”中。

B. 限制可选系统或设备的因素可能包括在这部分或者第 9 部“附录”中。

C. 与选装系统或设备相关的限制因素可以包含在本节内或者第 9 节“附录”中。

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2725.易燃物品与工作区域保持至少 50 英尺的距离。

A. A maximum distance of 50 feet is required between consumable materials and the work area.

B. Keep flammable materials at a minimum distance of 50 feet from the work area.

C. Explosive materials must be kept at least 50 feet away from the work area.

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1187.The values must not be more than the approved differences.

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

B. The values must not exceed the allowable differences.

C. The values must be less than the allowable differences.

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2329.That portion of the system provides the major support for the aircraft while on the ground,including items such as shock struts,bogie axles,drag struts,doors,linkages,attach bolts,etc.

A. 系统的这一部分能够为飞机在地面上提供主要支撑,包括减震支柱、轮架轴、阻力杆、门、连杆、固定螺栓等。

B. 这部分系统为飞机在地面上提供主要支持,包括控制装置、管道、阻力支柱、门、连杆、上下门闩等。

C. 这部分系统为飞机在地面上提供主要支持,包括旋转密封套、管道、防滑装置、门、连杆、连接栓等。

D. C.这部分系统为飞机在地面上提供主要支持,包括旋转密封套、管道、防滑装置、门、连杆、连接栓等。

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1134.The manufacturer supplies the safety procedures.

A. The safety procedures are provided by the operators.

B. The safety procedures are provided to the manufacturers.

C. The safety procedures are provided by the manufacturers.

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2662.在动力装置表面或其周围安装有阻热隔板或封严层。

A. The fire-proof materials and seals are mounted on or about the power unit.

B. The fire-resistant partitions and seals are mounted on the power unit.

C. The fire-resistant partitions and seals are mounted on or about the power package.

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1831.操作测试:这个过程仅需要确定系统或单元是可工作的。这些测试不应需要除已安装在飞机上外的任何特殊设备或设施,应该与机组人员执行的测试相当。操作测试不要求满足针对翻修或重大修理制定的规范和容错要求。

A. Operational Test: That procedure required to ascertain only that a system or unit is operable.These tests should require no special equipment or facilities other than that are installed on the aircraft and should be comparable to the tests performed by the flight crew.It is not intended that theoperational test of the unit shall meet the specifications and tolerances ordinarily established for overhaul,or major maintenance periods."

B. Operational Test: That procedure required to ascertain only that a system or unit is operable.These tests should require no special equipment or facilities other than that are installed on the aircraft and should be comparable to the tests performed by the flight crew.It is not intended that the operational test of the unit shall meet the specifications and errors ordinarily established for overhaul,or significant maintenance periods."

C. Operational Test: That procedure required to ascertain only that a system or unit is operable.These tests should require no special equipment or facilities other than that are installed on the aircraft and should be comparable to the tests performed by the flight crew.It is not intended that the operational test of the unit shall meet the specifications and tolerances ordinarily established for overhaul,or significant maintenance periods.

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