1499.When you apply hydraulic pressure,make sure that the lever does not touch the stop.

1151.Note is an operating procedure,inspection,repair or maintenance condition,etc.,which is deemed essential to highlight.

A. Notes emphasize conditions such as operating procedures,inspection,repair or maintenance,etc.,which may be met as appropriate.

B. Notes emphasize the conditions of operation procedure,inspection,repair or maintenance,etc.,must be followed.

C. Conditions for operating procedures,inspection,repair or maintenance,etc.must be emphasized in the notes.

229.Attach the two ends of the hose.

A. 把软管的两端连接起来。

B. 把两端和软管串起来。

C. 把孔的两端连接起来。

1856.发动机功率控制系统可以控制主燃油控制器或调节器,包括涡轮螺旋桨发动机上螺旋桨调速器的控制装置。

A. The engine power control system manages and controls the main fuel control or synchronizer,which is inclusive of controls to the propeller modulator on a turboprop engine.

B. The engine power control system furnishes a means of controlling the main fuel control or coordinator,which includes controls to the propeller regulator on turbo-prop engines.

C. The engine power control system regulates and controls the main oil,coordinator and propeller regulator of a turboprop engine.

2785.Functional Test: That procedure required to ascertain that a system or unit is functioning in all aspects in accordance with minimum acceptable system or unit design specifications .These tests may require supplemental ground support equipment and should be more specific and detailed than an operational test.It should contain all necessary information to perform proficiency test to maintain system or unit reliability at an acceptable level ,without reference to additional documents.

A. “功能测试:该过程旨在确定系统或组件按照最低可接受设计标准在所有方面的功能。这些测试可能需要补充地面支持设备,并且应该比飞行测试更具体和详细。它应该包含所有熟练检查所必要的信息,以维持系统或组件在可接受水平上的可靠性,无需参考其他文件。

B. “功能测试:该过程旨在确定系统或组件按照最低可接受设计标准在所有方面运行正常。这些测试可能需要补充地面支持设备,并且应该比操作测试更具体和详细。它应该包含所有熟练检查所必要的信息,以维持系统或组件在可接受水平上的可靠性,无需参考其他文件。

C. “功能测试:该过程旨在确定系统或组件按照可接受的最少系统和可接受的最低设计标准在所有方面的功能。这些测试可能需要补充地面支持设备,并且应该比飞行测试更具体和详细。它应该包含所有熟练检查所必要的信息,以维持系统或组件在可接受水平上的可靠性,无需参考其他文件。

D. B.“功能测试:该过程旨在确定系统或组件按照最低可接受设计标准在所有方面运行正常。这些测试可能需要补充地面支持设备,并且应该比操作测试更具体和详细。它应该包含所有熟练检查所必要的信息,以维持系统或组件在可接受水平上的可靠性,无需参考其他文件。

E. C.“功能测试:该过程旨在确定系统或组件按照可接受的最少系统和可接受的最低设计标准在所有方面的功能。这些测试可能需要补充地面支持设备,并且应该比飞行测试更具体和详细。它应该包含所有熟练检查所必要的信息,以维持系统或组件在可接受水平上的可靠性,无需参考其他文件。

2153.All text shall be prepared in one or two columns with justification at the discretion of the manufacturer; however,two columns are preferred for ease of reading.

A. The manufacturer shall prepare all text in either one or two columns with justification at his own discretion ,but,two columns are preferable for readability.

B. Manufacturers shall prepare all text both in one and two columns separately; however,two columns are better for reading.

C. According to the manufacturer' explanations,all text shall be prepared in one or two columns; however,two columns have better visual effect.

2946.缓慢地把 RAT 完全放出,并确保它不接触其他部件。

A. Slowly and fully extend the RAT and make sure that it does not touch other parts.

B. Quickly and fully retract the RAT and make sure that it does not touch other parts.

C. Slowly and carefully extend the RAT and make sure that it does not attach to other parts.

432.Align the drill until it is perpendicular to the surface.

A. 实施训练,直到熟练操作舵面。

B. 对准钻头,直到它与表面垂直。

C. 安装钻头,直到它与表面平齐。

1826.Accelerate Stop Distance is the distance required to accelerate an airplane to a specified speed and,assuming failure of an engine at the instant that speed is attained,to bring the airplane to a stop.

A. 加速停止距离是指飞机按照要求加速到指定速度所需的距离,并假定在达到该距离的那一刻发动机发生故障,飞机需要停止飞行。

B. 加速停止距离是指将飞机加速到指定速度,并假定在达到该速度的那一刻发动机发生故障,使飞机停止飞行所需的距离。

C. 加速停止距离是指将飞机加速到规定速度,并推测在达到该速度时发动机故障,飞机须立即停止飞行。

D. C.加速停止距离是指将飞机加速到规定速度,并推测在达到该速度时发动机故障,飞机须

E. C.加速停止距离是指将飞机加速到规定速度,并推测在达到该速度时发动机故障,飞机须立即停止飞行。

2005.Numbering shall be in numerical progression,prefixed by the Section Number.

A. 编号应成数字级数排列,以章节号为前缀。

B. 编号应冠以章节号,按数字顺序排列。

C. 以章节号开头,数字大小排列。

1915.You can do the test in two different ways -- either with the Central Maintenance Computer System via the MCDU,like you have probably learned already,or with a test switch on the VOR receiver in the avionics compartment.

A. Two controversial ways can be chosen to do the test,either with the Central Maintenance Computer System through a the MCDU,like you have probably learned already,and with a test switch on the VOR receiver in the avionics compartment.

B. You can do the test following procedures -- with the Central Maintenance Computer System bythe MCDU,you have probably learned already,and with a test switch on the VOR receiver in the avionics compartment.

C. The test can be done in either way below-- using the Central Maintenance Computer System via the MCDU,as you have probably already learned,or using a test switch on the VOR receiver in the avionics compartment.

D. U,as you have probably already learned,or using a test switch on the VOR receiver in the avionics compartment.