The anti-icing system of the engine eliminates and prevents ice formation by bleed air in all parts of the engine (excluding power cowling), and is inclusive of several components such as valves, plumbing, regulators, etc.

A. 位于连接发电机和驱动组件的法兰上的端口，使滑油在恒定转速驱动器和可用发电机之间流动。

B. 位于连接发电机和驱动组件的连接处的端口，使滑油产生了在变速驱动器和发电机之间流动的可能性。

C. 端口位于连接发电机和驱动组件的法兰上，使滑油可以在恒速驱动器和发电机之间流动。

A. Write instructions in the infinite form.

B. Write instructions in the command form.

C. Write instructions in the appropriate form.

A. Discard the removed fasteners.

B. Throw away the removed components.

C. Leave out the removed gaskets.

A. Navigation and full/static pressure systems refer to those units and components that provide aircraft navigation information, covering OOMB, pitot, static, ILS, flight guides, binnacles, indicators, etc.

B. Navigation and pitot/static systems refer to those units and components which provide aircraft navigational information, including VOR, pitot, static, ILS, flight director, compasses, indicators, etc.

C. Navigation and pitot/static systems refer to those units and components that provide aircraft navigation information, including VOR, pitot, still tubes, instrumental system, flight manual, compasses, indicator, etc.

A. Incorrect adjustment of the stops will lead to accurate test results.

B. In precision, test results cannot occur unless the stops are adjusted properly.

C. If the stops are not adjusted Incorrectly, the test results will not be precise.

A. The valve has flaps shaped like a full circle.

B. The shape of the valve flaps is a half ring.

C. The valve flaps have a shape of half circle.

A. 所有改版数量和日期都应该从页面上删除。

B. 所有版本号和日期都应该从页面上删除。

C. 所有改版次数和日期都应从页面上删除。

A. 《持续适航大纲检查文件》包含的检查数据连同运营人现有的维修大纲，有助于保持ABC公司 XXX系列飞机的结构完整性和持续适航性。

B. 《持续适航大纲检查文件》是一种检查数据，与运营人现有的维修计划相结合时，将有助于保持ABC 公司XXX系列飞机的结构完整性和持续适航性。

C. 《持续适航大纲检查文件》是检查数据，当与运营人现有的维护计划相结合时，将有助于保持ABC 公司XXX系列飞机的结构完整性和持续适航。

A. 提供液压动力的说明在显示液压动力警告的屏幕底部，你必须向下滚动屏幕才能看到说明。

B. 液压动力供给说明在屏幕底部显示液压动力警告，你必须向下滚动屏幕才能看到说明。

C. 你必须向下滚动屏幕才能看到液压动力供给指令，因为指令在显示警告的屏幕底部。

A. After a continued airworthiness process,almost every component composed of an airplane is involved in some form of preservation,inspection,preventative maintenance, overhaul,repair, and/or replacement activity.

B. Through a continuing airworthiness process, virtually every component comprising an airplane is involved in some form of preservation,inspection,preventative maintenance,overhaul, repair, and/or replacement activity.

C. Through a continuing airworthiness process, substantially every component of an airplane is excluded in some type of preservation,inspection,preventative maintenance, overhaul,repair, and/or replacement activity.