Recommended Fuel Conservation Information shall be integrated into this section to show the pilot how to minimize fuel usage during operation of the airplane.

A. 在性能图表和表格中，始终使用KNOTS，以避免将节(KTS)和英里每小时(MPH)混淆。

B. KNOTS在性能图和表格中一直被使用，以防止将节(KTS)和英里每小时(MPH)定义混淆。

C. 为了防止在节(KTS)和英里每小时(MPH)之间进行选择，规定在性能图表和表格中始终使用KNOTS。

A. 手册中可包括其他的程序，这些程序适用于飞机操作。

B. 与飞机操作有关或必要的其他程序可包括在手册中。

C. 说明中应包括飞机操作相关或适用的其他程序。

A. 本章中任何或所有部件的翻修必须使用部件制造商提供的数据完成。

B. 任何或所有部件的销售必须提供本章有关的部件生产商数据。

C. 本章中任何或所有部件的翻新必须由部件生产商完成并提供数据。

A. The specification gives the symbols for relays, diodes, and other parts of the system.

B. The specification gives the requirement for markings on relay, triode and other parts of the system.

C. The specification excludes symbols for relays, diodes, and other system parts.

A. The EEC processes the simulated signal from the fuel filter differential pressure bulb.

B. The fuel filter differential pressure sensor sends an modulated signal to the EEC.

C. The EEC receives the analog signal from the fuel filter differential pressure switch.

A. The forward movement of the control lever must be slow and continuous.

B. The control lever must be kept moving forward slowly and abruptly.

C. You must continuously slow down the forward movement of the control lever .

A. 最大起落架放下速度是指起落架放下状态下飞机可以安全飞行的最大速度。

B. 最大起落架收放速度是指起落架收放过程中飞机可以安全飞行的最大速度。

C. 最大起落架收上速度是飞机可以安全飞行的最大速度，起落架收上。

A. 描述飞机控制锁时，应说明如何连接控制锁或固定操纵面。

B. 描述飞机阵风锁时，应描述如何使用阵风锁或锁住操纵面。

C. 描述飞机舵面锁时，应说明如何参与舵面锁和操纵装置的固定。

A. This section includes limitations adapted by the airworthiness authority.

B. The limitations included in this Section are approved by the airworthinessauthority.

C. The limitations included in this Section are adopted by the airworthiness authority.

A. This system does not supersede the normal channels of communication for items not covered by the CAP.

B. This system will not change the normal ways of communication for items not listed by the CAP.

C. The normal methods of communication for items contained in the CAP will not be shifted.