Examine the bottom skin panels of the fuselage for cracks.

A. When the temperature is below zero, depressurize the water system.

B. If the temperature drops below zero, deflate the water system.

C. If the temperature decreases to less than zero, drain the water system.

A. 显示连接点的位置，转弯半径的图解应包括在内。

B. 附着点的位置和转弯半径应包括插图。

C. 插图显示连接点的位置还包括转弯半径。

A. 如果没有必需的修理程序，仔细检查燃油渗漏来确保不会渗漏更多。

B. 没有必须的维修程序。检查燃油使用频率确保使用量不会变大。

C. 无需执行修理程序。经常检查燃油渗漏情况，确认区域没有扩大。

A. This Specification was issued by the General Aviation Manufacturers Association

B. This Specification was revised by the General Aviation Manufacturers Association

C. This Specification was compiled by the General Aviation Manufacturers Association

A. 拆卸/安装部分应清晰地描述拆卸和重新安装部件或装置所要求的步骤方法，以及应观察的预防措施。

B. 拆卸/安装部分应明确地说明拆卸和重新安装部件或装置所需的步骤要求，不需包含观察到的预防措施。

C. 拆卸/安装部分应清楚地说明拆卸和重新安装部件或装置所需的步骤顺序，以及应遵守的预防措施。

A. 驾驶舱的控制允许选择温度和流速。

B. 在飞行舱的控制允许选择温度和流速。

C. 驾驶舱的控制允许选择温度和流动方向。

A. 拉力连杆组件将拉力载荷从轮轴传递到减震支柱。

B. 张力连杆组件将张力负载从轴心传递到减震支柱。

C. 扭力连杆组件能将扭力载荷从轴传递到减震支柱。

A. Do the weighing procedure in this sequence.

B. In this order to perform the swapping procedure.

C. In this sequence to do the analysis procedure.

A. 在外表面上涂抹密封胶。

B. 在外壁板施加载荷。

C. 在外壳上喷涂防锈剂。

A. Using a locally made tool to do the test is also accepted.

B. You can also make a local tool to do this test.

C. You can also make a tool to do this test locally.