2827. Outlet pressure of control unit fails to stabilize at proper pressure

A. 将透明塑料环从电子锁的末端拉岀。

B. 将透明塑料环从电子锁的前端拉岀。

C. 将透明塑料环从电子锁的顶端拉岀。

A. Total number of rules is decreased from 65 to 53.

B. Total number of rules ascended from 65 to 53.

C. Total number of rules increased from 65 to 53.

A. The isolation blanket has a waterproof layer that is installed in a brick configuration to prevent leakage of condensed water into the carriage.

B. The insulation blankets have a waterproof layer and are installed in a tiled configuration to prevent leakage of condensed water into the compartment.

C. The insulating blankets have a watertight layer which is mounted in a shingled configuration to protect leakage of water condensation into the compartment.

D.

E.

F.

G.

H.

I.

J.

A. For aircraft with a range of sophistic or complex systems, a system-wide indexing approach is recommended.

B. For aircraft including an article of exquisite or complex systems, a whole system indexing way is intended.

C. The aircraft which have a number of complicated or complex systems are suggested to use the full system/chapter index method.

A. 包括附件部分整流罩、整流片、整流罩支架、连接和锁定机构等项目的功能和维护方面,不包括与机身一体的结构,其应包含在对应的结构章节中。

B. 包括附件部分整流罩、整流片、整流罩支架、连接和锁定机构等项目的功能和维护方面,还包括与机身一体的结构。

C. 包括附件部分整流罩、整流片、整流罩支架、连接和锁定机构等项日的功能和维护方面,与机身一体的结构,不应包含在对应的结构卒节中。

A. remove the safety strips and tags after troubleshooting

B. remove the safety clips and tags after troubleshooting

C. remove the safety clips and tags before troubleshooting

A. 用于照亮桨叶的操作或显示的部分,包括灯、电门等。

B. 用于指示螺旋桨系统的操作或激活的部分。包括灯、电门等。

C. 用于指示桨叶的操作或显示的部分,包括灯、电门等。

A. Do not stretch the seal when installing it.

B. Do not over-extend the seal when installing it.

C. Do not bend the seal when installing it.

A. Evaporate the amount of cleaning fluid that is necessary;

B. Evaluate the amount of cleaning fluid that is necessary;

C. Estimate the amount of cleaning fluid that is necessary;

A. The following procedures will prevent deterioration of aircraft structural coatings or system components.

B. The procedures that follow will prevent the deterioration of the airplane structure, finish, or system components.

C. The delamination of the airplane structure, finish, or system parts will be blocked by the procedures listed below.