178. On going investments in airport infrastructure----runways,terminals and technology----will ensure that maximum benefits will be gained from transforming the air traffic system and renovating aircraft fleets

A. 如果此说明书被用于准备一份持续适航程序,目的是被适航当局FAA认可,那么可能需要更改为合适的机构和规章;

B. 如果此说明书被用于准备一份持续适航程序,目的是被适航当局,比如FAA认可,那么可能需要更改为合适的机构和规章;

C. 如果此说明书被用于准备一份持续适航程序,目的是被FAA以外的适航当局认可,那么可能需要更改为合适的机构和规章;

A. The distance between the edge of the panels and the partition must be less than 0.05 mm.

B. The distance between the edge of the panel and the partition must be equal to 0.05mm

C. The distance between the edge of the panel and the partition must be 0.05 mm or less.

A. 该组件分配和过滤油液。

B. 该组件增压和过滤油液。

C. 该组件增压和旁通油液。

A. As you do the valve test, make sure that there is no leakage. Assess the quantity of fuel needed.

B. While you do each step of the valve test, make sure that there is no leakage. Concern the quantity of fuel necessary.

C. As you do the valve test, make sure that there is no leakage. Release the quantity of fuel needed.

A. IF YOU USE SOLVENT IN A CLOSED SPACE, MAKE SURE THAT THERE IS GOOD AIRFLOW IN THE WORK AREA.

B. IF YOU USE SOLVENT IN A ENCLOSED SPACE, MAKE SURE THAT THERE IS GOOD AIRFLOW IN THE WORK AREA.

C. IF YOU USE SOLVENT IN A CLOSED SPACE, ENSURE THAT THERE IS GOOD AIRFLOW IN THE WORK AREA.

A. Refer to FIG.401 for the distance between rivets.

B. If you want to know the distance between bolts, refer to FIG.401.

C. Look at FIG.401 for the dimension between bolts.

A. Alternatively, you can do test B.

B. Test A is irreplaceable.

C. Test A is the equivalent of test B.

A. 内部喇叭打到开位并且保持在开位,当探测器有动力的时间够长,并且烟雾传感器探测到烟雾。

B. 只有探测器有电, 并且烟雾传感器探测到烟雾, 内部开关才会打开到开位并且保持在开位。

C. 只要探测器有电源并且烟雾传感器探测到烟雾,内部的喇叭就会打开并且保持在开位。

A. Both particle and chemical contaminants can adversely affect the nature and longevity of aircraft hydraulic system components.

B. Particular and chemical contamination is not conductive to the property and lifespan of aircraft hydraulic system.

C. The pollution of dust and chemicals will damage the performance and life of components in the aircrafts hydraulic system.

A. The power for the airplane＇s ascent comes from the dynamic action of the wings relative to the air.

B. The power for the airplane＇s going up is from the dynamic action of the wings by use of the air.

C. Taking advantage of the air between the dynamic wings, lift for the airplane is obtained.