A、 This procedure gives you the disassembly process.
B、 You can find the procedures for disassembling in this section.
C、 The assembly process can be found in this section.
答案:B
A、 This procedure gives you the disassembly process.
B、 You can find the procedures for disassembling in this section.
C、 The assembly process can be found in this section.
答案:B
A. Estimate the quality of fuel used for the flight.
B. Compute the quantity of fuel required for the flight.
C. Evaluate the quantity of fuel in the flight.
A. The job is required to be divided into logical steps or operations.
B. This needs to break the work and distribute the logical steps or operations.
C. This requires to destroy the job logically into steps or operations.
A. This document lists appropriate description of Continuous Airworthiness as indicated in Appendix G.
B. This document marks the Appendix G as an appropriate descriptions of Continuous Airworthiness.
C. This document contains appropriate instructions for Continued Airworthiness as described in Appendix G.
A. 将装置连接到液压测试仪表上。
B. 将配件装到液压试验器上。
C. 将接头连接到液压测试台。
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. Write the instructions in the mandatory mode.
B. Write the instructions in the imperative form.
C. Write the instructions in the active mode.
A. Make a little oil to the threads of the two bolts.
B. Apply a small quantity of oil to the threads of the two bolts.
C. Apply a small quantity of oil to the threads of the two nuts.
A. AMM 的第 12 章第 10 节是关于补给的。它提供了添加燃油、滑油、液压油、水、其他液体和轮胎充气等所需的说明。
B. AMM 的第 12 章第 10 节是关于补液的。它提供了补给燃油、滑油、液压油、水、其他液体和轮胎压力等所需的说明。
C. AMM 的第 12 章第 10 节是关于补液的。它提供了补给液压油、滑油、燃油、水、其他液体和轮胎压力等所需的说明。
D. B.AMM 的第 12 章第 10 节是关于补液的。它提供了补给燃油、滑油、液压油、水、其他液体和轮胎压力等所需的说明。
E. C.AMM 的第 12 章第 10 节是关于补液的。它提供了补给液压油、滑油、燃油、水、其他
F. C.AMM 的第 12 章第 10 节是关于补液的。它提供了补给液压油、滑油、燃油、水、其他液体和轮胎压力等所需的说明。
A. 另外,它应提供手册中使用的符号、缩略语和术语的定义或解释。
B. 另外,它应提供象征的定义或解释、缩略语和手册中使用的术语。
C. 另外,它应提供符号和缩略语的定义或解释、以及手册中使用的技术。
A. Horsepower Radius and Engine Revolving Speed
B. Horsepower Ratings and Propeller Rotational Speed
C. Horsepower Values and Propeller Turning Speed