1354. Troubleshooting information may be presented by either troubleshooting charts or by text, or a combination of text and supplementary charts

A. The section of the engine which by-passes a portion of the normal engine airflow for the prime purpose of adding to engine thrust or reducing specific fuel consumption.

B. The section of the engine which by-passes a portion of the normal engine airflow for the prime purpose of reducing to engine thrust or adding specific fuel consumption.

C. The section of the engine by-passes a portion of the normal engine airflow to add to engine thrust or reduce specific fuel consumption.

A. 用直尺和塞尺测量划痕的深度。

B. 用直尺和塞尺测量凹痕深度。

C. 用直边的卡尺测量凹坑的深度。

A. The lateral axis is perpendicular to the longitude axis.

B. The lateral axis is the axis about which the aircraft rolls.

C. The lateral axis consist of left wing and right wing.

A. The first tape is applied on the cut out, then the second and third tapes are applied horizontally.

B. Applied the first layer of tape across the cutout and the second and third layers diagonally.

C. First attch the tape to the cutout, and attch the second and third layers of tape perpendicularly.

A. 面罩

B. 护目镜

C. 防护服

A. Basic control and operation information describing how the airplane components are controlled and how they operate, including any special procedures, and limitations that apply.

B. Basic control and operation information describing how the airplane components are controlled and operated, including any special procedures, and limitations that apply.

C. Basic control and operation information describing how the airplane components controll and operate, including any special procedures, and limitations that apply.

A. The actuator travel is limited by the stroke of surface

B. The actuator move is limited by the move of surface

C. The actuator travel is limited by the move of surface

A. 距离皮托管中心线半径3英寸的修复表面轮廓外形,误差不应大于0.007英寸。

B. 距离静压盘中心线3英寸半径上的修复表面等高线,误差不应大于0.007英寸。

C. 静压孔中心线3英寸半径内的修复表面轮廓,误差不应大于0.007英寸。

A. After 10-flight cycles or 25 flight hours, which comes first the rod end bearing shall be discarded if its wear is greater than 0.010 inch of diameter.

B. If the rod end bearing wear is greater than 0.010 inch in radial play, reject it within newt 10 flight cycles or 25 flight hours whichever comes first.

C. Destroy the rod end bearing during 10 flight cycles or 2 flight hours when its wear is more than 0.010 inch of its radius, whichever comes first.

A. 列出了技术名称一个示例。

B. 列出的技术员名称只是示例。

C. 列出的技术名称只是示例。