A、 如果这个部件应该纳入CAP,那么使用最终数据做出判断。
B、 公司应利用现有数据判断该部件是否与CAP相关联。
C、 已用所得数据来确定是否应将该部件纳入CAP。
答案:C
A、 如果这个部件应该纳入CAP,那么使用最终数据做出判断。
B、 公司应利用现有数据判断该部件是否与CAP相关联。
C、 已用所得数据来确定是否应将该部件纳入CAP。
答案:C
A. 每个主燃油箱的通气油箱外侧控制溢出的燃油和排气系统中的燃油。
B. 每个主燃油箱外侧的通气油箱收集溢出的燃油和来自排气系统中的燃油。
C. 每个主燃油箱的通气油箱从外侧防止排气系统中的燃油溢出。
A. Check left engine inboard wing leading edge if have damage and dent before the aircraft takes off.
B. Check wing leading edge inboard left engine for damage and dent before the aircraft takes off.
C. Check the wing leading edge of left engine inboard for damage and dent before the aircraft takes off.
A. 改变面板的位置。
B. 将面板移动到位。
C. 将脚蹬移动到位。
A. 某些词会有注释告诉你使用其他批准的专用词汇或不同的形式。
B. 某些词会有注释告诉你使用其他批准的更佳的词汇或不同的结构。
C. 某些词会有注释告诉你使用其他批准的替代词汇或不同的形式。
A. Ensure that the label adheres tightly to the surface and that no bubbles are present.
B. Verify the full attachment of the label to the surface and accept the presence of bubbles.
C. Make sure the label is partially attached to the surface, ensuring there are no bubbles present.
A. Maximum attitude for flight planning will be affected.
B. Maximum altitude for flight planning will be affected.
C. Maximum attitude for flight planning will be effected.
A. For all fuel loadings, the initial airplane weight should be the maximum allowable.
B. The initial airplane weight should contain the maximum allowable for all fuel loads.
C. For all kinds of fuels, the initial aircraft weight should be the maximum allowable.
A. The section of the engine which contains the sleeve, master and link rod assemblies, cams, cam drive gears, tappet guides, rollers, carriers, etc.
B. The section of the engine which contains the crankshaft, master and link rod assemblies, cams, cam drive gears, tappet guides, rollers, carriers, etc.
C. The section of the engine which contains the crankshaft, master and manifold assemblies, cams, cam drive gears, tappet guides, rollers, carriers, etc.
A. 保护漆将防止腐蚀达6个月。
B. 保护涂层将防止锈蚀达6个月。
C. 保护漆将保护腐蚀达6个月。
A. The Specification provides flexibility in Handbook preparation based on the complexity of the airplane while maintaining a high degree of standardization of arrangement, definitions, and performance information.
B. The Specification provides flexibility in Handbook preparation based on the complicacy of the airplane, but ignoring a high degree of standardization of structure, definitions, and performance information.
C. The Specification provides uniformity in Handbook preparation based on the simplicity of the airplane while retaining a high degree of standardization of arrangement, definitions, and performance information.