A、 Outside Air Temperature is the free air static temperature, obtained either from inflight temperature indications or ground meteorological sources, adjusted for instrument error and compressibility effects.
B、 Outdoor Air Temperature is the dynamic temperature of free air, obtained from flight temperature indications or ground meteorological sources and adjusted for instrumental error and compressibility effects.
C、 Outdoor Air Temperature is free air stagnation temperature, from flight temperature indicating or ground meteorological resource, and according to the instrument error and compressibility effects to adjust.
答案：A
A、 Outside Air Temperature is the free air static temperature, obtained either from inflight temperature indications or ground meteorological sources, adjusted for instrument error and compressibility effects.
B、 Outdoor Air Temperature is the dynamic temperature of free air, obtained from flight temperature indications or ground meteorological sources and adjusted for instrumental error and compressibility effects.
C、 Outdoor Air Temperature is free air stagnation temperature, from flight temperature indicating or ground meteorological resource, and according to the instrument error and compressibility effects to adjust.
答案：A
A. This Specification is designed to provide guidance for the development of Handbooks for all types of general aviation airplanes. These airplanes are originally certificated at minimum takeoff weights of 12,500 pounds or more.
B. This specification is intended to provide guidance for the development of Handbooks for all types of general aviation aircraft, which are initially certificated at maximum takeoff weights of 12,500 pounds or less.
C. This specification is intended to provide guidance for the preparation of Handbooks. For all types of general aviation aircraft, their maximum take-off weight is more than 12,500 pounds.
A. 评估一个事故造成的损伤。
B. 通过事件来检查一个损伤。
C. 事故后检查损伤。
A. An "Airplane Weighing Form" shall be included in each handbook and the form shall contain an airplane side view that shows the location of weighing points (using jacking points or landing gear) relative to the datum line.
B. Each handbook shall provide an aircraft side view that is included in an "Airplane Weighing Form" to show the position of weighing points (using jacking points or landing gear) related to the datum line.
C. An airplane three view that shows the weighing points ((using jacking points or undercarriage) relative to the datum line shall be excluded in an "Airplane Weighing Form" of each handbook.
A. Measure the Outside Air Temperature and the temperature in the cockpit with a thermometer.
B. Do the Outside Air Temperature and the temperature in the cabin with a barometer.
C. Measure the Surrounding Air Temperature and the temperature in the cockpit with a thermometer.
A. 描述飞机燃油系统时，应解释燃油测量系统并阐述检测和校对的需要。
B. 描述飞机燃油系统时，应解释燃油计量系统并阐述检查和修正的需要。
C. 描述飞机燃油系统时，应说明燃油测量系统并阐述监控和校正的必要性。
A. 螺旋桨的翻修必须与螺旋桨制造商提供的数据保持一致，并在常规的车间中完成。
B. 螺旋桨的修理必须在被批准的车间中，按照螺旋桨制造商提供的数据完成。
C. 螺旋桨的大修必须按照螺旋桨制造商提供的数据在合格的车间中完成。
A. According to instrument error and compressibility effects, Outside Air Temperature is corrected.
B. Outside Air Temperature is set to avoid instrument error and compressibility effects.
C. Due to instrument error and compressibility effects, Outside Air Temperature is modified.
A. 仔细评估损伤区域。
B. 仔细测量损伤区域。
C. 仔细评估磨损区域。
A. 结果是，孔的直径达到了允许的最大值。
B. 结果是，允许孔的尺寸超出最大范围。
C. 结果是，孔的尺寸大于允许的最大尺寸。
A. In designing schematic diagrams, it may be necessary to combine two aspects: specification necessary to make the diagram clear; And the similarity essential for ease of reading and understanding.
B. In designing schematic diagrams, it may be necessary to comprehend two aspects: detection necessary to make the diagram self-contained; And the simplification essential for ease of reading and understanding.
C. In designing schematic diagrams, it may be necessary to compromise two aspects: detail necessary to make the diagram self-explanatory; And the simplicity essential for ease of reading and understanding.
