A、 That portion of the system that uses radio/radar beam, heading and horizontal gyro, Pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes powering devices, interlocking devices and amplifying, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights , etc.
B、 That portion of the system that uses radio/radar beam, directional and vertical gyro, Pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes power source devices, interlocking devices and amplifying, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights, etc.
C、 That portion of the system that uses radio/radar beam, directional and vertical gyro, Pilot static and, manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes power source devices, locking devices and shrinking, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights, etc.
答案：B
A、 That portion of the system that uses radio/radar beam, heading and horizontal gyro, Pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes powering devices, interlocking devices and amplifying, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights , etc.
B、 That portion of the system that uses radio/radar beam, directional and vertical gyro, Pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes power source devices, interlocking devices and amplifying, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights, etc.
C、 That portion of the system that uses radio/radar beam, directional and vertical gyro, Pilot static and, manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes power source devices, locking devices and shrinking, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights, etc.
答案：B
A. Fill the accumulator with oil;
B. Recharge the accumulator with nitrogen;
C. Release oil from the accumulator;
A. 一百三十二是一个整数的例子。
B. 三十二分之一是一个分数的例子。
C. 一分三十二秒是一个剪辑的片段。
A. 在可能的地方,将分号从定义和核准示例文本中删除是可行的。
B. 在可能和不得已的情况下,将标记符号从定义和示范示例的文本中删除。
C. 在可能和可行的情况下,将引号从定义和批准示例的文本中删除。
A. ADVISE
B. SUGGEST
C. RECOMMEND
A. 功能测试足在较长维护期间内进行的测试。
B. 功能测试是在较短维护期间内进行的测试。
C. 功能测试是在定期维护期间内进行的测试。
A. The producer of the manual should make an arrangement for the material in the paragraphs in such a way that he thinks it will be most advantageous to the pilot who will use the manual.
B. The producer of the manual should make a layout of the material in the paragraphs under way as he thinks it will be most informing to the pilot who is going to use the manual.
C. The manual producer shall compile the content in each paragraph in the manner that he deems to be most practical to the pilot who intends to use the manual.
A. 小心修理损伤的零件。
B. 小心易损伤的零件。
C. 对于损伤的零件要小心。
A. 给出控制面板的原理图或图片。
B. 画出娱乐面板的示意图或图片。
C. 提供仪表板的图纸或图片。
A. 不要使用含油的溶剂
B. 使用不含油的溶剂。
C. 使用不含溶剂的油。
A. Tighten the nuts between 55 to 75 pound-inches due to ATA32-05-10.
B. Tighten the nuts between 55 to 75 pound-inches according to ATA32-05-1.
C. Tighten the nuts above 55 or 75 pound-inches according to ATA32-05-10.
