飞行手册翻译作业..docx

飞行器设计与工程 专业英语阅读（三） 期末大作业 班级：1315071 学号：131507137 姓名：张世秋 日期：２０１６年１０月２8日 目录 TOC \o 1-3 \h \z \u HYPERLINK \l _Toc465275426 第25章703节 起飞警告系统 PAGEREF _Toc465275426 \h 1 HYPERLINK \l _Toc465275427 第25章721节 起落架总论 PAGEREF _Toc465275427 \h 3 HYPERLINK \l _Toc465275428 第25章723节 撞击吸收测试 PAGEREF _Toc465275428 \h 5 HYPERLINK \l _Toc465275429 第25章729节 收放机械装置 PAGEREF _Toc465275429 \h 7 HYPERLINK \l _Toc465275430 第25章731节 机轮 PAGEREF _Toc465275430 \h 12 HYPERLINK \l _Toc465275431 第25章733节 轮胎 PAGEREF _Toc465275431 \h 13 HYPERLINK \l _Toc465275432 第25章735节 刹车和制动系统 PAGEREF _Toc465275432 \h 17 PAGE \* MERGEFORMAT4 CS 25.703 Take-off warning system (See AMC 25.703) 第25章703节 起飞警告系统 A take-off warning system must be installed and must meet the following requirements: 起飞警告系统必须安装且满足如下要求： The system must provide to the pilots an aural warning that is automatically activated during the initial portion of the take-off roll if the aero plane is in a configuration, including any of the following that would not allow a safe take-off: 在起飞滑跑的最初阶段，如果飞机的（舵面）布局包括以下情况中的任何一种时，该系统必须可以以声音的形式自动警告飞行员。 The wing-flaps or leading edge devices are not within the approved range of take-off positions. 襟翼前缘增升装置的转角不在安全起飞所允许的范围内。 Wing spoilers (except lateral control spoilers meeting the requirements of CS 25.671), speed brakes, or longitudinal trim devices are in a position that would not allow a safe take-off. 机翼的扰流器（除了后面为满足第25章671节控制扰流器外），速度刹车器，或者纵向的减阻装置，不在安全起飞所允许的位置。 The parking brake is unreleased. 停机刹车器未被释放。 The aural warning required by sub- paragraph (a) of this paragraph must continue until – （a）段中声音警告应该一直持续到下面段的情况得到满足时— The take-off configuration is changed to allow a safe take-off? 起飞的（舵面）布局被改变，满足安全起飞要求。 Action is taken by the pilot to terminate the take-off roll? 飞行员采取措施终止了滑跑起飞。 The aero plane is rotated for take- off? or 飞机转换起飞滑跑状态，或者是 The warning is manually silenced by the pilot. The means to silence the warning must not be readily available to the flight crew such that it could be o