飞行手册 目录
目 录
章 节 标 题 页码 I 操作限定...........................................................................................1-1 1-1
配重限定…........................................................................................1-1 1-1 “A”类 操作...................................................................................1-1 1-1 “B”类 操作...................................................................................1-1 1-1 重心(C.G.)限定..................................................................................1-1 1-1 装载限定...........................................................................................1-1 1-1 最大燃油流量速率引起的总重减少……….....………………….……………..1-5 1-5 操作类型...........................................................................................1-6 1-6 “A”类和“B”类操作........................................................................1-6 1-6 “B”类旋翼机–外部装载组合……..................................................1-6 1-6 最小飞行机组....................................................................................1-6 1-6 单个驾驶员(仪表飞行规则).........................................................1-6 1-6 两个驾驶员(仪表飞行规则).........................................................1-6 1-6 空速限定............................................................................................1-7 1-7 高度限定............................................................................................1-8 1-8 周围温度限定....................................................................................1-8 1-8 飞行限定............................................................................................1-8 1-8 电子飞行仪表系统(EFIS)限定...........................................................1-9 1-9 客舱滑动门限定................................................................................1-10 1-10 漂浮系统限定....................................................................................1-10 1-10 发动机限定........................................................................................1-11 1-11 发动机和驱动系统操作限定.......................................................1-13 1-13 发动机扭矩限定...........................................................................1-14 1-14 N1(气体发生器)速度限定............................................................1-14 1-14 N2(动力涡轮)速度限定................................................................1-15 1-15 T5 (动力涡轮)进气温度限定........................................................1-15 1-15 稳定状态限定...........................................................................1-15 1-15 起动和关车...............................................................................1-16 1-16 数字发动机控制单元(DECU)限定................................................1-16 1-16 燃油................................................................................................1-16 1-16 燃油添加剂...............................................................................1-17 1-17 燃油流量范围................................................................................1-17 1-17 发动机滑油....................................................................................1-18 1-18 发动机滑油温度限定....................................................................1-18 1-18 发动机滑油压力限定 ................................................................. 1-18 1-18 传动装置限定................................................................................... 1-18 1-18 扭矩限定...................................................................................... 1-19 1-19 双发操作.................................................................................. 1-19 1-19 单发失效操作 ........................................................................ 1-19 1-19 传动装置滑油.............................................................................. 1-19 1-19 传动装置滑油温度限定 ............................................................. 1-19 1-19 传动装置滑油压力限定 ............................................................. 1-19 1-19
i
1999年12月20日
SA 4047-76C-14 第一部分
飞行手册 目录
目 录
章 节 标 题 页码
旋翼限定 ...................................................................................... 1-20 1-20 动力断开 ................................................................................. 1-20 1-20 动力打开 ................................................................................. 1-20 1-20 旋翼刹车限定................................................................................ 1-20 1-20 旋翼旋转 ................................................................................. 1-20 1-20 旋翼停止 ................................................................................. 1-21 1-21 发动机整流罩限定 ...................................................................... 1-21 1-21 可收起式登机踏板限定................................................................ 1-21 1-21 紧急示位信标发射器 (ELT) ......................................................... 1-21 1-21 Bendix/King CAS-66A TCAS I交通防撞系统................................. 1-22 1-22 Primus 440 数字气象雷达系统................................................... 1-22 1-22 仪表标记 ..................................................................................... 1-22 1-22 标牌............................................................................................... 1-22 1-22
II 常规程序...................................................................................... 2-1 2-1
外部检查 ..................................................................................... 2-1 2-1 内部检查 ..................................................................................... 2-7 2-7 夜间飞行....................................................................................... 2-7 2-7 发动机起动前............................................................................... 2-7 2-7 起动发动机(电瓶或外接电源) .................................................... 2-13 2-13 特别检查....................................................................................... 2-20 2-20 滑行 ............................................................................................. 2-20 2-20 起飞前 ......................................................................................... 2-21 2-21 滑行和起飞 ................................................................................. 2-28 2-28 “A”类 起飞 ............................................................................. 2-33 2-33 “B”类 起飞 ............................................................................. 2-33 2-33 爬升............................................................................................... 2-34 2-34 巡航 ............................................................................................. 2-34 2-34 着陆前 ......................................................................................... 2-34 2-34 进近和着陆 ................................................................................. 2-35 2-35 下滑道 .................................................................................... 2-35 2-35 复飞 ........................................................................................ 2-35 2-35 关车前........................................................................................... 2-36 2-36 关车............................................................................................... 2-36 2-36 关车后 ......................................................................................... 2-37 2-37 可选操作程序............................................................................... 2-37 2-37 发动机灭火器系统测试............................................................... 2-37 2-37 浮筒系统测试............................................................................... 2-38 2-38 燃油供油程序－正常起动时....................................................... 2-39 2-39 导航测试电门功能....................................................................... 2-40 2-40 功能检查– 防雪组件件号76076-30008-012............................. 2-41 2-41 功能检查– 可收起式登机踏板................................................... 2-422-42
ii
1999年12月20日
SA 4047-76C-14 第一部分
飞行手册 目录
目 录
章 节 标 题 页码
功能检查– 紧急示位信标发射器 (ELT)……………….………………….. 2-42 2-42 操作.......................................................................................... 2-42 2-42 大气数据存取单元....................................................................... 2-43 2-43 操作.......................................................................................... 2-43 2-43 Litef LCR-92S 姿态航向基准系统(AHRS) .................................... 2-44 2-44 操作.......................................................................................... 2-44 2-44 Pulselite系统 .............................................................................. 2-45 2-45 操作.......................................................................................... 2-45 2-45 识别灯 ......................................................................................... 2-45 2-45 操作.......................................................................................... 2-45 2-45 客舱照明控制系统 ..................................................................... 2-46 2-46 操作.......................................................................................... 2-46 2-46 标识灯系统 ................................................................................. 2-46 2-46 操作.......................................................................................... 2-46 2-46 固定着陆灯 ................................................................................. 2-46 2-46 操作.......................................................................................... 2-46 2-46 Collins ALT-50和ALT-55B无线电高度系统地面测试................. 2-47 2-47 Bendix/King CAS-66A交通防撞系统功能测试……………………………2-48 2-48
III 应急程序 ..................................................................................... 3-1 3-1
引言 ............................................................................................. 3-1 3-1 发动机系统故障 ......................................................................... 3-2 3-2 单发功率故障............................................................................... 3-2 3-2 有除冰功能的单发功率故障...... ………………………………………….3-3 3-3 单发故障－悬停(5至10英尺)............................................... 3-3 3-3 起飞时单发故障 － “A”类 .................................................... 3-3 3-3 到达30节前........................................................................ 3-3 3-3 30节后到CDP前包括CDP，轮高5-10英尺.................... 3-3 3-3 CDP后（5-10英尺轮高）.................................................. 3-4 3-4 起飞时单发故障 － \"B\"类 .................................................... 3-5 3-5 巡航时单发故障....................................................................... 3-5 3-5 飞行中发动机重启............................................................... 3-6 3-6 发动机失效后燃油交注....................................................... 3-7 3-7 飞行中发动机关车…………………………………………………………….3-8 3-8 进近时单发故障 － “A”类…………………………………………………... 3-8 3-8 LDP或之前—中断降落（复飞）…………………………….......... 3-8 3-8 LDP之后................................................................................ 3-8 3-8 单发着陆 － “A”类或\"B\" ......................................................... 3-8 3-8 进近时单发故障 – 备用“A”类................................................. 3-9 3-9 降落决策点之前- 中断着陆(复飞)...................................... 3-9 3-9 LDP之后................................................................................ 3-103-10
iii
2008年11月25日
SA 4047-76C-14 第一部分
飞行手册 目录
目 录
章 节 标 题 页码
单发着陆 – 备用“A”类剖面图………………………………………………3-10 3-10 双发故障....................................................................................... 3-10 3-10 概述.......................................................................................... 3-10 3-10 悬停时或10英尺高度以下起飞时双发故障......................... 3-11 3-11 起飞或开始爬升时双发故障 ................................................. 3-11 3-11 巡航时双发故障....................................................................... 3-11 3-11 自转着陆....................................................................................... 3-12 3-12 发动机控制设备故障 .................................................................. 3-13 3-13 一台发动机DECU严重故障（DECU MAJOR）..................... 3-13 3-13 起飞中.................................................................................. 3-14 3-14 巡航中.................................................................................. 3-15 3-15 进近或着陆过程中“DECU MAJOR”故障........................... 3-15 3-15 双发数字发动机控制单元全部故障 ..................................... 3-16 3-16 DECU性能下降（DECU DGRAD）…………….......................... 3-17 3-17 DECU小故障（minor）… ....................................................... 3-18 3-18 发动机控制设备性能变化....................................................... 3-19 3-19 有动力飞行中，发动机超速告诫灯亮....................................... 3-19 3-19 发动机辅助系统故障 .................................................................. 3-20 3-20 发动机滑油系统故障............................................................... 3-20 3-20 燃油压力警告灯亮.................................................................. 3-20 3-20 燃油过滤警告灯亮 ................................................................ 3-21 3-21 燃油流量超出正常范围 ........................................................ 3-21 3-21 防冰警告灯亮 ........................................................................ 3-21 3-21 电子飞行仪表系统(EFIS)故障...................................................... 3-23 3-23 发动机仪表故障 ......................................................................... 3-23 3-23 N1指示器故障 ....................................................................... 3-23 3-23 T5指示器故障 ........................................................................ 3-23 3-24 发动机碎片探测器警报灯亮 ..................................................3-24 3-24 主变速箱系统故障........................................................................ 3-24 3-24 主变速箱滑油系统故障............................................................ 3-25 3-25 主变速箱滑油泵故障............................................................ 3-25 3-25 中减或尾减探测到金属屑/滑油温度高........................................ 3-26 3-26 旋翼刹车警告灯亮－旋翼转动 .................................................... 3-27 3-27 飞行控制液压伺服系统故障 ....................................................... 3-27 3-28 主液压系统油泵故障或压力丧失............................................. 3-28 3-28 尾旋翼伺服系统液压压力丧失................................................. 3-28 3-28 伺服装置卡住或伺服关闭活门故障 ……………………………………. 3-30 3-30 飞行控制阻尼卡住 ....................................................................... 3-31 3-31 尾旋翼故障..................................................................................... 3-32 3-32 前飞中尾旋翼驱动系统故障 .................................................. 3-32 3-32 悬停中尾旋翼驱动系统故障 .................................................. 3-32 3-32 尾旋翼控制系统故障 .............................................................. 3-32 3-33
iv
1999年12月20日
SA 4047-76C-14 第一部分
飞行手册 目录
目 录
章 节 标 题 页码
桨距固定—一般情况…………………………………………………….……3-33 3-33 桨距固定—低功率………………………………………………………………3-33 3-33 大功率时桨距固定………………………………………………………………3-33 3-33 巡航功率时桨距固定………………………………………………..………..3-34 3-34 尾桨钢索失效—中立弹簧起作用…………………………………..….3-34 3-34 着陆程序—尾桨控制钢索失效，中立弹簧起作用……….….3-34 3-34 尾桨受损……………………………………………………………………………….….3-35 3-35 火警................................................................................................. 3-35 3-35 发动机机舱失火 ...................................................................... 3-35 3-35 关车后发动机内部起火 ........................................................... 3-36 3-36 客舱或驾驶舱失火..................................................................... 3-36 3-36 已探明行李舱烟雾 ................................................................... 3-37 3-37 烟雾和烟气消除.............................................................................. 3-37 3-37 电器着火 ........................................................................................ 3-37 3-37 起落架故障 .................................................................................... 3-38 3-38 起落架不能放下......................................................................... 3-40 3-40 不安全指示－放起落架 ........................................................... 3-40 3-40 不安全指示－收起落架............................................................. 3-41 3-41 电器系统故障 ................................................................................ 3-42 3-42 电瓶超温...................................................................................... 3-42 3-42 馈电故障.................................................................................... 3-42 3-42 一台直流发动机故障.................................................................. 3-42 3-42 两台直流发动机故障 ............................................................... 3-43 3-43 直流发电机超温......................................................................... 3-45 3-45 直流重要设备汇流条馈电故障.................................................. 3-46 3-46 变流机故障 ............................................................................... 3-47 3-47 交流发动机故障......................................................................... 3-47 3-47 交流发电机轴承故障.............................................................. 3-48 3-48 各种系统故障或事故征候 .............................................................. 3-48 3-48 数字自动飞行控制系统 ............................................................. 3-49 3-49 自动驾驶 ................................................................................ 3-49 3-49 飞行指引仪 ............................................................................ 3-50 3-50 大气数据故障 ........................................................................ 3-51 3-51 总距杆 .................................................................................... 3-51 3-51 各种故障.................................................................................. 3-52 3-52 驾驶员音频设备................................................................. 3-52 3-52 磁刹失效（驾驶杆）......................................................... 3-52 3-52 应急电瓶指示器................................................................. 3-53 3-53
空速管加热告诫灯亮........................................................................ 3-53 3-53 风挡热告诫灯 ................................................................................. 3-54 3-54 紧急出入口和出口........................................................................... 3-54 3-54 铰链式舱门................................................................................. 3-543-54
v
1999年12月20日
SA 4047-76C-14 第一部分
飞行手册 目录
目 录
章 节 标 题 页码
舱门抛掷程序..................................................................... 3-55 3-55 滑动舱门(选装)........................................................................ 3-55 3-55 门窗抛掷程序....................................................................... 3-55 3-55 飞行中滑动门打开.............................................................. 3-55 3-55 可收起式登机踏板 ...................................................................... 3-56 3-56 水上迫降(有浮筒系统) ................................................................. 3-56 3-56 水上迫降程序 ......................................................................... 3-59 3-59 水上单发着陆(浮筒装置充气)................................................ 3-60 3-60 水上自转降落……. .................................................................... 3-61 3-61 LITEF LCR-92S 姿态航向基准系统 (AHRS)................................... 3-61 3-61 丧失26 Vac基准 ................................................................... 3-62 3-62 丧失26 Vac高度基准.............................................................. 3-62 3-62 丧失26 Vac航向基准 ............................................................. 3-62 3-62 水上迫降(没有浮筒系统) ........................................................ 3-63 3-63 综合仪表显示系统显示故障......................................................... 3-63 3-63 无线电主系统 ............................................................................. 3-64 3-64
IV 性能资料
性能图表目录............................................................................... 4-1 4-1 噪音水平检定................................................................................. 4-6 4-6 发动机状况……… ............................................................................. 4-6 4-6 防冰对性能影响 ............................................................................. 4-7 4-7 “A”类起飞 ........................................................................................ 4-7 4-7 描述 ........................................................................................... 4-9 4-9 操作方法..............................................…….................................. 4-9 4-9 相关条件.................................................................................... 4-9 4-9 “A”类着陆........................................................................................ 4-21 4-21 相关条件..................................................................................... 4-21 4-21 着陆距离...................................................................................... 4-21 4-21 备用“A”类着陆方法 ...................................................................... 4-21 4-21 相关条件...................................................................................... 4-21 4-21 着陆距离....................................................................................... 4-21 4-21 “B”类起飞 ........................................................................................ 4-25 4-25 技术............................................................................................... 4-25 4-25 相关条件....................................................................................... 4-25 4-25 起飞距离 ..................................................................................... 4-25 4-25 “B”类着陆 ........................................................................................ 4-25 4-25 技术.............................................................................................. 4-25 4-25 相关条件...................................................................................... 4-25 4-25 着陆距离...................................................................................... 4-254-25
vi
2008年11月25日
SA 4047-76C-14 第一部分
飞行手册 目录
插图列表
图编号 标题 页码
1-1 “A”类最大起飞着陆总重………………................................. 1-2 1-2 1-2 “B”类最大起飞着陆总重…………….................................... 1-3 1-3 1-3 不同总重时的重心限定...................................................... 1-4 1-4 1-4 高度/速度表 ...................................................................... 1-12 1-12 1-5 仪表标记……………………………………………............................... 1-24 1-24 1-6 不可超越速度(Vne)标牌……………..…................................... 1-28 1-28 2-1 功率保障检查…………………………………………………………………...2-29 2-29 2-2 T5余度检查图表……………………………………………………………….2-32 2-32 3-1 电器火警程序，仪表气象条件.......................................... 3-39 3-39 3-2 数字自动飞行控制系统警告面板...................................... 3-48 3-48 3-3 紧急出入口……………………………………………………………........... 3-57 3-57 4-1 密度高度表.......................................................................... 4-2 4-2 4-2 温度换算表.......................................................................... 4-3 4-3 4-3 空速校准－驾驶员系统 .................................................... 4-4 4-4 4-4 空速校准－副驾驶系统 .................................................... 4-5 4-5 4-5 “A”类 起飞剖面图............................................................... 4-10 4-10 4-6 风分量 ................................................................................ 4-11 4-11 4-7 “A”类中断起飞和距离和继续起飞距离............................. 4-12 4-12 4-8 “A”类最大起飞和着陆总重................................................. 4-13 4-13 4-9 向前爬升性能－单发2分钟功率...................................... 4-14 4-14 4-10 “A”类起飞飞行轨迹)............................................................ 4-15 4-15 4-11 向前爬升性能－单发最大连续功率................................... 4-20 4-20 4-12 “A”类着陆剖面图 ............................................................... 4-22 4-22 4-13 “A”类备用着陆剖面图 ....................................................... 4-23 4-23 4-14 “A”类着陆距离 ................................................................... 4-24 4-24 4-15 “B”类 起飞剖面图.............................................................. 4-26 4-26 4-16 “B”类 起飞距离……………….......................................... 4-27 4-27 4-17 “B”类 起飞顶风影响 ........................................................ 4-28 4-28 4-18 向前爬升性能－双发最大连续功率.................................. 4-29 4-29 4-19 向前爬升性能－双发正常巡航功率.................................. 4-30 4-30 4-19 “B”类着陆剖面图 .............................................................. 4-31 4-31 4-20 “B”类着陆距离 .................................................................. 4-32 4-32 4-21 起飞功率时无地效悬停……….….………….................... 4-33 4-33
vii
1999年12月20日
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