B737NG ATA章节中英文对照表

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B737NG训练手册-中文版 32-09-00_空地系统

有效性 YE201
R RA REF SBRK SMYD sys sw TCAS TE T/O V VHF VOR WW WX
—右 — 无线电高度表 — 基准 — 速度刹车 — 失速管理偏航阻尼器 — 系统 — 电门 — 空中交通防撞系统 — 后缘 — 起飞 — 伏特 — 甚高频 — 甚高频全向信标 — 轮舱 — 气象雷达
当地面扰流板在不安全状态打开时，速度刹车打开指示系统点亮速度刹车伸出（SPEEDBRAKES EXTENDED）灯。参阅速度刹车控制系统部分可得关于琥珀色速度刹车伸出（SPEEDBRAKES EXTEDED）灯的详细信息。
飞机起飞警告系统在起飞前（在地面）或起飞后（在空中），当飞机处于不安全状态时启动音响警告喇叭。参阅起飞警告系统可得关于起飞警告系统的详细信息。（AMM 第 I 部分分 31—53）
位置
前起落架压缩传感器位于上扭力臂连接到前起落架外筒部位的两侧。目标位于前起落架外筒的下部区域。
传感器托架上的传感器标识牌显示传感器号码。下面是前起落架压缩传感器号码：
传感器号码
位置
S1014
左
S1015
右
位于前起落架轮舱左墙上的接线盒内有两个传感器线缆的接头。
功能介绍
当前起落架减震支柱压缩时，目标接近传感器。当飞机在地面时向接近电门电子组件内的空/地系统发送信号。
空/地系统 — 介绍
目的
空/地系统为许多飞机系统提供离散信号。
接近电门电子组件（PSEU）是空/地系统的一个部件。许多飞机系统通过传感器和电门向 PSEU 发送信号。PSEU 控制空/地继电器（12）。
下面是接近电门电子组件（PSEU）控制的系统/部件：
— 起落架转换活门 — 起落架位置指示和警告 — 速度刹车打开指示 — 起飞警告 — 舱门警告 — 空/地继电器

波音737NG机型ATA中文手册电源部分

电源－介绍目的电源系统可进行发电，供电及控制等功能。

系统有自动和人工控制两种方法，机内测试设备（BITE ）和备用电源可使系统保持较高可靠性。

电源系统有如下子系统：－发电机传动－交流发电－直流电－外部电源－交流电载荷分配缩略语AGCU － APU 发电机控制组件 AGB －附件齿轮箱altn －备用APB － APU 断路器APS － APU 电源电门 APU －辅助动力装置 ASG － APU 起动机－发电机 auto －自动bat －电瓶BPCU －汇流条电源控制组件 BTB －汇流条断路器 CSD －恒速传动装置CT －电流变压器 chgr －充电器disc －断开DEU －显示电子组件 DPCT －差动保护电流变压器 EEC －电子发动机控制 EP －外部电源EPC －外部电源接头flt －飞行fltr －油滤F/O －副驾驶GCB －发电机控制断路器 GCR －发电机控制继电器 GCU －发电机控制组件 gen －发电机gnd －地面grd －地面GSTR －地面勤务转换继电器 IDG －整体传动发电机j －接头LRU －航线可更换组件 NCT －中线电流变压器 PDP －电源分配面板 PMG －水磁发电机pwr －电源QAD －快速拆装rly －继电器RMS －均方根值RTL －准备加载24—00—00—000 R e v 4 07/08/1999电源－介绍scav －回油，清除SCU －起动交流机组件 sect －节，段SPCU －备用电源控制组件 SPU －起动电源组件 srvce －服务 stdby －备用 sys －系统 thrm －热TRU －变压整流器组件 VR －电压调节器 xfr－变压器24—00—00—000 R e v 4 07/08/199924—00—00—000 R e v 4 09/12/2000交流电负载分配电源－介绍外部电源直流电电源交流发电发电机传动电源－电源和控制－概况介绍本页空白24—00—00—001 R e v 3 02/19/1998电源－电源和控制－概况介绍目的电源系统为飞机提供交流和直流电，系统有自动和人工控制和保护。

B737NG训练手册-中文版 34-57-00_自动定向机系统

— 为 RF 组件产生自动增益控制（AGC） — 台站音频过滤 — 莫尔斯码语音探测 — 监控 BITE — 根据来自 ADF 控制面板的调谐数据为合成器编程。
方位、音频和莫尔斯码标识符数据从信号处理器到达 486 处理器。双口 RAM 作为两个处理器间的数据连接。486 处理器处理来自信号处理器的 BIT 数据用于在前面板上显示信息。它同时提供到输入／输出（I／O）部分的数据和控制信号。该处理器控制 ADF 接收机的所有主要功能。它也提供到内存和数据记录／数据装载闪存卡装置的接口。处理器在将来自信号处理器的方位数据输出到外部系统之前执行 QEC 和上／下补偿。
ADF 接收机计算相对于 ADF 地面站的方位并将它发送到 DEU 用于显示。ADF 方位同时送到无线电磁指示器（RMI）。ADF 接收机处理来自地面站的音频信号并把它送到遥控电子组件（REU）。
34—57—00—002 Rev 13 10/02/2000
有效性
控制面板
ADF 控制面板输入
ADF 接收机系统处理器在一条 ARINC 429 数据总线上接收来自 ADF 控制面板的人工调谐输入和控制面板模式选项。
PSEU
接近电门电子组件（PSEU）向系统处理器发一个空／地离散信号。该离散信号为故障存储器设置飞行阶段计数。
程序销钉输入
ADF 接收机从一个插座电门接收程序销钉离散信号。方位计算机电路使用象限误差修正（QEC）程序销钉输入来调整由飞机结构引起的信号失真。
描述
天线组件是一片模制壳。天线用 12 个螺栓连接到飞机上。天线组件包含下列部件：
— 环形天线组件（2） — 垂直天线（1） — 电子组件
ADF 天线电子组件包含每个天线组件的放大器。放大器接收来自 ADF 接收机的 12V 直流电源。

B737CL ATA章节中英文对照表

设备和装饰
10 FLIGHT COMPARTMENT
驾驶舱
11 FLIGHT COMPARTMENT EQUIPMENT
驾驶舱设备
20 PASSENGER COMPARTMENT
客舱
21 PASSENGER CABIN LINING AND INSULATION 客舱衬里和隔热棉
22 SEATS - PASSENGER
垂直安定面和方向舵站位图表
42
HORIZONTAL STABILIZER AND ELEVATOR STATION DIAGRAM
水平安定面和升降舵站位图表
52 WING STATION DIAGRAM
大翼站位图
62 ENGINE AND NACELLE STATION DIAGRAM
发动机和吊舱站位图
飞行管理系统自测试设备
02
FLIGHT MANAGEMENT COMPUTER SYSTEM BUILT-IN TEST EQUIPMENT
飞行管理计算机系统自测试设备
03
DIGITAL FLIGHT CONTROL SYSTEM - BUILT- 数字式飞行控制系统自测试设
IN TEST EQUIPMENT
接近门和盖板
31 ACCESS DOORS AND PANELS -
接近门和盖板识别
32 LATCHES
锁扣
33 COLD WEATHER MAINTENANCE
寒冷天气维护
40 CLEANING AND WASHING
清洁和盥洗
00 STANDARD PRACTICES
标准施工
09 FLOOR PANEL
客舱座椅
23 SERVICE UNITS

B737NG训练手册-中文版 34-46-00_近地警告系统

语音报数 — 方式 7 — 风切变的警告
除了 1 — 7 方式以外，还有两种附加功能：
— 地形净空基底 — 进近中下降过界 — 地形觉察 — 显示飞机周围的地形
缩略语
ADI ADIRU alt AOA approx BITE capt DEU DFCS FDAU FMC F/O FPM FPS GND PROX GPS GPWC GPWM
34—46—00—002 Rev 10 12/19/2000
飞行管理计算机系统（FMCS）
有效性 YE201
数字式飞行控制系统方式控制板（MCP）
近地警告计算机（GPWC）
GPWS — 概述
避撞计算机
远距电子组件（REU）
34—46—00
GPWS — 驾驶舱内的部件位置
驾驶舱部件位置
以下 GPWS 部件为在驾驶舱内的： — 机长和副驾驶的下滑禁止电门 — 近地警告模件板
有效性
YE201
34—46—00
34—46—00—005 Rev 11 12/19/2000
有效性 YE201
115 交流转换汇流条
近地警告
1 号 28 伏直流汇流条
地形显示
P—18 板跳开关板
地形/气象继电器
地形/气象继电器
起落架位置起落架手柄电门模件
测试起落架禁止
襟翼禁止地形禁止
mod
— 组件、模数
ND
— 导航显示器
ovrd
— 超控
P
— 压下
PFD
— 主飞行显示器
pos
— 位置
PSEU
— 接近电门电子组件
PWS
— 预测风切变
RA
— 无线电高度

B737点火系统维修手册英文翻译

B737 Ignition1.IGNITION – INTRODUCTION2.IGNITION - GENERAL DESCRIPTION3.IGNITION - ENGINE COMPONENT LOCATION4.IGNITION - FLIGHT COMPARTMENT COMPONENT LOCATIONS5.IGNITION - IGNITION EXCITER6.IGNITION - DISTRIBUTION - IGNITION LEADS AND SPARK IGNITERS7.IGNITION - FUNCTIONAL DESCRIPTION8.IGNITION – OPERATION9.IGNITION - TRAINING INFORMATION POINTIGNITION - INTRODUCTIONGeneralThe ignition systems supply electrical sparks in the combustion chamber for combustion. Each engine has two ignition systems that operate independently. The ignition system usually operates manually. However, the ignition systems operate automatically when the electronic engine control (EEC) sees a possible engineflameout condition.You use ignition during these times:1. Ground start2. Takeoff and landings3. In-flight (during heavy turbulence or bad weather)4. In-flight start.Abbreviations and Acronyms1. CDS - common display system2. CDU - control display unit3. CONT - continuous4. DEU - display electronics unit5. EEC - electronic engine control6. FLT - flight7. FMC - flight management computer8. GRD - ground9. IGN - ignition10. L - left11. R – rightIGNITION - INTRODUCTIONIGNITION - GENERAL DESCRIPTIONGeneralThese components control ignition:1. Start levers2. Start switches3. Ignition selector switch4. Electronic engine control (EEC).The start lever controls ignition system power to the EEC. The start switch and the ignition selector switch supply inputs to the EEC. The EEC uses these inputs to supply power to the ignition exciters. The ignition exciters supply power to the spark igniters.The engine starting system also uses the switch positions for control.See the engine starting chapter for more informationElectrical PowerThe engine 1 ignition systems receive 115v ac from ac transfer bus 1 and the ac standby bus. The EEC has internal switches that control the 115v ac to the ignition exciters. The ignition exciters change the 115v ac input to a dc voltage ofapproximately 15,000 to 20,000v for the spark igniters. The spark igniters give a spark for combustion. The ignition systems of engine 2 receive ac power from ac transfer bus 2 and the ac standby bus.IGNITION - GENERAL DESCRIPTIONIGNITION - ENGINE COMPONENT LOCATIONGeneralEach engine has a right and a left ignition system. These are the components of each ignition system:1. Ignition exciter2. Ignition lead3. Air manifold4. Spark igniter.Component LocationsThe ignition exciters are on the right side, lower portion, of the fan case.The ignition leads go from the ignition exciters to the spark igniters on the right and left sides of the engine.The air manifold goes around the ignition leads. The air manifold starts in the 6:00 strut and goes to the igniters.The spark igniters are just forward of the fuel manifold, at the 4:00 position and the 8:00 position.IGNITION - ENGINE COMPONENT LOCATIONIGNITION - FLIGHT COMPARTMENT COMPONENT LOCATIONS GeneralThese components which control the ignition system are in the flight compartment:1. Engine start switches2. Ignition selector switch3. Start levers.Component LocationsThe ignition selector switch and engine start switches are on the forward overhead panel (P5).The start levers are on the control stand.IGNITION - FLIGHT COMPARTMENT COMPONENT LOCATIONSIGNITION - IGNITION EXCITERPurposeThe ignition exciters supply power to spark igniters.GeneralThe ignition exciters change 115v ac to 20,000v dc. The output of the ignition exciter is 14.5 to 16 joules. The spark igniter uses this power to ignite the fuel/air mixture in the combustion chamber. Usually, only one ignition exciter per engine operates at a time.Physical DescriptionA 115v ac electrical connector attaches to the forward face of the ignition exciter. The ignition lead attaches to the aft face of the ignition exciter.The ignition exciters attach to the fan case with four shockmounts.Each ignition exciter has a bond jumper that attaches to the engine.Training Information PointWARNING: MAKE SURE THAT THE IGNITION EXCITERS ARE DE-ENERGIZED FOR A MINIMUM OF FIVE MINUTES BEFORE YOU STARTWORK ON THE IGNITION SYSTEM. THE IGNITION SYSTEM VOLTAGE IS DANGEROUSLY HIGH. DO NOT TOUCH THE ELECTRICAL CONTACTS. THE IGNITION EXCITERS CAN HA VE AN ELECTRICAL CHARGE EVEN WHEN NOT ENERGIZED. IF YOU DO NOT OBEY THIS STEP, INJURY TO PERSONS CAN OCCUR.IGNITION - IGNITION EXCITERIGNITION - DISTRIBUTION - IGNITION LEADS AND SPARK IGNITERS PurposeThe spark igniters supply an electrical spark to ignite the fuel/air mixture in the combustion chamber.The ignition leads transmit power from the ignition exciters to the spark igniters. General DescriptionEach spark igniter has its own ignition lead. Air goes around each ignition lead to decrease the temperature of the lead.Ignition Lead CoolingEach ignition lead goes into an air manifold at the 6:00 position at the aft end of the fan case. Booster air (low pressure compressor exhaust air), makes each ignition lead cool. The booster air goes into the air manifold and moves around the inner partof the ignition lead shroud. Booster air comes out of the spark igniter end of the ignition lead to cool the spark igniter.Spark IgnitersEach spark igniter installs into an adapter at the 4:00 and 8:00 positions on the engine. The spark igniter electrode is inside the combustion chamber.IGNITION - DISTRIBUTION - IGNITION LEADS AND SPARK IGNITERSIGNITION - FUNCTIONAL DESCRIPTIONGeneralThese are the components that operate the ignition system:1. Start levers2. Engine start switches3. Ignition selector switch4. EEC.The ac transfer bus 1 supplies 115v ac electrical power to the EEC for the left ignition exciter. The ac standby bus supplies 115v ac electrical power to the EEC for right ignition exciter. The left ignition exciter for engine 2 uses power from ac transfer bus 2. The right ignition exciter uses the ac standby bus.The EEC controls power to the ignition exciters. Input from the flight compartment components give manual control. The EEC has internal logic forautomatic ignition system control.Manual ControlThe EEC and the CDS/DEUs monitor the position of these flight compartment components:1. Ignition selector switch2. Engine start switches3. Start levers.Each CDS/DEU sends a digital data signals to the EEC with switch position information.The EEC looks at the CDS/DEU digital data signal and the analog signal. The EEC compares the two signals. If the CDS/DEU 1 or CDS/DEU 2 digital data signal to the EEC logic stops, the EEC uses the analog signal as the flight compartment input.The EEC uses switch position data to control four internal EEC ignition on/off switches. These switches control the 115v ac power to the ignition exciters. Each EEC channel (A and B) controls one ignition on/off switch to each ignition exciter. Only one EEC channel is active at a time. Therefore, only one ignition on/off switch, for an ignition exciter, works at a time. The other EEC channel is in the standby mode. 115v ac power goes to the EEC when you move the start lever to the idle position. The 115v ac power goes through the start lever switches that are in the closed position.The ignition exciters receive power and supply 15,000 to 20,000v dc of electrical power to the spark igniters. The voltage goes across the electrodes of the spark igniter to make sparks.Flameout ProtectionThe EEC turns on both ignition systems of an engine automatically if one of these conditions are true:1.The engine start lever is in the IDLE position, the start switch is in the FLTposition2.The engine start lever is in the IDLE position, start switches in GRD or CONTposition, N2 less than idle and the airplane is in flight3.The engine start lever is in the IDLE position, engine speed decreasesuncommanded or N2 is less than 57% and N2 is more than 50%. For this condition only, both ignition systems are energized for 30 secondsGUN 001-099, 101-122, 155-157The engine start lever is in the IDLE position, the airplane is in flight, start switch is in the OFF position, N2 speed is less than idle, and N2 speed is more than 5%.GUN 201-999The engine start lever is in the IDLE position, the airplane is in flight, start switch is in the AUTO position, N2 speed is less than idle, and N2 speed is more than 5%.GUN ALLThe EEC turns ignition off when these conditions are true:1. Engine start switches are not in a position that command ignition operation2. Hot start on the ground3. Wet start on the ground4. The engine start lever is in the IDLE position, airplane is on the ground, the engine completed a start, N2 speed goes less than 50% and EGT is more than the start limit5. Ignition system energized because of N2 less than idle or uncommanded decrease in N2 and engine speed goes back to normal.GUN 201-999Automatic IgnitionThe EEC turns on the selected igniter(s) when the flaps are not up or the engine anti-ice is selected on. To keep ignitors off when they are not needed or have no effect, more EEC logic is used to turn ignitors on when all of these conditions are true:1. Automatic ignition feature is enabled in the CDS software2. N2 is more than 20% (engine running)3. Burner pressure is less than the igniter firing limit pressure(175 psia)4. Thrust lever resolver angle is more than 50 degrees or the airplane is in-flight5. Engine anti-ice is selected on or wing flaps are not up and airplane altitude is less than 18,000 feet.GUN ALLIGNITION - FUNCTIONAL DESCRIPTIONIGNITION - OPERATIONGeneralThese are the flight compartment controls you use to operate the engine ignition:1. Start lever2. Ignition selector switch3. Engine start switch.Start LeverThe start lever controls ignition electrical power to the EEC. The EEC receives 115v ac power for ignition when the start lever is in the idle position.Ignition Selector SwitchThere are three ignition selector switch positions:1. IGN L (Left spark igniter)2. IGN R (right spark igniter)3. BOTH (both spark igniters).Engine Start SwitchThere are four engine start switch selection positions:1. GRD (ground start)2. OFF3. CONT (continuous ignition)4. FLT (flight).Engine Start Switch Position (GRD)The engine starter engages and turns the engine when you put the engine start switch to the GRD position. You supply ignition and fuel to the engine combustor when you move the start lever to the idle position.You use the GRD position to start the engine on the ground.See the engine starting chapter for more information.Engine Start Switch Position (OFF)Usually the igniters do not operate when the start switch is in the OFF position. However, the EEC turns on the ignition system automatically if the EEC sees a possible engine flameout condition. See the functional description page in this section for more information about this function.IGNITION - OPERATIONEngine Start Switch Position (AUTO)Usually the igniters do not operate when the start switch is in the AUTO position. However, the EEC turns on the ignition system automatically if the engine cowl anti-ice system is turned on or flaps are down. The EEC will turn on igniters if it sees a possible engine flameout condition. See the functional description page in this section for more information about this function.Engine Start Switch Position (CONT)The flight crew may turn the engine start switch to the CONT position at these times:1. Takeoff2. Approach3. Landing4. Bad WeatherThe spark igniters, as selected by the ignition selector switch, turn on and operate continuously when the switch is in this position.Engine Start Switch Position (FLT)Both spark igniters operate continuously when you turn the engine start switch to FLT position. The EEC does not use the ignition selector switch position information.IGNITION - OPERATIONIGNITION - TRAINING INFORMATION POINTGeneralThe control display unit (CDU) helps you do troubleshooting of the ignition system. You can also use the CDU to do a ground test of the ignition system.See the engine indicating chapter for more information.IGNITION - TRAINING INFORMATION POINT波音737点火系统1．（1）点火系统简介。

波音737ng机型基础知识总结ATA31

波音737ng机型基础知识总结ATA31展开全文ATA31章指示记录系统电子时钟位于P1 P3 外侧现在UTC时间即格林威治时间（MMR 控制）当地时间（北京时间UTC+8）日期因可由热电瓶汇流条供电所以时钟时刻有电黑匣子：坐舱话音记录器（CVR,记录最后2h语音信息）位于后货舱飞行数据记录器（FDR，记录最后25h数据）位于后厨房顶板橘红色飞行数据记录系统飞行记录器/马赫空速测试组件位于P5后顶板飞行数据采集组件（FDAU）位于电子舱飞行数据记录器（FDR）位于后厨房顶板打印机（printer）位于P8板（因构型而异）FDAU状态继电器位于前轮舱音响警告系统自驾脱开着陆警告超速警告起飞或客舱高度警告火警谐音“录音机”位于P9板下部只有一个在副驾位置主警告系统P7板 4个灯（左右各4个）通用显示系统EFIS（电子飞行仪表系统）控制面板位于P7板(共2个)显示源选择器位于P5板发动机显示控制面板（P2）显示电子组件（DEU）共2个位于电子舱显示选择面板位于P1 P3 各一个远距离光传感器（RLS）（共2个）自动调节DU亮度（位于遮光板上面）DU框上面有白色的感光点也能自动调节DU亮度亮度控制面板（2个）位于P1 P3共有6个DU（PDU ND）任一一个DEU科控制显示任一DUDEU产生视频信号在DU上显示上DU 主发动机显示下DU 次要发动机显示或者系统页面显示PFD比ND重要当PFD损坏时会在UD显示（自动切换）ND能通过P1 P2 P3 面板人工切换详情看31章图ATA32章起落架起落架作用为飞机提供支撑滑行、转弯、起跑减震和耗能刹车和减速NG飞机起落架为前三点可收放油气支柱套筒双轮式起落架选择活门：控制来自转换活门的液压压力流向主起落架和前起落架的收放管路。

起落架控制手柄通过连接到选择活门控制杆上的控制钢索来控制选择活门的位置。

起落架转换活门：起落架转换活门可将起落架压力供应自动或人工地由液压系统A转向液压系统B。

B737NG_起落架

7/20/2013
2
起落架
机务培训中心
7/20/2013
3
起落架
机务培训中心
7/20/2013
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起落架
机务培训中心
空地系统 Clearing system

空地系统介绍 Clearing system is introduced 空地系统主要部件 Space, the main components of the system

7/20/2013
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起落架
机务培训中心
PSEU
简介 PSEU提供控制信号给六个子系统并且为多个飞机系统提供了空/地信号和离散信号 PSEU provide control signals to the six subsystems and for multiple aircraft system provides the empty/signal and discrete signal 位置 PSEU位于前设备舱 Located on the front PSEU equipment tank
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起落架
机务培训中心
7/20/2013
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起落架
机务培训中心
PSEU
空/地继电器 air/ground relay 继电器从直流汇流条或者电瓶汇流条获得电源，PSEU输出控制信号控制各个继电器 Relay from dc bus bar or battery bar gain power, PSEU output control signal control each relay
7/20/2013 9
起落架
机务培训中心

ATA章节中英对照

Chapter 1 – Brief History of AviationChapter 2 – DeregulationChapter 3 – Structure of the IndustryChapter 4 – Airline EconomicsChapter 5 – How Aircraft FlyChapter 6 – SafetyChapter 7 – SecurityChapter 8 – AirportsChapter 9 – Air Traffic ControlChapter 10 – Airlines and the Environment5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage) 11章标牌和铭记(Placards and Markings)12章勤务(Servicing)20章标准施工---机体(Standard Practices---Airframe) 21章空调（Air Conditioning）22章自动飞行（Auto Flight）23章通讯（Communications）24章电源（Electrical Power）25章设备/装饰（Equipment/Furnishings）26章.防火(Fire Protection)27章飞行操纵（Flight Controls）28章燃油（Fuel）29章液压源（Hydraulic Power）30章防冰和排雨（Ice and Rain Protection）31章指示/记录系统（Indicating/Recording system）32章起落架(Landing Gear)33章灯光（Lights）34章导航（Navigation）35章氧气(Oxygen)36章气源(Pneumatic)37章真空（Vacuum）38章水/污水（Water/waste）45章中央维护系统（Central maintenance System）49章机载辅助动力装置(Airborne Auxiliary Power)51章结构与标准施工(Structures & Standard Practices) 52章舱门(Doors)53章机身(Fuselage)54章发动机吊舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)安定面56章窗户(Windows)57章机翼(Wings)70章标准施工—发动机(Standard Practices—Engines)71章动力装置(Power Plant( Package))72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))01 INTRODUCTION05 PERIODIC INSPECTIONS06 DIMENSIONS AND AREAS07 LIFTING AND SHORING08 LEVELING AND WEIGHING09 TOWING AND TAXIING10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE11 PLACARDS AND MARKINGS12 SERVICING - ROUTINE MAINTENANCE18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)20 STANDARD PRACTICES - AIRFRAME21 AIR CONDITIONING22 AUTO FLIGHT23 COMMUNICATIONS24 ELECTRICAL POWER25 EQUIPMENT / FURNISHINGS26 FIRE PROTECTION27 FLIGHT CONTROLS28 FUEL29 HYDRAULIC POWER30 ICE AND RAIN PROTECTION31 INDICATING / RECORDING SYSTEMS32 LANDING GEAR33 LIGHTS34 NAVIGATION35 OXYGEN36 PNEUMATIC37 VACUUM38 WATER / WASTE39 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS41 WATER BALLAST45 CENTRAL MAINTENANCE SYSTEM (CMS)46 INFORMATION SYSTEMS49 AIRBORNE AUXILIARY POWER51 STANDARD PRACTICES AND STRUCTURES - GENERAL52 DOORS53 FUSELAGE54 NACELLES / PYLONS55 STABILIZERS56 WINDOWS57 WINGS60 STANDARD PRACTICES - PROPELLER / ROTOR61 PROPELLERS / PROPULSORS62 MAIN ROTOR(S)63 MAIN ROTOR DRIVE(S)64 TAIL ROTOR65 TAIL ROTOR DRIVE66 ROTOR BLADE AND TAIL PYLON FOLDING67 ROTORS FLIGHT CONTROL70 STANDARD PRACTICES - ENGINE71 POWER PLANT - GENERAL72 ENGINE72(T) ENGINE - TURBINE / TURBOPROP, DUCTED FAN / UNDUCTED FAN 72(R) ENGINE - RECIPROCATING73 ENGINE - FUEL AND CONTROL74 IGNITION75 BLEED AIR76 ENGINE CONTROLS77 ENGINE INDICATING78 EXHAUST79 OIL80 STARTING81 TURBINES (RECIPROCATING ENGINES)82 WATER INJECTION83 ACCESSORY GEAR BOXES (ENGINE DRIVEN)84 PROPULSION AUGMENTATION91 CHARTS5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage)11章标牌和铭记(Placards and Markings)12章勤务(Servicing)BMS3-33润滑脂的介绍20章标准施工---机体(Standard Practices---Airframe)21章空调(Air Conditioning)空调出口温度高原创]关于737-300/500的空调空中超温，会有那些原因引起呢（专业贴）22章自动飞行(Auto Flight)737NG的Y/D故障分析供大家参考23章通讯(Communications)24章电源(Electrical Power)IDG和GEN B2972电源及APU自动关车排故思路之分析25章设备/装饰(Equipment/Furnishings)26章防火(Fire Protection)有关737灭火瓶...... 火警探测27章飞行操纵(Flight Controls)28章燃油(Fuel)737飞机燃油浮子电门29章液压源(Hydraulic Power)液压问题关于液压保险在液压管路的作用和位置请教液压系统故障30章防冰和排雨(Ice and Rain Protection)31章指示/记录系统(Indicating/Recording system)32章起落架(Landing Gear)如何延长飞机轮胎的使用寿命前轮磨损谁能说说金属刹车片和碳刹车片的优缺点请问哪位对防滞刹车结构熟悉的，简单介绍一下，谢谢那里有资料，网上有吗请教:飞机换轮子的时候为什么要转动轮子一起B737-300飞机使用自动速度刹车时，AUTO SPEED BRAKE 跳开关跳开33章灯光(Lights)34章导航(Navigation)35章氧气(Oxygen)36章气源(Pneumatic)一起引气故障导致的增压故障（B737NG）37章真空(Vacuum)38章水/污水(Water/waste)45章中央维护系统(Central maintenance System)49章机载辅助动力装置(Airborne Auxiliary Power)APU启动不起来了! 维护灯亮51章结构与标准施工(Structures & Standard Practices)52章舱门(Doors)53章机身(Fuselage)54章发动机短舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)56章窗户(windows)[讨论]玻璃上裂纹深度的测量57章机翼(wings)70章标准施工---发动机(Standard Practices---Engines)71章动力装置(Power Plant (Package))IAEV2500系列发动机试车总结72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)737反推故障79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))ATA Specification 22001 *Reserved for Airline Use2 *Reserved for Airline Use3 *Reserved for Airline Use4 *Reserved for Airline Use5 TIME LIMITS/ MAINTENANCE CHECKS-00 General-10 Time Limits-20 Scheduled Maintenance Checks-30 & -40 Reserved-50 Unscheduled Maintenance checks6 DIMENSIONS AND AREAS7 LIFTING & SHORING-00 General-10 Jacking-20 Shoring8 LEVELING & WEIGHING-00 General-10 Weighing and Balancing-20 Leveling9 TOWING & TAXIING-00 General-10 Towing-20 Taxiing10 PARKING, MOORING, STORAGE & RETURN TO SERVICE -00 General-10 Parking/Storage-20 Mooring-30 Return to Service11 PLACARDS AND MARKINGS-00 General-10 Exterior Color Schemes and Markings-20 Exterior Placards and Markings-30 Interior Placards12 SERVICING-00 General-10 Replenishing-20 Scheduled Servicing-30 Unscheduled Servicing13 *Unassigned14 *Unassigned15 *Unassigned16 *Unassigned17 *Unassigned18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY) -00 GENERAL --10 VIBRATION ANALYSIS-20 NOISE ANALYSIS19 *Unassigned20 STANDARD PRACTICES-AIRFRAME-90 *Reserved for Airline Use21 AIR CONDITIONING-00 General-10 Compression-20 Distribution-30 Pressurization Control-40 Heating-50 Cooling-60 Temperature Control-70 Moisture/Air Contaminant22 AUTO FLIGHT-00 General-10 Autopilot-20 Speed-Attitude Correction-30 Auto Throttle-40 System Monitor-50 Aerodynamic Load Alleviating23 COMMUNICATIONS-00 General-10 Speech Communications-15 SATCOM-20 Data Transmission and Automatic Calling-30 Comfort-40 Interphone-50 Audio Integrating-60 Static Discharging-70 Audio & Video Monitoring-80 Integrated Automatic24 ELECTRICAL POWER-00 General-10 Generator Drive-20 AC Generation-30 DC Generation-40 External Power-50 AC Electrical Load Distribution-60 DC Electrical Load Distribution25 EQUIPMENT/FURNISHINGS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Galley-40 Lavatories-50 Additional Compartments-60 Emergency-70 Available-80 Insulation26 FIRE PROTECTION-00 General-10 Detection-20 Extinguishing-30 Explosion Suppression27 FLIGHT CONTROLS-00 General-10 Aileron & Tab-20 Rudder & Tab-30 Elevator & Tab-40 Horizontal Stabilizer-50 Flaps-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -70 Gust Lock & Dampener-80 Lift Augmenting28 FUEL-00 General-10 Storage-20 Distribution-30 Dump-40 Indicating29 HYDRAULIC POWER-00 General-10 Main-20 Auxiliary-30 Indicating30 ICE AND RAIN PROTECTION-00 General-10 Airfoil-20 Air Intakes-30 Pitot and Static-40 Windows, Windshields and Doors -50 Antennas and Radomes-60 Propellers/Rotors-70 Water Lines-80 Detection31 INDICATING/RECORDING SYSTEMS-00 General-10 Instrument & Control Panels-20 Independent Instruments-30 Recorders-40 Central Computers-50 Central Warning Systems-60 Central Display Systems-70 Automatic Data Reporting Systems 32 LANDING GEAR-00 General-10 Main Gear and Doors-20 Nose Gear and Doors-30 Extension and Retraction-40 Wheels and Brakes-50 Steering-60 Position and Warning-70 Supplementary Gear33 LIGHTS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Cargo and Service Compartments -40 Exterior-50 Emergency Lighting34 NAVIGATION-00 General-10 Flight Environment-20 Attitude & Direction-30 Landing and Taxiing Aids-40 Independent Position Determining -50 Dependent Position Determining -60 Flight Management Computing35 OXYGEN-00 General-10 Crew-20 Passenger-20 Passenger-30 Portable36 PNEUMATIC-00 General-10 Distribution-20 Indicating37 VACUUM-00 General-10 Distribution-20 Indicating38 WATER/WASTE-00 General-10 Potable-20 Wash-30 Waste Disposal-40 Air Supply39 *Unassigned40 *Unassigned41 WATER BALLAST-00 General-10 Storage-20 Dump-30 Indication42 *Unassigned43 *Unassigned44 CABIN SYSTEMS-00 General-10 Cabin Core System-20 Inflight Entertainment System-30 External Communication System-40 Cabin Mass Memory System-50 Cabin Monitoring System-60 Miscellaneous Cabin System45 CENTRAL MAINTENANCE SYSTEM-00 General-5 thru -19 CMS/Aircraft General-20 thru -49 CMS/Airframe Systems-45 Central Maintenance System-50 thru -59 CMS/Structures-60 thru -69 CMS/Propellers-70 thru -89 CMS/Power Plant45INFORMATION SYSTEMS-00 General-10 Airplane General Information Systems -20 Flight Deck Information Systems-30 Maintenance Information Systems-40 Passenger Cabin Information Systems -50 Miscellaneous Information Systems47 *Unassigned48 *Unassigned49 AIRBORNE AUXILIARY POWER-00 General-10 Power Plant-20 Engine-30 Engine Fuel and Control-40 Ignition/Starting-50 Air-60 Engine Controls .-70 Indicating-80 Exhaust-90 Oil50 Cargo and Accessory Compartments-00 General-10 Cargo Compartments-20 Cargo Loading Systems-30 Cargo Related Systems-40 Available-50 Accessory-60 Insulation51 Standard Practices, General-00 General-10 Investigation, Cleanup and Aerodynamic Smoothness-20 Processes-30 Materials-40 Fasteners-50 Support of Airplane for Repair and Alignment Check Procedures -60 Control-Surface Balancing-70 Repairs-80 Electrical Bonding52 DOORS-00 General-10 Passenger/Crew-20 Emergency Exit-30 Cargo-40 Service and Miscellaneous-50 Fixed Interior-60 Entrance Stairs-70 Monitoring and Operation-80 Landing Gear53 FUSELAGE-00 General-10 thru -90 (As Required) Fuselage Sections54 NACELLES/PYLONS-00 General-10 thru -40 (As Required) Nacelle Section-50 thru -80 (As Required) Pylon55 STABILIZERS-00 General-10 Horizontal Stabilizer or Canard-20 Elevator-30 Vertical Stabilizer-40 Rudder56 WINDOWS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Door-40 Inspection and Observation57 WINGS-00 General-10 Center Wing-20 Outer Wing-30 Wing Tip-40 Leading Edge and Leading Edge Devices -50 Trailing Edge Trailing Edge Devices -60 Ailerons and Elevons-70 Spoilers-80 (as required)-90 Wing Folding System58 *Unassigned59 *Reserved for Airline Use60 STANDARD PRACTICES - PROPELLER/ROTOR61 PROPELLERS/PROPULSION-00 General-10 Propeller Assembly-20 Controlling-30 Braking-40 Indicating-50 Propulsor Duct62 ROTOR(S)-00 General-10 Rotor blades-20 Rotor head(s)-30 Rotor Shaft(s)/Swashplate Assy(ies) -4063 ROTOR DRIVE(S)-00 General-10 Engine/Gearbox couplings-20 Gearbox(es)-30 Mounts, attachments-40 Indicating64 TAIL ROTOR-00 General-10* Rotor blades-20* Rotor head-30 Available-40 Indicating65 TAIL ROTOR DRIVE-00 General-10 Shafts-20 Gearboxes-30 Available-40 Indicating66 FOLDING BLADES/PYLON-00 General-10 Rotor blades-20 Tail pylon-30 Controls and Indicating67 ROTORS FLIGHT CONTROL-00 General-10 Rotor-20 Anti-torque Rotor control (Yaw control)-30 Servo-control System68 *Unassigned69*Unassigned70 STANDARD PRACTICES - ENGINES71 POWER PLANT-00 General-10 Cowling-30 Fireseals-40 Attach Fittings-50 Electrical Harness-60 Air Intakes-70 Engine Drains72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN-00 General-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor) -20 Air Inlet Section-30 Compressor Section-40 Combustion Section-50 Turbine Section-60 Accessory Drives-70 By-pass Section-80 Propulsor Section (Rear Mounted)73 ENGINE FUEL AND CONTROL-00 General-10 Distribution-30 Indicating74 IGNITION-00 General-10 Electrical Power-20 Distribution-30 Switching75 AIR-00 General-10 Engine Anti-Icing-20 Cooling-30 Compressor Control-40 Indicating76 ENGINE CONTROLS-00 General-10 Power Control-20 Emergency Shutdown77 ENGINE INDICATING-00 General-10 Power-20 Temperature-30 Analyzers That-40 Integrated Engine Instrument Systems 78 EXHAUST-00 General-10 Collector/Nozzle-20 Noise Suppressor-30 Thrust Reverser-40 Supplementary Air79 OIL-00 General-10 Storage-20 Distribution-30 Indicating80 STARTING-00 General-10 Cranking81 TURBINES-00 General-10 Power Recovery-20 Turbo-Supercharger82 WATER INJECTION-00 General-10 Storage-20 Distribution-30 Dumping and Purging83 ACCESSORY GEAR-BOXES-00 General-10 Drive Shaft Section-20 Gearbox Section84 Propulsion Augmentation-00 General-10 Jet Assist Takeoff85 *Unassigned86 *Unassigned87 *Unassigned88 *Unassigned89 *Unassigned90 *Unassigned91 CHARTS92 *Unassigned93 *Unassigned94 *Unassigned95 *Reserved for Airline Use96 *Reserved for Airline Use97 WIRING REPORTING-00-00 General-01-00 Zone 100 Fuselage Lower-02-00 Zone 200 Fuselage Top-03-00 Zone 300 Stabilizers-04-00 Zone 400 Nacelles-Pylons-05-00 Zone 500 Left Wing-06-00 Zone 600 Right Wing-07-00 Zone 700 Landing Gear Compartment -08-00 Zone 800 Doors-09-00 Zone 900 Lavatories & Galleys-20-00 Electrical Standard Items/Practices -21-00 Air Conditioning - General-21-10 Compression-21-20 Distribution-21-30 Pressurization Control-21-40 Heating-21-50 Cooling-21-60 Temperature Control-21-70 Moisture/Air Contaminant Control-22-00 Auto Flight - General-22-10 Autopilot-22-20 Speed - Attitude Correction-22-30 Auto Throttle-22-40 System Monitors-22-50 Aerodynamic Load Alleviating-23-00 Communications - General-23-10 Speech Communications-23-15 SATCOM-23-20 Data Transmission and Automatic Calling-23-30 Passenger Address, Entertainment and Comfort-23-40 Interphone-23-50 Audio Integrating-23-60 Static Discharging-23-70 Audio and Video Monitoring-23-80 Integrated Automatic Tuning-24-00 Electrical Power - General-24-10 Generator Drive-24-20 AC Generation-24-30 DC Generation-24-40 External Power-24-50 AC Electrical Load Distribution-24-60 DC Electrical Load Distribution-25-00 Equipment/Furnishings - General-25-10 Flight Compartment-25-20 Passenger Compartment-25-30 Galley-25-40 Lavatories-25-60 Emergency-25-80 Insulation-26-00 Fire Protection - General-26-10 Detection-26-20 Extinguishing-26-30 Explosion Suppression-27-00 Flight Controls - General-27-10 Aileron & Tab-27-20 Rudder & Tab-27-30 Elevator & Tab-27-40 Horizontal Stabilizer-27-50 Flaps-27-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -27-70 Gust Lock & Dampener-27-80 Lift Augmenting-28-00 Fuel - General-28-10 Storage-28-20 Distribution-28-30 Dump-28-40 Indicating-29-00 Hydraulic Power - General-29-10 Main-29-20 Auxiliary-29-30 Indicating-30-00 Ice and Rain Protection - General-30-10 Airfoil-30-20 Air Intakes-30-30 Pitot and Static-30-40 Windows, Windshields and Doors-30-50 Antennas And Radomes-30-60 Propellers/Rotors-30-70 Water Lines-30-80 Detection-31-00 Indicating/Recording Systems - General -31-10 Instrument and Control Panels-31-20 Independent Instruments-31-30 Recorders-31-40 Central Computers-31-50 Central Warning Systems-31-60 Central Display Systems-31-70 Automatic Data Reporting Systems-32-00 Landing Gear- General-32-10 Main Gear and Doors-32-20 Nose Gear and Doors-32-30 Extension and Retraction-32-40 Wheels and Brakes-32-50 Steering-32-60 Position And Warning-32-70 Supplementary Gear-33-00 Lights - General-33-10 Flight Compartment-33-20 Passenger Compartment-33-30 Cargo and Service Compartments-33-40 Exterior-33-50 Emergency Lighting-34-00 Navigation - General-34-10 Flight Environment Data-34-20 Attitude & Direction-34-30 Landing and Taxiing Aids-34-40 Independent Position Determining-34-50 Dependent Position Determining-34-60 Flight Management Computing-35-00 Oxygen - General-35-10 Crew-35-20 Passenger-35-30 Portable-36-00 Pneumatic - General-36-10 Distribution-36-20 Indicating-37-00 Vacuum - General-37-10 Distribution-37-20 Indicating-38-00 Water/Waste - General-38-10 Potable-38-20 Wash-38-30 Waste Disposal-38-40 Air Supply-44-00 Cabin Systems - General-44-10 Cabin Core System-44-20 In-flight Entertainment System-44-30 External Communication System-44-40 Cabin Mass Memory System-44-50 Cabin Monitoring System-44-60 Miscellaneous Cabin System-45-00 Central Maintenance System (CMS) General -45-05 CMS/Aircraft General-45-20 CMS/Airframe Systems-45-45 Central Maintenance System-45-50 CMS/Structures-45-60 CMS/Propellers-45-70 CMS/Power Plant-46-00 Information Systems - General-46-10 Airplane General Information Systems-46-20 Flight Deck Information Systems-46-30 Maintenance Information Systems-46-40 Passenger Cabin Information Systems-46-50 Miscellaneous Information Systems-49-00 Airborne Auxiliary Power - General-49-10 Power Plant-49-20 Engine-49-30 Engine Fuel And Control-49-40 Ignition And Starting-49-50 Air-49-60 Engine Controls-49-70 Indicating-49-80 Exhaust-49-90 Oil-50-00 Cargo And Accessory Compartments General -50-10 Cargo Compartments-50-20 Cargo Loading Systems-50-30 Cargo Related Systems-50-40 Available-50-50 Accessory Compartments-50-60 Insulation-52-00 Doors - General-52-10 Passenger/Crew-52-20 Emergency Exit-52-30 Cargo-52-40 Service-52-50 Fixed Interior-52-60 Entrance Stairs-52-70 Door Warning-52-80 Landing Gear-53-00 Fuselage - General-54-00 Nacelles/Pylons - General-54-10 Nacelle Section-54-50 Pylon-55-00 Stabilizers - General-55-10 Horizontal Stabilizer or Canard-55-20 Elevator-55-30 Vertical Stabilizer-55-40 Rudder-56-00 Windows - General-56-10 Flight Compartment-56-20 Passenger Compartment-56-30 Door-56-40 Inspection and Observation-57-00 Wings - General-57-10 Center Wing-57-20 Outer Wing-57-30 Wing Tip-57-40 Leading Edge and Leading Edge Devices -57-50 Trailing Edge and Trailing Edge Devices -57-60 Ailerons-57-70 Spoilers-57-90 Wing Folding System-61-00 Propellers/Propulsors - General-61-10 Propeller Assembly-61-20 Controlling-61-30 Braking-61-40 Indicating-61-50 Propulsor Duct-62-00 Rotors-63-00 Rotor Drives-64-00 Tail Rotor-65-00 Tail Rotor Drive-66-00 Folding Blades/Pylon-67-00 Rotors Flight Control-71-00 Power Plant - General-71-10 Cowling-71-20 Mounts-71-30 Fire seals-71-40 Attach Fittings-71-50 Electrical Harness-71-60 Air Intakes-71-70 Engine Drains-72-00 Engine Turbine/Turbo Prop Ducted Fan/Unducted Fan-72-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor)-72-20 Air Inlet Section-72-30 Compressor Section-72-40 Combustion Section-72-50 Turbine Section-72-60 Accessory Drives-72-70 By-pass Section-72-80 Propulsor Section (Rear Mounted)-73-00 Engine Fuel And Control - General-73-10 Distribution-73-20 Controlling-73-30 Indicating-74-00 Ignition - General-74-10 Electrical Power Supply-74-20 Distribution-74-30 Switching-75-00 Air - General-75-10 Engine Anti-Icing-75-20 Cooling-75-30 Compressor Control-75-40 Indicating-76-00 Engine Controls - General-76-10 Power Control-76-20 Emergency Shutdown-77-00 Engine Indicating - General-77-10 Power-77-20 Temperature-77-30 Analyzers-77-40 Integrated Engine Instrument Systems-78-00 Exhaust - General-78-10 Collector/Nozzle-78-20 Noise Suppressor-78-30 Thrust Reverser-78-40 Supplementary Air-79-00 Oil - General-79-10 Storage-79-30 Indicating-80-00 Starting - General-80-10 Cranking98 *Reserved for Airline Use99 *Unassigned100 *Do not use101 *Do not use102 *Do not use103 *Do not use104 *Do not use105 *Do not use106 *Do not use107 *Do not use108 *Do not use109 *Do not use110 *Do not use111 *Do not use112 *Do not use113 *Do not use114 *Do not use115 Flight Simulator Systems。

B737NG ATA章节中英文对照表

水平安定面配平控制系统
51
TRAILING EDGE FLAP SYSTEM
后缘襟翼系统
58
FLAP POSITION TRANSMITTERS AND INDICATORS
襟翼位置传感器和指示
59
FLAP SKEW DETECTION SYSTEM
襟翼倾斜探测系统
61
SPOILER CONTROL SYSTEM
06
24
WING STATION DIAGRAM
大翼站位尺寸
25
ENGINE AND NACELLE STATION DIAGRAM
发动机和吊舱站位图
30
ZONE DIAGRAM
区域图
41
FUSELAGE(MAJLR ZONES 100 AND 200)ACCESS DOORS AND PANELS
自动飞行
11
DIGITAL FLIGHT CONTROL SYSTEM
数字式飞行控制系统
23
YAW DAMPER SYSTEM
偏航阻尼系统
31
AUTO THROTTLE SYSTEM
自动油门系统
23
00
COMMUNICATION
通讯
11
HIGH FREQUENCY COMMUNICATION SYSTEM
副翼和副翼配平控制系统
21
RUDDER AND RUDDER TRIM CONTROL SYSTEM
方向舵和方向舵配 AND TAB CONTROL SYSTEM
升降舵和调整片控制系统
32
STALL WARNING SYSTEM
失速警告系统
41
HORIZONTAL STABILIZER TRIM CONTROL SYSTEM

ATA章节中英对照

Chapter 1 – Brief History of AviationChapter 2 – DeregulationChapter 3 – Structure of the IndustryChapter 4 – Airline EconomicsChapter 5 – How Aircraft FlyChapter 6 – SafetyChapter 7 – SecurityChapter 8 – AirportsChapter 9 – Air Traffic ControlChapter 10 – Airlines and the Environment5章时间限制、维修检查(Time Limits,Maint. Checks) 6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage) 11章标牌和铭记(Placards and Markings)12章勤务(Servicing)20章标准施工---机体(Standard Practices---Airframe) 21章空调（Air Conditioning）22章自动飞行（Auto Flight）23章通讯（Communications）24章电源（Electrical Power）25章设备/装饰（Equipment/Furnishings）26章.防火(Fire Protection)27章飞行操纵（Flight Controls）28章燃油（Fuel）29章液压源（Hydraulic Power）30章防冰和排雨（Ice and Rain Protection）31章指示/记录系统（Indicating/Recording system）32章起落架(Landing Gear)33章灯光（Lights）34章导航（Navigation）35章氧气(Oxygen)36章气源(Pneumatic)37章真空（Vacuum）38章水/污水（Water/waste）45章中央维护系统（Central maintenance System）49章机载辅助动力装置(Airborne Auxiliary Power)51章结构与标准施工(Structures & Standard Practices) 52章舱门(Doors)53章机身(Fuselage)54章发动机吊舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)安定面56章窗户(Windows)57章机翼(Wings)70章标准施工—发动机(Standard Practices—Engines) 71章动力装置(Power Plant( Package))72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))01 INTRODUCTION05 PERIODIC INSPECTIONS06 DIMENSIONS AND AREAS07 LIFTING AND SHORING08 LEVELING AND WEIGHING09 TOWING AND TAXIING10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE11 PLACARDS AND MARKINGS12 SERVICING - ROUTINE MAINTENANCE18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)20 STANDARD PRACTICES - AIRFRAME21 AIR CONDITIONING22 AUTO FLIGHT23 COMMUNICATIONS24 ELECTRICAL POWER25 EQUIPMENT / FURNISHINGS26 FIRE PROTECTION27 FLIGHT CONTROLS28 FUEL29 HYDRAULIC POWER30 ICE AND RAIN PROTECTION31 INDICATING / RECORDING SYSTEMS32 LANDING GEAR33 LIGHTS34 NAVIGATION35 OXYGEN36 PNEUMATIC37 VACUUM38 WATER / WASTE39 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS 41 WATER BALLAST45 CENTRAL MAINTENANCE SYSTEM (CMS)46 INFORMATION SYSTEMS49 AIRBORNE AUXILIARY POWER51 STANDARD PRACTICES AND STRUCTURES - GENERAL52 DOORS53 FUSELAGE54 NACELLES / PYLONS55 STABILIZERS56 WINDOWS57 WINGS60 STANDARD PRACTICES - PROPELLER / ROTOR61 PROPELLERS / PROPULSORS62 MAIN ROTOR(S)63 MAIN ROTOR DRIVE(S)64 TAIL ROTOR65 TAIL ROTOR DRIVE66 ROTOR BLADE AND TAIL PYLON FOLDING67 ROTORS FLIGHT CONTROL70 STANDARD PRACTICES - ENGINE71 POWER PLANT - GENERAL72 ENGINE72(T) ENGINE - TURBINE / TURBOPROP, DUCTED FAN / UNDUCTED FAN 72(R) ENGINE - RECIPROCATING73 ENGINE - FUEL AND CONTROL74 IGNITION75 BLEED AIR76 ENGINE CONTROLS77 ENGINE INDICATING78 EXHAUST79 OIL80 STARTING81 TURBINES (RECIPROCATING ENGINES)82 WATER INJECTION83 ACCESSORY GEAR BOXES (ENGINE DRIVEN)84 PROPULSION AUGMENTATION91 CHARTS5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage)11章标牌和铭记(Placards and Markings)12章勤务(Servicing)BMS3-33润滑脂的介绍20章标准施工---机体(Standard Practices---Airframe)21章空调(Air Conditioning)空调出口温度高原创]关于737-300/500的空调空中超温，会有那些原因引起呢（专业贴）22章自动飞行(Auto Flight)737NG的Y/D故障分析供大家参考23章通讯(Communications)24章电源(Electrical Power)IDG和GEN B2972电源及APU自动关车排故思路之分析25章设备/装饰(Equipment/Furnishings)26章防火(Fire Protection)有关737灭火瓶...... 火警探测27章飞行操纵(Flight Controls)28章燃油(Fuel)737飞机燃油浮子电门29章液压源(Hydraulic Power)液压问题关于液压保险在液压管路的作用和位置请教液压系统故障30章防冰和排雨(Ice and Rain Protection)31章指示/记录系统(Indicating/Recording system)32章起落架(Landing Gear)如何延长飞机轮胎的使用寿命前轮磨损谁能说说金属刹车片和碳刹车片的优缺点请问哪位对防滞刹车结构熟悉的，简单介绍一下，谢谢那里有资料，网上有吗请教:飞机换轮子的时候为什么要转动轮子一起B737-300飞机使用自动速度刹车时，AUTO SPEED BRAKE 跳开关跳开33章灯光(Lights)34章导航(Navigation)35章氧气(Oxygen)36章气源(Pneumatic)一起引气故障导致的增压故障（B737NG）37章真空(Vacuum)38章水/污水(Water/waste)45章中央维护系统(Central maintenance System)49章机载辅助动力装置(Airborne Auxiliary Power)APU启动不起来了! 维护灯亮51章结构与标准施工(Structures & Standard Practices) 52章舱门(Doors)53章机身(Fuselage)54章发动机短舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)56章窗户(windows)[讨论]玻璃上裂纹深度的测量57章机翼(wings)70章标准施工---发动机(Standard Practices---Engines)71章动力装置(Power Plant (Package))IAEV2500系列发动机试车总结72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)737反推故障79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))ATA Specification 22001 *Reserved for Airline Use2 *Reserved for Airline Use3 *Reserved for Airline Use4 *Reserved for Airline Use5 TIME LIMITS/ MAINTENANCE CHECKS-00 General-10 Time Limits-20 Scheduled Maintenance Checks-30 & -40 Reserved-50 Unscheduled Maintenance checks6 DIMENSIONS AND AREAS7 LIFTING & SHORING-00 General-10 Jacking-20 Shoring8 LEVELING & WEIGHING-00 General-10 Weighing and Balancing-20 Leveling9 TOWING & TAXIING-00 General-10 Towing-20 Taxiing10 PARKING, MOORING, STORAGE & RETURN TO SERVICE -00 General-10 Parking/Storage-20 Mooring-30 Return to Service11 PLACARDS AND MARKINGS-00 General-10 Exterior Color Schemes and Markings-20 Exterior Placards and Markings-30 Interior Placards12 SERVICING-00 General-10 Replenishing-20 Scheduled Servicing-30 Unscheduled Servicing13 *Unassigned14 *Unassigned15 *Unassigned16 *Unassigned17 *Unassigned18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY) -00 GENERAL --10 VIBRATION ANALYSIS-20 NOISE ANALYSIS19 *Unassigned20 STANDARD PRACTICES-AIRFRAME-90 *Reserved for Airline Use21 AIR CONDITIONING-00 General-10 Compression-20 Distribution-30 Pressurization Control-40 Heating-50 Cooling-60 Temperature Control-70 Moisture/Air Contaminant22 AUTO FLIGHT-00 General-10 Autopilot-20 Speed-Attitude Correction-30 Auto Throttle-40 System Monitor-50 Aerodynamic Load Alleviating23 COMMUNICATIONS-00 General-10 Speech Communications-15 SATCOM-20 Data Transmission and Automatic Calling -30 Comfort-40 Interphone-50 Audio Integrating-60 Static Discharging-70 Audio & Video Monitoring-80 Integrated Automatic24 ELECTRICAL POWER-00 General-10 Generator Drive-20 AC Generation-30 DC Generation-40 External Power-50 AC Electrical Load Distribution -60 DC Electrical Load Distribution 25 EQUIPMENT/FURNISHINGS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Galley-40 Lavatories-50 Additional Compartments-60 Emergency-70 Available-80 Insulation26 FIRE PROTECTION-00 General-10 Detection-20 Extinguishing-30 Explosion Suppression27 FLIGHT CONTROLS-00 General-10 Aileron & Tab-20 Rudder & Tab-30 Elevator & Tab-40 Horizontal Stabilizer-50 Flaps-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -70 Gust Lock & Dampener-80 Lift Augmenting28 FUEL-00 General-10 Storage-20 Distribution-30 Dump-40 Indicating29 HYDRAULIC POWER-00 General-10 Main-20 Auxiliary-30 Indicating30 ICE AND RAIN PROTECTION-00 General-10 Airfoil-20 Air Intakes-30 Pitot and Static-40 Windows, Windshields and Doors -50 Antennas and Radomes-60 Propellers/Rotors-70 Water Lines-80 Detection31 INDICATING/RECORDING SYSTEMS-00 General-10 Instrument & Control Panels-20 Independent Instruments-30 Recorders-40 Central Computers-50 Central Warning Systems-60 Central Display Systems-70 Automatic Data Reporting Systems 32 LANDING GEAR-00 General-10 Main Gear and Doors-20 Nose Gear and Doors-30 Extension and Retraction-40 Wheels and Brakes-50 Steering-60 Position and Warning-70 Supplementary Gear33 LIGHTS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Cargo and Service Compartments -40 Exterior-50 Emergency Lighting34 NAVIGATION-00 General-10 Flight Environment-20 Attitude & Direction-30 Landing and Taxiing Aids-40 Independent Position Determining -50 Dependent Position Determining -60 Flight Management Computing35 OXYGEN-00 General-10 Crew-20 Passenger-20 Passenger-30 Portable36 PNEUMATIC-00 General-10 Distribution-20 Indicating37 VACUUM-00 General-10 Distribution-20 Indicating38 WATER/WASTE-00 General-10 Potable-20 Wash-30 Waste Disposal-40 Air Supply39 *Unassigned40 *Unassigned41 WATER BALLAST-00 General-10 Storage-20 Dump-30 Indication42 *Unassigned43 *Unassigned44 CABIN SYSTEMS-00 General-10 Cabin Core System-20 Inflight Entertainment System -30 External Communication System -40 Cabin Mass Memory System-50 Cabin Monitoring System-60 Miscellaneous Cabin System45 CENTRAL MAINTENANCE SYSTEM-00 General-5 thru -19 CMS/Aircraft General -20 thru -49 CMS/Airframe Systems -45 Central Maintenance System-50 thru -59 CMS/Structures-60 thru -69 CMS/Propellers-70 thru -89 CMS/Power Plant45INFORMATION SYSTEMS-00 General-10 Airplane General Information Systems -20 Flight Deck Information Systems-30 Maintenance Information Systems-40 Passenger Cabin Information Systems -50 Miscellaneous Information Systems47 *Unassigned48 *Unassigned49 AIRBORNE AUXILIARY POWER-00 General-10 Power Plant-20 Engine-30 Engine Fuel and Control-40 Ignition/Starting-50 Air-60 Engine Controls .-70 Indicating-80 Exhaust-90 Oil50 Cargo and Accessory Compartments-00 General-10 Cargo Compartments-20 Cargo Loading Systems-30 Cargo Related Systems-40 Available-50 Accessory-60 Insulation51 Standard Practices, General-00 General-10 Investigation, Cleanup and Aerodynamic Smoothness-20 Processes-30 Materials-40 Fasteners-50 Support of Airplane for Repair and Alignment Check Procedures -60 Control-Surface Balancing-70 Repairs-80 Electrical Bonding52 DOORS-00 General-10 Passenger/Crew-20 Emergency Exit-30 Cargo-40 Service and Miscellaneous-50 Fixed Interior-60 Entrance Stairs-70 Monitoring and Operation-80 Landing Gear53 FUSELAGE-00 General-10 thru -90 (As Required) Fuselage Sections54 NACELLES/PYLONS-00 General-10 thru -40 (As Required) Nacelle Section -50 thru -80 (As Required) Pylon55 STABILIZERS-00 General-10 Horizontal Stabilizer or Canard-20 Elevator-30 Vertical Stabilizer-40 Rudder56 WINDOWS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Door-40 Inspection and Observation57 WINGS-00 General-10 Center Wing-20 Outer Wing-30 Wing Tip-40 Leading Edge and Leading Edge Devices -50 Trailing Edge Trailing Edge Devices-60 Ailerons and Elevons-70 Spoilers-80 (as required)-90 Wing Folding System58 *Unassigned59 *Reserved for Airline Use60 STANDARD PRACTICES - PROPELLER/ROTOR61 PROPELLERS/PROPULSION-00 General-10 Propeller Assembly-20 Controlling-30 Braking-40 Indicating-50 Propulsor Duct62 ROTOR(S)-00 General-10 Rotor blades-20 Rotor head(s)-30 Rotor Shaft(s)/Swashplate Assy(ies) -4063 ROTOR DRIVE(S)-00 General-10 Engine/Gearbox couplings-20 Gearbox(es)-30 Mounts, attachments-40 Indicating64 TAIL ROTOR-00 General-10* Rotor blades-20* Rotor head-30 Available-40 Indicating65 TAIL ROTOR DRIVE-00 General-10 Shafts-20 Gearboxes-30 Available-40 Indicating66 FOLDING BLADES/PYLON-00 General-10 Rotor blades-20 Tail pylon-30 Controls and Indicating67 ROTORS FLIGHT CONTROL-00 General-10 Rotor-20 Anti-torque Rotor control (Yaw control) -30 Servo-control System68 *Unassigned69*Unassigned70 STANDARD PRACTICES - ENGINES71 POWER PLANT-00 General-10 Cowling-30 Fireseals-40 Attach Fittings-50 Electrical Harness-60 Air Intakes-70 Engine Drains72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN-00 General-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor)-20 Air Inlet Section-30 Compressor Section-40 Combustion Section-50 Turbine Section-60 Accessory Drives-70 By-pass Section-80 Propulsor Section (Rear Mounted)73 ENGINE FUEL AND CONTROL-00 General-10 Distribution-20 Controlling-30 Indicating74 IGNITION-00 General-10 Electrical Power-20 Distribution-30 Switching75 AIR-00 General-10 Engine Anti-Icing-20 Cooling-30 Compressor Control-40 Indicating76 ENGINE CONTROLS-00 General-10 Power Control-20 Emergency Shutdown77 ENGINE INDICATING-00 General-10 Power-20 Temperature-30 Analyzers That-40 Integrated Engine Instrument Systems 78 EXHAUST-00 General-10 Collector/Nozzle-20 Noise Suppressor-30 Thrust Reverser-40 Supplementary Air79 OIL-00 General-10 Storage-20 Distribution-30 Indicating80 STARTING-00 General-10 Cranking81 TURBINES-00 General-10 Power Recovery-20 Turbo-Supercharger82 WATER INJECTION-00 General-10 Storage-20 Distribution-30 Dumping and Purging-40 Indicating83 ACCESSORY GEAR-BOXES-00 General-10 Drive Shaft Section-20 Gearbox Section84 Propulsion Augmentation -00 General-10 Jet Assist Takeoff85 *Unassigned86 *Unassigned87 *Unassigned88 *Unassigned89 *Unassigned90 *Unassigned91 CHARTS92 *Unassigned93 *Unassigned94 *Unassigned95 *Reserved for Airline Use96 *Reserved for Airline Use97 WIRING REPORTING-00-00 General-01-00 Zone 100 Fuselage Lower-02-00 Zone 200 Fuselage Top-03-00 Zone 300 Stabilizers-04-00 Zone 400 Nacelles-Pylons-05-00 Zone 500 Left Wing-06-00 Zone 600 Right Wing-07-00 Zone 700 Landing Gear Compartment -08-00 Zone 800 Doors-09-00 Zone 900 Lavatories & Galleys-20-00 Electrical Standard Items/Practices -21-00 Air Conditioning - General-21-10 Compression-21-20 Distribution-21-30 Pressurization Control-21-40 Heating-21-50 Cooling-21-60 Temperature Control-21-70 Moisture/Air Contaminant Control-22-00 Auto Flight - General-22-10 Autopilot-22-20 Speed - Attitude Correction-22-30 Auto Throttle-22-40 System Monitors-22-50 Aerodynamic Load Alleviating-23-00 Communications - General-23-10 Speech Communications-23-15 SATCOM-23-20 Data Transmission and Automatic Calling-23-30 Passenger Address, Entertainment and Comfort -23-40 Interphone-23-50 Audio Integrating-23-60 Static Discharging-23-70 Audio and Video Monitoring-23-80 Integrated Automatic Tuning-24-00 Electrical Power - General-24-10 Generator Drive-24-20 AC Generation-24-30 DC Generation-24-40 External Power-24-50 AC Electrical Load Distribution-24-60 DC Electrical Load Distribution-25-00 Equipment/Furnishings - General-25-10 Flight Compartment-25-20 Passenger Compartment-25-30 Galley-25-40 Lavatories-25-60 Emergency-25-80 Insulation-26-00 Fire Protection - General-26-10 Detection-26-20 Extinguishing-26-30 Explosion Suppression-27-00 Flight Controls - General-27-10 Aileron & Tab-27-20 Rudder & Tab-27-30 Elevator & Tab-27-40 Horizontal Stabilizer-27-50 Flaps-27-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -27-70 Gust Lock & Dampener-27-80 Lift Augmenting-28-00 Fuel - General-28-10 Storage-28-20 Distribution-28-30 Dump-28-40 Indicating-29-00 Hydraulic Power - General-29-10 Main-29-20 Auxiliary-29-30 Indicating-30-00 Ice and Rain Protection - General-30-10 Airfoil-30-20 Air Intakes-30-30 Pitot and Static-30-40 Windows, Windshields and Doors-30-50 Antennas And Radomes-30-60 Propellers/Rotors-30-70 Water Lines-30-80 Detection-31-00 Indicating/Recording Systems - General-31-10 Instrument and Control Panels-31-20 Independent Instruments-31-30 Recorders-31-40 Central Computers-31-50 Central Warning Systems-31-60 Central Display Systems-31-70 Automatic Data Reporting Systems -32-00 Landing Gear- General-32-10 Main Gear and Doors-32-20 Nose Gear and Doors-32-30 Extension and Retraction-32-40 Wheels and Brakes-32-50 Steering-32-60 Position And Warning-32-70 Supplementary Gear-33-00 Lights - General-33-10 Flight Compartment-33-20 Passenger Compartment-33-30 Cargo and Service Compartments -33-40 Exterior-33-50 Emergency Lighting-34-00 Navigation - General-34-10 Flight Environment Data-34-20 Attitude & Direction-34-30 Landing and Taxiing Aids-34-40 Independent Position Determining -34-50 Dependent Position Determining-34-60 Flight Management Computing-35-00 Oxygen - General-35-10 Crew-35-20 Passenger-35-30 Portable-36-00 Pneumatic - General-36-10 Distribution-36-20 Indicating-37-00 Vacuum - General-37-10 Distribution-37-20 Indicating-38-00 Water/Waste - General-38-10 Potable-38-20 Wash-38-30 Waste Disposal-38-40 Air Supply-44-00 Cabin Systems - General-44-10 Cabin Core System-44-20 In-flight Entertainment System-44-30 External Communication System-44-40 Cabin Mass Memory System-44-50 Cabin Monitoring System-44-60 Miscellaneous Cabin System-45-00 Central Maintenance System (CMS) General -45-05 CMS/Aircraft General-45-20 CMS/Airframe Systems-45-45 Central Maintenance System-45-50 CMS/Structures-45-60 CMS/Propellers-45-70 CMS/Power Plant-46-00 Information Systems - General-46-10 Airplane General Information Systems-46-20 Flight Deck Information Systems-46-30 Maintenance Information Systems-46-40 Passenger Cabin Information Systems-46-50 Miscellaneous Information Systems-49-00 Airborne Auxiliary Power - General-49-10 Power Plant-49-20 Engine-49-30 Engine Fuel And Control-49-40 Ignition And Starting-49-50 Air-49-60 Engine Controls-49-70 Indicating-49-80 Exhaust-49-90 Oil-50-00 Cargo And Accessory Compartments General -50-10 Cargo Compartments-50-20 Cargo Loading Systems-50-30 Cargo Related Systems-50-40 Available-50-50 Accessory Compartments-50-60 Insulation-52-00 Doors - General-52-10 Passenger/Crew-52-20 Emergency Exit-52-30 Cargo-52-40 Service-52-50 Fixed Interior-52-60 Entrance Stairs-52-70 Door Warning-52-80 Landing Gear-53-00 Fuselage - General-54-00 Nacelles/Pylons - General-54-10 Nacelle Section-54-50 Pylon-55-00 Stabilizers - General-55-10 Horizontal Stabilizer or Canard-55-20 Elevator-55-30 Vertical Stabilizer-55-40 Rudder-56-00 Windows - General-56-10 Flight Compartment-56-20 Passenger Compartment-56-30 Door-56-40 Inspection and Observation-57-00 Wings - General-57-10 Center Wing-57-20 Outer Wing-57-30 Wing Tip-57-40 Leading Edge and Leading Edge Devices-57-50 Trailing Edge and Trailing Edge Devices-57-60 Ailerons-57-70 Spoilers-57-90 Wing Folding System-61-00 Propellers/Propulsors - General-61-10 Propeller Assembly-61-20 Controlling-61-30 Braking-61-40 Indicating-61-50 Propulsor Duct-62-00 Rotors-63-00 Rotor Drives-64-00 Tail Rotor-65-00 Tail Rotor Drive-66-00 Folding Blades/Pylon-67-00 Rotors Flight Control-71-00 Power Plant - General-71-10 Cowling-71-20 Mounts-71-30 Fire seals-71-40 Attach Fittings-71-50 Electrical Harness-71-60 Air Intakes-71-70 Engine Drains-72-00 Engine Turbine/Turbo Prop Ducted Fan/Unducted Fan-72-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted GearDriven Propulsor)-72-20 Air Inlet Section-72-30 Compressor Section-72-40 Combustion Section-72-50 Turbine Section-72-60 Accessory Drives-72-70 By-pass Section-72-80 Propulsor Section (Rear Mounted) -73-00 Engine Fuel And Control - General -73-10 Distribution-73-20 Controlling-73-30 Indicating-74-00 Ignition - General-74-10 Electrical Power Supply-74-20 Distribution-74-30 Switching-75-00 Air - General-75-10 Engine Anti-Icing-75-20 Cooling-75-30 Compressor Control-75-40 Indicating-76-00 Engine Controls - General-76-10 Power Control-76-20 Emergency Shutdown-77-00 Engine Indicating - General-77-10 Power-77-20 Temperature-77-30 Analyzers-77-40 Integrated Engine Instrument Systems -78-00 Exhaust - General-78-10 Collector/Nozzle-78-20 Noise Suppressor-78-30 Thrust Reverser-78-40 Supplementary Air-79-00 Oil - General-79-10 Storage-79-30 Indicating-80-00 Starting - General-80-10 Cranking98 *Reserved for Airline Use99 *Unassigned100 *Do not use101 *Do not use102 *Do not use103 *Do not use104 *Do not use105 *Do not use106 *Do not use107 *Do not use108 *Do not use109 *Do not use110 *Do not use111 *Do not use112 *Do not use113 *Do not use114 *Do not use115 Flight Simulator Systems。

B737NG训练手册-中文版 80-00-00_发动机起动

起动机通过发动机附件齿轮箱（AGB）转动发动机 N2 转子。
发动机电子控制器（EEC）
在起动过程中 EEC 保护发动机。在一次起动过程中当 EEC 发现发动机的参数是超过极限时，EEC 就关断至发动机的燃油供给。
显示电子装置（DEU）
显示电子装置（DEU）是公用显示系统（CDS）的部件。DEU 监控 N2 并在起动机断开时使发动机起动电门回到 OFF（关断）位置。
发动机起动电门
你把发动机起动电门放在 GRD（地面）位置用起动机转动发动机。在起动机断开后，电门自动移到关断位置。
当电源和气压动力可用时，当你把起动电门放在 GRD（地面）位置时，发生如下：
— 发动机电子控制器（EEC）收到起动信号 — APU 收到发动机起动信号 — 起动活门打开和气动起动机转动发动机。
有效性 YE201
—11—
80—00—00
发动机起动 — 起动机
目的
起动机为发动机起动或冷转程序转动发动机。起动机改变空气压力为机械能。
具体说明
起动机有一个单级，轴流，涡轮空气马达。起动机使用减速齿轮和一个制动离合器转动连接至发动机附件齿轮箱（AGB）的输出轴。
减速齿轮减速且离合器脱开。起动机输出轴然后随齿轮箱和发动机转动。涡轮和减速齿轮继续减慢直至它们停止为止。
有效性 YE201
—12—
80—00—00
发动机起动 — 起动机
告诫：不要用传动轴悬吊起动机。能够发生起动机内部的损坏。
80—00—00—005 Rev 1 10/13/96
有效性 YE201
—13—
80—00—00
80—00—00—005 Rev 1 10/13/96
下气压起动机管道组件联轴器

B737NG训练手册-中文版 34-58-00_全球定位系统

实物描述
MMR 为 ARINC-600 标准的 3MCU 组件，宽 3.6 英寸、高 7.9 英尺、长 14.6 英寸，无源冷却。MMR 重 10 磅，用 115 伏 400 用交流电工作。
34—58—00—006 Rev 8 11/02/1999
有效性
YE201
34—58—00
34—58—00—006 Rev 8 04/07/1998
MMR 利用这些数据进行系统初始化，并有助于在卫星信号覆盖不好时系统的工作。
MMR 数据输出总线
MMR 输出如下数据：－ GPS 纬度－ GPS 纬度（精值）－ GPS 经度－ GPS 经度（精值）－ GPS 时间和日期－ GPS 状态－水平品质指标－水平完好性限度
有效性 YE201
控制段
34—58—00
GPS — 工作原理 — 2
34—58—00—007 Rev 3 05/16/1997
有效性
YE201
34—58—00
安装螺丝孔
34—58—00—007 Rev 3 02/13/1997
有效性 YE201
顶视图
不准涂漆
插座ቤተ መጻሕፍቲ ባይዱ底视图
GPS — GPS 天线
34—58—00
GPS — 工作原理 — 1
空白页
34—58—00—008 Rev 3 01/05/1998
时钟
时钟使用 GPS 时间及其数据
近地警告计算机（GPWC）
MMR 向 GPWC 送出如下 GPS 参数：－纬度（粗值）－经度（粗值）－纬度（精值）
34—58—00
GPS — 接口
－经度（精值）－地速－真航迹角－高度－垂直速度－水平精度扩散因子（HDOP）－垂直精度扩散因子（VDOP）－水平品质指标（HFOM）－垂直品质指标（VFOM）－日期－时间（世界协调时）－水平完好性限度（HIL）－传感器状态

飞行记录本中英文对照

目录第一部分航线填本常用语句范例......检查发现 (1)参考/按....更换（件）......，检查/ 测试正常 . (2)检查发现...故障，按...保留，...号/类别，同意放行 (4)按...，更换...件，测试正常，撤消/ 关闭...保留 . (4)遭遇鸟击 (5)为判断...故障/因为航材缺件，对串...件，测试... . (6)更换......件，试车检查.. (7)第二部分飞机/故障基础知识飞机概况 (7)方位描述 (9)航材 (10)故障描述 (10)解决故障 (13)第三部各章节单词和故障描述用语A T A21空调 (16)A T A22自动驾驶 (18)A T A23通信 (20)A T A24电源 (23)A T A25设备和装饰 (25)A T A26防火 (27)A T A27飞行控制 (29)A T A28燃油 (33)A T A29液压 (35)A T A30防冰/防雨 (37)1A T A31指示/记录系统 (38)A T A32起落架 (45)A T A33灯 (49)A T A34导航 (53)A T A35氧气 (59)A T A36气源系统 (61)A T A38水和废物 (62)A T A44客舱系统 (64)A T A49辅助动力装置 (66)A T A52门 (68)A T A55安定面 (71)A T A71动力装置 (71)A T A73发动机燃油和控制 (73)A T A74点火 (74)A T A75发动机空气 (74)A T A76发动机控制 (74)A T A77发动机指示 (78)A T A78排气 (79)A T A79发动机滑油 (79)A T A80起动 (80)2第一部分航线填本常用语句范例……检查发现/报告故障……1. 航后：检查发现左后航行灯不亮。

AF ：Checked and found L AFT NA V light was not on.Do AF Check and find L aft position light does not work.Do AF Check and find L aft navigation light does not work.Do Task：TZ-AF-01，find L aft position light does not work.Do Task：TZ-AF-01，find L aft navigation light does not work.2. 检查发现右前轮销磨损超标。

ATA100章节名称中英文对照

20
VHF
甚高频
30
PA & Pass. Entertainment
旅客广播与娱乐系统
40
Interphone
内部通话
50
Audio Integrating
60
Static Discharging
静电放电
70
Voice Recorders
舱音记录器
24
00
ELECTRICAL POWER
电源
10
Generator Drive
loaddistributionequipfurnishingsflightcompartmentpassengercompartmentbuffetgallerylavatorycargoaccessorycompartmentemergencyfireprotectiondetectionextinguishingflightcontrolsailerontabruddertabelevatortabhorizontalstabilizercontrolflapsspoilerdraggustlockdampenerliftaugmentingfuelstoragedistributiondumpindicationshydraulicpowermainauxiliaryindicatingicerainprotectionairfoilairintakespitotandstaticwindowswindshieldsantennasradomespropellersrotorswaterlinesdetectioninstrumentspanelsindependentinstrumentslandinggearmaindoorsnosedoorsextensionretractionwheelsandbrakes空调压缩分配增压控制加温冷却温度控制湿度调节自动驾驶放大作动控制指示传感偶合通讯高频甚高频旅客广播与娱乐系统内部通话静电放电舱音记录器电源交流发电直流发电外部电源电源分配设备与装饰驾驶舱座舱餐柜厨房盥洗室货舱与附件舱应急防火火警探测灭火飞行操纵副翼与调整片方向舵与调整片升降舵与调整片水平安定面控制逢翼扰流板与阻力阵风锁定与阻尼升力增益燃油储存分配放泄指示液压主系统辅助系统指示防冰与防雨机翼剖面引气皮托管和静压管窗户与风挡天线与雷达螺旋桨旋翼水管探测仪表面板独立面板起落架主起落架与舱门前起落架与舱门放下与收起机轮与刹车system系统33343536373849515253545556sub

B737NG ATA章节中英文对照表

区域温度控制和指示
62
TRIM AIR PRESSURE REGULATION AND SHUTOFF CONTROL
配平空气压力调节和关断控制
73
OZONE
臭氧
21
74
HUMIDITY CONTROL
湿度控制
75
PACK SUPPLY AIR CLENAER SYSTEM
组件供气清洁系统
22
00
AUTO FLIGHT
释压活门
33
CABIN PRESSURE INDICATION SYSTEM
客舱增压指示系统
45
DOOR AREA HEATING SYSTEM
门区域加热系统
51
PACK FLOW CONTROL AND COOLING SYSTEM
组件流量控制和冷却系统
61
ZONE TEMPERATURE CONTROL AND INDICATION
滑油勤务
14
POTABLE WATER
饮用水勤务
15
MISCELLANEOUS REPLENISHING
杂项补充
16
WINDOWS
窗
17
WASTE TANK
废水箱
20
AIRPLANE LUBRICATION
飞机润滑
21
PERIODIC LUBRICATION
间隔润滑
22
PERIODIC LUBRICATION
乘务员座椅和面板
27
FLOOR COVERING
地板覆盖物
31
GALLEYS
厨房
40
LAVATORIES
厕所
25

737缩写中英对照

acc
Aｃｃumulator
聚集器
ＡＣC
Aｃcｅssory
附件
ACＦＴ
Aircraft
航空器
ACK
Ackｎowｌeｄgｅ
确认;肯定；证实
ACＭ
AｉｒCycleMacｈine
涡轮冷却器
ACMS
ＡirＣonｄitiｏnMonitｏrinｇSｙｓteｍ
空气环境监控系统
ACP
Ａｕdｉo CoｎtrolＰanel
CＭD
Coｍmand
命令;控制
ｃmptr
Ｃomputｅr
计算机
ＣNＸ
Caｎcｅｌled
取消;删除
CＯ
Captain
机长
ＣOAX
Coaxiａｌ
同轴的；共心的
ＣOMＭ
Cｏｍmunicatｉon
通信;联络
ｃoｍp
Coｍｐrｅssor
压气机；压缩机
CON
Cｏntinuｏｕs or Mａximum Coｎtinuous Tｈrusｔ
EAＤI
EｌectｒonicＡttitude DｉrｅctionＩndｉcator
电子姿态指引仪
ECON
Economy
经济
EＤP
EngineDriｖe Pump
发动机驱动泵
EDSＤ
ElｅcｔｒoｓtaｔｉｃDischaｒｇeSenｓitive Device
静电放出敏感装置
EEＰROM
EleｃtricErasaｂｌe Programmａble RｅadOnｌyＭｅｍo
数模适配(转换)器
DACS
DigiｔaｌAudioＣｏｎtrolＳystem
数字音频控制系统

B NG飞机勤务手册中文版

B737NG飞机勤务手册B737NG飞机航线勤务培训内容1.勤务概述2.燃油勤务（1）补加燃油限制和注意事项（2）补加燃油准备工作（3）压力加燃油程序（4）燃油系统放沉淀3.液压油箱勤务（1）液压油箱油量检查（2）液压油箱油量补加4.发动机滑油勤务（1）发动机滑油量检查（2）发动机滑油补加5.IDG滑油勤务（1）I DG滑油量检查（2）I DG滑油补加6.饮用水系统勤务（1）饮用水系统排放（2）饮用水箱加水7.起落架轮胎勤务（1）起落架轮胎压力检查（2）主起落架和前起落架热轮胎压力检查（3）起落架轮胎勤务8.污水箱勤务9.飞机拖行10.飞机登机门、勤务门和货舱门的开/关11.飞机停放规定12.气源车使用二、图1所示，为对飞机勤务时，各勤务车辆的位置；三、图2所示，为飞机勤务点的位置。

图1图21.补加燃油时限制和注意事项：（1）勤务区域应在户外进行，航空器应停放在使救援与消防设备易于接近的区域。

（2）在任何一种可能导致人员和设备等不安全状况发生时，立即停止加油程序。

（3）加油过程中应注意观察加油车各种仪表运行是否正常，发现异常，应停止加油。

检查飞机有无燃油渗漏，在翼尖有无燃油溢出。

（4）如在加油过程中发生溢油时：A.立即停止加油。

B.卸掉APU负载，并使APU停车。

C.按照《民用航空器行业标准》上的程序进行处理。

（5）在加油过程中，不要使用飞机的HF通讯系统；不要连接或断开电瓶充电器、其它地面电气部件；不要对电源设备进行测试。

（6）不要对氧气瓶进行勤务。

（7）不要断开电源。

（8）在发动机火警或过热以及起落架温度异常高的情况下，不要加油。

（9）在加油前，要确保轮挡不要接触到轮胎。

（10）确保所加燃油规格是适用的。

（11）不要使用宽馏分的燃油。

（12）确保加油设备良好。

2.加油准备程序：（1）给飞机供电（可以使用飞机电瓶和地面电源）。

（2）加油时，飞机机头向下1.140,这样可以加更多的燃油。

（3）在加油前，需要给燃油箱放沉淀。