05 AMM手册

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飞机维护手册(AMM)简介精编版

客户化手册有:

● 维护手册

●线路图册

● 图解零件目录

● 系统图册

● 发动机手册

● 机载测试设备手册。
这类手册没有通用性，各航空公司之间不可互用，他们之间修改版次也不一样。
2.通用化手册
通用化手册在各用户之间是可以通用的，其修改版次也是一致的。
通用化手册有:

飞机维护手册体系及使用简介
§1 飞机维护手册体系
§1·1 飞机维护手册体系的组成
制造厂作为一种技术支援形式，在向用户交付飞机之时，提供一系列的手册。共有三类手册:

飞机飞行手册 (AFM);
第一类手册
维修大纲 (MRB);

最低设备清单 (MMEL)。
这类手册需经民航总局审查批准或认可。这些审查、批准工作是在型号合格审查时进行的。
●翻修手册

●结构修理手册

● 图解工具和设备手册

● 无损探测手册

● 防腐手册

● 布线施工手册等。

§ 3 飞机维护手册

Airplane Maintenance Manual
一、概述
维护手册是由主机厂按ATA-100编号规范要求编写的，手册量很大，范围也广，其内容包括对安装在飞机上所有系统和设备实施各种勤务、维护、检查、排除故障、系统功能试验、调节、清洁、修理和更换零部件等工作的详细技术标准和程序、检查手段、使用的工装、消耗性器材及安全操作要求……等等。

维修手册 (M M)，

翻修和零部件维护手册 (OH/CMM);

结构修理手册(SRM);

AMM手册的使用

经批准的修理和适当处的特定步骤的组合。
• 当要求的维护程序不长并相对简单时，以上的组合组成到“维护施工”
标题下。
2. AMM的结构
• 301-399 勤务 Servicing • 勤务程序包含在其他维护工作
通常要求的程序中，勤务程序应该是独立的，并可常规化或可恢复。
• 勤务包括如燃油、滑油、液压
ቤተ መጻሕፍቲ ባይዱ
• 最新版本（波音737-600/700/800/900飞机）的维护手册在工作的分类上，
将通用性、原理性的信息另成一册称为系统描述部分SDS（Systems Description Section）继承了原来（波音737-300/400/500飞机）在01-99 页部分的概述内容，由于这部分内容的错误不涉及工作内容，波音公司可以免责。
关系等所需的详细程序。
2. AMM的结构
• 701-799 清洁/涂漆 Cleaning/Painting
2. AMM的结构
• 801-899 核准修理方法
2. AMM的结构
• 901-999 放行偏离指南 Dispatch Deviation Guide
3. AMM手册的有效性
• 一、 AMM 是客户化的文件
2. AMM的结构
• 501-599 调试/测试 Adjustment/Test • 调节/测试部分提供所有程序和参数以评估执行功能操作的系统、子系统、
单元、部件或零部件之间的连接件的操作有效性和完整性。
— 操作测试 — 功能测试 — 系统测试
2. AMM的结构
• 操作测试 Operational Test • 这项程序仅为了证实某系统或组件可正常工作，这些测试除了使用飞机
• 而原有的第五章定时性检修的数据，都写在维修计划数据MPD中，这部分

飞机维护手册(AMM)简介课件

参考资料
列出了一些重要的参考资料和标准，用户可以通过这些资料进一步了解和维护飞机的相关知识和技术要求。
03
AMM手册的编写规范和要求
语言和文字规范
总结词：准确、清晰、专业详细描述：使用准确、简练的语言描述飞机维护操作，避免使用模糊或含
糊不清的措辞。
总结词：易于理解
详细描述：使用简单易懂的语言，避免使用过于专业或复杂的术语，确保手册易于阅读和理解。
说明
对维护程序的详细解释和说明，包括操作步骤、注意事项、安全要求等。
图表和插图
图表
通过各种图表直观地展示数据和信息，如零件更换周期表、故障率曲线图等。
VS
插图
插图部分提供了飞机各个部件的示意图，帮助用户更好地理解飞机结构和维护操作。
附录和参考资料
附录
附录部分包含了手册编制过程中使用的各种表格、公式和数据，方便用户在维护过程中随时查阅。
A
B
C
D
环保性
数字化手册减少了对纸张的依赖，有利于环境保护。
交互性
数字化手册可以加入多媒体元素，提供更丰富的信息呈现方式，如动画、视频等，提高阅读和理解效率。
数字化手册的实现方式
电子文档格式
采用PDF、DOC、XLS等电子文档格式，通过文件存储和传输实现数字化。
在线平台
建立在线平台，将手册内容发布在平台上，用户通过账号登录访问。
详细描述
遵循行业或公司内部的引用和注释规范，统一使用标准的引用格式，如APA、MLA 等。
04
AMM手册的数字化发展
数字化手册的优势
可更新性
数字化手册可以随时更新，保证信息的准确性和时效性，减少因手册过时而导致的

飞机维修的各种手册介绍

感谢您的观看
主要系统介绍
01
02
03
04
动力系统
包括发动机、螺旋桨等，提供飞机飞行所需的动力。
液压系统
用于控制飞机的各种机械运动，如起落架收放、襟翼调节等
。
电气系统
提供飞机各系统的电力供应，包括发电、配电和用电设备。
航电系统
包括导航、通信、飞行控制等电子设备，保障飞行安全。
结构与系统关系
结构承载系统
飞机维修的各种手册介绍
目录
• 飞机维修手册概述 • 飞机结构与系统手册 • 飞机维修程序手册 • 飞机维修技术手册 • 飞机维修工具与设备手册 • 飞机维修安全与质量管理手册
01 飞机维修手册概述
维修手册定义与作用
维修手册是一种详细描述飞机及其系统、部件的维修要求、程序和方法的技术文件。
它是飞机维修工作的重要依据，为维修人员提供准确、可靠的维修指导，确保飞机安全、经济、可靠地运行。
技术手册使用指南
01
02
03
手册查阅方法
介绍如何快速查找所需信息，包括目录结构、索引和关键词搜索等技巧。
手册更新与替换
说明手册的更新周期和替换流程，确保维修人员使用的是最新版本的手册。
手册使用注意事项
提醒维修员在使用手册时需要注意的事项，如遵守安全规定、保持手册整洁等。
技术更新与手册修订
系统故障
如发动机熄火、液压系统泄漏等，需根据具体情况进行相应的维修和更换。
航电故障
如导航设备失灵、通信中断等，需及时检查和修复相关设备。
应急处理
在紧急情况下，需采取相应的应急措施，如关闭故障系统、启用备用设备等，以确保飞行安全。

AMM手册查询教材R1

AMM手册查询1AMM手册概述1.1 用途飞机维护手册(Aicraft Maintenance Manual，AMM)提供航线和定检维护时所需要的详细技术信息，包含系统及部件的工作描述、勤务、修理、更换、调节、检查的必需信息和正常在停机坪或维护机库完成飞机检查所需要的工具设备。

该手册可以用来满足维修人员工作和培训的需要。

1.2 手册有效性1.2.1客户化手册任何维修文件都有有效性(Effectivity)，也就是此文件的适用性，即该维修文件是针对哪种机型制定的，对哪些飞机有效。

一般定义为：维修文件的有效性是指该文件是否适用于指定飞机及机载设备的依据。

维修文件对应飞机的有效性可以体现在以下4个方面：客户化(机型、机队有效性)、飞机型别号码(单架飞机的有效性)、型别特征(装备系统、APU、发动机的有效性)、时效性(手册改版的有效性)。

AMM手册为客户化的手册。

通过FSN（机队序列号）来确定有效性。

1.2.2飞机识别号一架飞机从设计、实验、成批的生产到投入运行，过程是非常复杂的，也是非常严谨的，每一个过程都会有一些代表该过程的编号，这些编号用以对机型进行识别，同时，也用来确定各类手册、服务通告、适航指令等的有效性。

在各手册前言都有飞机有效性对照表，以方便用户查询手册时了解手册有效性。

1.2.3空客飞机有效性对照表A.机队序列号(Fleet Serial Number，FSN) 航空公司机队的飞机按照顺序编号，如：001、002。

B.飞机构型(Version Rank) 如：G8E01 0010、G8E01 0011。

C.飞机型号(Model) 如：320-214。

D.厂家序列号(Manufacturer Serial Number，MSN) 某一机型持续生产的编号，如：0772、0799。

E.注册登记号(Registration)如：B-2360、B-2361。

1.2.4手册修订AMM手册修订分为：定期修订临时修订TR临时修订的内容包含在List of Effective TemporaryRevisions（LETR）中，客户可以通过Airbus-World 和CD的形式获得最新的临时修订，在收到临时修订后应尽快将其上传至AirNav/Maintenance中。

AMM手册的使用[1]

2. AMM的结构的结构
2. AMM的结构的结构
• 401-499 拆卸安装 Removal/Installation 拆卸/安装
2. AMM的结构的结构
2. AMM的结构的结构
• 501-599 调试测试 Adjustment/Test 调试/测试 • 调节/测试部分提供所有程序和参数以评估执行功能操作的系统、子系统、
4.飞机维护工卡辅助系统飞机维护工卡辅助系统AMTOSS 飞机维护工卡辅助系统
• 耗材是指在工作中使用的消耗性材料，它的第一个字母标明该材料的性
质。 “A”表示粘结剂、填充剂、封严剂； “B”表示清洁剂、光洁剂； “C”表示整修材料； “D”表示滑油、润滑脂、固体润滑剂等润滑介质； “E”表示除漆、除胶等的清除剂； “F”表示焊接材料； “G”表示复合材料。
是不相同的。
3. AMM手册的有效性手册的有效性
• 二、 AMM 的时效性
• AMM 手册的内容并不是从飞机投入飞行至对出服役一成不变的。 • 由于飞机在飞行过程中，需要进行组件的更换，或是根据航空公司的要
求进行系统的改装，这样一来，AMM的内容就要发生变化。
• 在AMM 每一章的索引中第一部分就是关于时效有效性的列表时效有效性的列表，表中把时效有效性的列表
TECHNICAL TRAINING
FOR INFORMATION ONLY
05 AMM手册手册
1.概述概述
• 飞机维护手册（AMM）是外场维护用到频率很高的一本手册，是飞机工作
人员的工作指南，这本手册的内容丰富、充实、多样。而且，在维修文件历史的传承中，出现了很多维护手册内容的分支，因此不同时代出现了不同内容的维护手册，新旧不同版本的维护手册的内容也不尽相同。

AMM手册的使用说明

Version: B2, B3INTRODUCTION1.Authority approvalA.The technical content of this document is approved under authority of DOA EASA21J056.B.When the name EUROCOPTER is found in the documentation, you should readAirbus Helicopters.2.Purpose of the ManualA.The Aircraft Maintenance Manual (AMM) is designed to provide helicopteroperators with the necessary information to ensure the maintenance of thehelicopter.B.The AMM contains maintenance, inspection and repair data for the Operationaland Intermediate levels only.Whenever the repair criteria defined in the AMM are exceeded, please contactthe Airbus Helicopters network for the definition of a repair, if applicable, or thedecision to discard the component.C.The following publications are associated with the operation and maintenance ofthe helicopter:-The Component Maintenance Manual (CMM).-The Flight Manual (FLM).-The Illustrated Parts Catalogue (IPC).-The Illustrated Tool Catalog (ICO or Chapter 13 of the IPC).-The Master Servicing Manual (MSM).-The Standard Practices Manual (MTC).-The Wiring Diagram Manual (WDM).-The Index of Modifications (SIM).-The Structural Repair Manual (SRM) (if exists).The modifications listed in the Index of Modifications (SIM) havebeen dealt with in the maintenance documentation, but may nothave any impact on the documentation.In addition to the AMM, the corresponding engine publications (EMM) areprovided with each helicopter delivered.(1)Identification: Information for warehouse staff-Illustrated Parts Catalog (IPC)-Illustrated Tool Catalog (ICO or Chapter 13 of the IPC)(2)Special: Time-sensitive information-Service Bulletin (SB)-Alert Service Bulletin (ASB)3.Definition of required maintenance levels for application of the repairsThe various maintenance tasks are classified in levels so as to take into account the complexity of the tasks, the place of execution of the operations, the equipment and the training of the personnel.For structural repair requirements, these levels are defined by the letters "O", "I", "I+"and "D":-“O” LEVEL (Operation Level): This refers to implementation of simple structural repairs, carried out during line maintenance by the crew and/or line mechanicsusing limited equipment, in order to maintain the operational capability of theaircraft.-“I” LEVEL (Intermediate level): This refers to implementation of small repairs on or out of the aircraft, in a repair workshop using fixed facilities, by skilled,trained and qualified personnel, in order to restore the operational capability ofthe aircraft or equipment.For the "O" and "I" levels, repairs may be carried out in accordancewith the instructions of Airbus Helicopters publications: AMM /SRM / MTC.The rules defined for the "O" level are applicable to the "I" level.-“I+” LEVEL: This refers to implementation of repairs on the primary structure or on stressed composite parts, with the approval of the Airbus HelicoptersTechnical Support Department,. In a Repair Center mandatorily approved by Airbus Helicopters,. Or with mandatory Technical Assistance from Airbus Helicopters if the work iscarried out of an Airbus Helicopters Approved Repair Center,. Or with the assistance of an Airbus Helicopters Approved Repair Center if the work is performed out of an Airbus Helicopters Approved Repair Center.“I+” level repairs require approval from the Airbus HelicoptersTechnical Support Department. The repair work must be approvedby Airbus Helicopters ("I+" specific maintenance documentation, orspecific repair sheet submitted to Airbus Helicopters for approval),or transmitted to Airbus Helicopters if already approved by thesupervisory authorities of the repair workshop. The "I+" level workcards are identified in the work card title.The rules defined for the "I" level are applicable to the "I+" level.-"D" LEVEL: This corresponds to repairs which affect the interchangeability of major structural couplings or the general geometry of the aircraft, using toolingwhich ensures interchangeability, by a maintenance center and specialists dulyqualified by Airbus Helicopters.The supply of documentation (SRMD), tooling and "D" level spareparts is reserved for "D" level Maintenance Centers qualified byAirbus Helicopters.An aircraft cannot be reconstituted using the identification plateof an aircraft which has been declared scrapped by AirbusHelicopters without the prior written approval of Airbus Helicopters.The rules defined for the "I+" level are applicable to the "D" level.Airbus Helicopters reminds you that it is forbidden to reuse structural parts orassemblies which have been involved in an accident without prior approval from the Airbus Helicopters Technical Support Department.The major structural couplings are the following:Landing gear attachment points, MGB bar attachments, attachment points ontransmission deck, engine mount attachment points, fuselage/tail boom junction,horizontal stabilizer-Fenestron junction and TGB attachment points.4.Following up the technical publicationsA.The manuals are valid only if they are regularly kept up to date by the users.The Updating department is governed by the “General Terms and Conditions ofSale” appended to any contract.Documentation may be distributed in three formats: Paper/DVD/PDF (e-techpub).B.Advice to operatorsPaper manuals that have not been kept up to date must not be used forhelicopter maintenance. They must be destroyed on the spot or clearly marked“documentation not up to date”.DVDs must be replaced when each new revision is issued. A DVD that pre-datesthe latest revision must not be used for helicopter maintenance.The e-techpub documentation is updated directly on the Internet.5.Updating the manualA.Normal Revision (NR)Paper issue:-The Maintenance Manuals are updated by a regular updating system. The revision completely or partially updates the manual. The revisions are issuedwith the modification instructions (Highlights).The user or operator is responsible for ensuring that only the correct issueof the manual is used. The effectivity of the manual is indicated on the titlepage.-All the modifications (new, canceled or superseded pages) made to the manuals must be incorporated and recorded in the update list.-Follow the Highlights: these will ensure that the manual is compliant with its new composition, each chapter complying with its own list of effective pages(LOEDU).-The modifications are identified as follows:. All modifications to, additions to or deletions from a text or modifications toa figure are indicated by a black line in the margin.. If part of the text is relocated this may result in changes to the numbering ofthe pages, tables or figures but these changes are not indicated.. All the pages of a modified page block show the modification date.PDF issue:-The Maintenance Manuals are updated by a regular updating system. The revision completely or partially updates the manual. The revisions are issuedwith the modification instructions (Highlights).The user or operator is responsible for ensuring that only the correct issueof the manual is used. The effectivity of the manual is indicated on the titlepage.-The modifications are identified as follows:. All modifications to, additions to or deletions from a text or modifications toa figure are indicated by a black line in the margin.. If part of the text is relocated this may result in changes to the numbering ofthe pages, tables or figures but these changes are not indicated.. All the pages of a modified page block show the modification date.DVD issue:-The Maintenance Manuals are updated by a regular updating system. The revision completely or partially updates the manual. The revisions are issuedwith the modification instructions (Highlights).The user or operator is responsible for ensuring that only the correct issue ofthe manual is used. The effectivity of the manual is given by the "LOIM" (listof manuals included in the DVD-ROM).. If part of the text is relocated this may result in changes to the numbering ofthe pages, tables or figures but these changes are not indicated.. All the pages of a modified page block show the modification date.6.Temporary Revision (TR)A.GeneralBetween two Normal Revisions, Airbus Helicopters may need to makemodifications to points of the manual considered important; this will be donethrough temporary revisions. The Temporary Revision deals with informationwhich requires quick distribution and which cannot wait until the next normalrevision is issued.Several Temporary Revisions may be issued between two Normal Revisions.The new, revised or deleted Documentary Units (DU) are issued on yellow colorpaper. The changes are indicated by a vertical line in the margin.Temporary Revisions are identified by the number of the next Normal Revisionfollowed by a letter (taken in alphabetical order) and a date code.position and updatingThe Temporary Revision is composed of an "Update instructions" section, a Listof Effective Pages of the Temporary Revision, one (or several) List(s) of EffectivePages for the chapter(s) and one (or several) Documentary Unit(s).The "Update instructions" section gives a list of the highlights of the TemporaryRevision. This information is issued with each new Temporary Revision (TR).The List of Effective Pages of the Temporary Revision (LOEDU-TR) identifiesthe chapters modified by all the Temporary Revisions. The date code associatedwith the Documentary Unit corresponds to the date of the Temporary Revision at which it was modified. This list is issued with each new Temporary Revision and supersedes the previous one. It must be inserted at the beginning of the manual in the preliminary Documentary Units and kept until the next Normal Revision (RN).The List of Effective Pages of the chapters "XX-LOEDU-TR" identifies the new, revised or deleted Documentary Units of the chapters affected by the Temporary Revisions. The date code associated with the chapter corresponds to the date of the TR at which it was modified. Only the List of Effective Pages of the modified chapters are issued. These lists must be inserted at the beginning of the chapters concerned and they cancel and supersede the previous ones. They must be retained until the next RN.New, revised or deleted Documentary Units:-For a new Documentary Unit: the new yellow-colored Documentary Unit must be inserted directly in the manual.-For a revised Documentary Unit: all the pages of the yellow-colored revised Documentary Unit cancel and supersede all the pages of the white-colored Documentary Unit concerned. This white-colored Documentary Unit must be removed from the manual.-For a deleted Documentary Unit: only the first page of the Documentary Unit that must be removed is issued on yellow-colored paper through theTemporary Revision. This page bears the word "DELETED". It cancels and supersedes all the pages of the white-colored Documentary Unit concerned.This white-colored Documentary Unit must be removed from the manual.ALL TEMPORARY REVISIONS INCORPORATED INTOTHE MANUAL MUST BE RECORDED IN THE RECORD OFTEMPORARY REVISIONS.PDF issue:The Temporary Revision is composed of "Highlights", a List of Effective Pages of the Temporary Revision, one (or several) List(s) of Effective Pages and one (or several) Documentary Unit(s).The "Highlights" list the major points of the Temporary Revision. This information is issued with each new Temporary Revision.The List of Effective Pages of the Temporary Revision (LOEDU-TR) identifiesthe chapters modified by all the Temporary Revisions. The date code associated with the Documentary Unit corresponds to the date of the Temporary Revision at which it was modified. This list is issued with each new Temporary Revision andsupersedes the previous one. It must be inserted at the beginning of the manualin the preliminary Documentary Units and kept until the next NR.The List of Effective Pages of the chapters "LOEDU-TR" identifies the new,revised or deleted Documentary Units of the chapters affected by the TemporaryRevisions. The date code associated with the chapter corresponds to the date ofthe TR at which it was modified. Only the List of Effective Pages of the modifiedchapters are issued.DVD issue:The Temporary Revision is composed of "Highlights" and one (or several)Documentary Unit(s).The "Highlights" list the major points of the Temporary Revision. This informationis issued with each new Temporary Revision.The "Highlights" of the Temporary Revision identifies the DUs modified by all ofthe Temporary Revisions. The date code associated with the Documentary Unitcorresponds to the date of the Temporary Revision at which it was modified. Thislist is issued with each new Temporary Revision and supersedes the previousone. The manual revision date code is indicated in the "LOIM".ALL TEMPORARY REVISIONS INCORPORATED IN THEMANUAL MUST BE RECORDED IN THE RECORD OFTEMPORARY REVISIONS.7.ErratumThis procedure is used to correct composition errors that do not in any way affect the technical data involving flight safety and the certification of the aircraft. This procedure is used to correct these errors rapidly and is completely separated from the revisions.The date code marked on the replacement page is underlined but it remainsunchanged.Consequently, the page enclosed with the erratum page must replace the pageissued previously.8.PreprintPreprint is a preliminary edition, which is used to transmit an update of the technical documentation in advance of the normal process of management and publication of the information.This procedure is used:-to reply to a customer after he has reported irregularities that require changes to the technical publications,-to introduce new parts and/or systems not included as part of technical publications supplied by Airbus Helicopters.Airbus Helicopters approves the contents of the data transmitted by Preprint.For the approved parts (certification), no page can be sent beforeapproval is granted by the authorities.Rules for the Preprint diffusion process:-The Documentary Units are printed on salmon-colored paper.-The Documentary Units bear the word "PREPRINT" in the diagonal.-The Documentary Units are identified by a new date code.-The Documentary Units must be inserted in place of the modified Documentary Units.Airbus Helicopters preferably transmits the Preprints electronically.In any case no preliminary edition will remain as is. It will always be followed bythe standard procedure of revision (TR and RN). The DUs must be removed by the customer upon receipt of the corresponding DU TR and/or DU RN which take into account the modifications transmitted through Preprint.position of the manualThe Aircraft Maintenance Manual (AMM) is made up of two parts:-Part I of the manual contains all the descriptive type data for all the systems. This Part I is called Systems Description Section (SDS). It is physically separated from Part II and is totally self-contained.-Part II contains the data required for the maintenance and fault isolation operations and procedures.10.Structure of the manualThe AMM is broken down into several levels in accordance with the ATA Specification No.100, Revision 31, with a "Chapter - Section - Subject" numbering system that uses six digits.11.Structure pagesThe AMM contains a series of pages called "Structure pages". They contain general instructions and/or guidelines to find the information.The structure pages contained in the AMM are as follows:-Update instructions.-Title page.-Record of temporary revisions.-List of effective pages of the manual.-Introduction.-List of Service Bulletins.-List of chapters.12.Chapter structure pagesEach chapter starts with a List of Effective Pages of the Documentary Units (LOEDU).This list gives the aircraft version or aircraft serial number effectivity of eachDocumentary Unit.13.Breakdown into chaptersThe manual is broken down into chapters, in accordance with the ATA 100Specification.The chapter below was added:Chapter 01:-List of Materials (in AMM Part II).-List of Critical Parts (depending on aircraft).The numbering principle for the Manual is a breakdown into Chapter - Section -Subject, in a digital form:-the first three digits are given by the ATA 100 SpecificationExample: 62-2x-yz62-2 Main Rotor (system)-the last three digits are left at the manufacturer's disposal:. digit x to complete a sub-system number,. digits yz to complete a sub-sub-system number.Example: 62-2x-yz62-21 Main Rotor Hub (sub-system)62-21-11 Spring vibration damper (sub-sub-system)14.Chapter breakdown into topics (SDS section)Inside the chapters of the manual, the subjects are broken down into topics which gather tasks depending on the maintenance operations.The System Description Section gives explanations on the location, use, description and operation of the complete system and its sub-systems.This section is designed so that it can be used as a training manual.The identification comes in the form of a series of Documentary Units (DU).There are two title levels:-The higher level represents a set of information of the same type (e.g.: General, General Description, Detailed Description, etc.). All the illustrations of a"Documentary Unit" are grouped at the end of this Documentary Unit.Each UD is broken down into subsets.These subsets represent a group of paragraphs.Each subset begins with a title (Introduction, Description, Characteristics,Operation, etc.).15.Chapter breakdown into topics (AMM section)A.Fault IsolationThis section gives the information for the ground maintenance teams to locatefailures and faulty operation and to determine the necessary corrective actions.This topic comes in the form of a table:-The first column "Failure Indication" gives a detailed description of the fault.-The second column "Probable Cause" lists the possible causes of the fault, in the logical fault isolation order.-The third column "Corrective action" indicates the action(s) to be taken to correct each possible cause of the failures listed.B.Maintenance tasksThese topics describe the processes which allow the ground maintenancepersonnel to carry out the maintenance, removal/installation, adjustment, checkoperations, etc.When the task is given for reference, the Chapter - Section - Subject number is followed by the task number:Example: 62-21-00, 4-1 Removal - Main rotor hubIf an instruction requires the execution of a task, its reference number appears between brackets at the end of the instruction.Example: Remove main rotor hub (62-21-00, 4-1).Depending on aircraft configuration, the reference number of the task may be preceded by a configuration number. The selection of this configuration number is the responsibility of the operator.ex: conf 001 62-21-00, 4-1,ex: conf 002 62-21-00, 4-1Further to changes in aircraft configuration, compliance with a Service Bulletin, change of component part number ("Manufacturer Part Number") or a series production modification, the maintenance task can be followed by a configuration letter. The selection of the configuration letter is the responsibility of the operator. Example: 62-21-00, 4-1a Removal - Main rotor hub (PRE MOD 07xxxx) Example: 62-21-00, 4-1b Removal - Main rotor hub (POST MOD 07xxxx)Each task contains the information below:-List of Applicable Documents1. Main informationContains references to other tasks that are essential to carry out theprocedure.2. Conditional informationContains references to other tasks the application of which in the procedure depends on the maintenance environment, the choice or skills of thecustomer.3. General informationContains references to other tasks containing information that is supposedly known by the operator, as well as the code of the manual(s) where suchinformation can be found.-List of special toolsThis is the list of the special tools required to carry out the Task. These "special" tools are those that are not normally available to the maintenance personnel. These tools are identified with their "part numbers" and descriptions.These special tools are listed in the ICO (or in Chapter 13 of the IPC).Certain tools (not listed in the ICO (or in Chapter 13 of the IPC) and not normally available to the maintenance teams) are identified by the term "Commercial" to indicate that they are purchased "off the shelf".-List of MaterialsThis is the list of the consumable materials required to carry out the Task. They are identified with a "CM" code and their description.Details of the products that correspond to these codes are given in W.C.20-01-01-102 of manual MTC.The 20-01-01-102 of MTC describes the "NATO" code, the different references of the French, German and US Specifications and the list of the source products. It also refers to the implementation procedures described in the Standard Practices Manual (MTC) for certain products.Certain materials are identified by the term "Commercial". This means that they can be purchased off the shelf.-List of Routine Replacement PartsThis is the list of the parts discarded and replaced during a Task.This list comes in the form of a table:-the first and second columns give the position of the part (text/figure/set),-the third column gives the name of the part,-the fourth column gives the part number (MP/N).-Job Set-up (optional)This topic specifies how to prepare the helicopter for the work to be done.-ProcedureThe procedure is described in the form of a logical sequence of phases, broken down as follows:(1) phase(a) sub-phase of (1)1 sub-phase of (a)a sub-phase of 1The figures and tables are numbered in chronological order so that they can be used for several phases inside the same Task.All the figures inside a Task are gathered at the end of the Task.The items are identified in a continuous ascending order starting with Item 1 on Set 1 and finishing with Item n on Set m. If a part appears on several figures/sets, it shall always have the same item number.Figure 401 is the first figure in a "Removal / Installation" topic.Table 602 is the second table in an "Inspection / Check" topic.A figure can include several sets. In this case, the figure number remains the same, and only the set number is changed.Furthermore, the items are defined on all the sets of the figure.Figure 401 (Sheet 1)Figure 401 (Sheet 2)If there are no specific indications of the tightening torques onthe figures, then the tightening torque values are the Standardtorque values. To determine this standard value, refer to (MTC20-02-05-404).-Special NotesUSED TO EMPHASIZE A MAINTENANCE OPERATION ORPRACTICE, A CONDITION, A STATEMENT, WICH IF IT IS NOTSTRICTLY RESPECTED MAY CAUSE SERIOUS INJURY ORDEATH.USED TO EMPHASIZE A MAINTENANCE OPERATION ORPRACTICE, A CONDITION, A STATEMENT, WICH IF IT IS NOTSTRICTLY RESPECTED MAY DAMAGE OR DESTROY ANEQUIPMENT ITEM OR PREVENT FULL COMPLETION OF THEMISSION.Used to emphasize an operation or a condition that with help thepersonnel or simplify a maintenance procedure.-Close-up (optional)This topic specifies how to return the helicopter to its initial configuration (asbefore the maintenance operation).16.SymbologyAll the symbols used in the maintenance publications (SDS and AMM Part II) are explained in the following table.17.List of AbbreviationsAFNOR: Association Française de Normalisation (French Industrial Standards Association)ALL P/N: All part numbersAMM: Aircraft Maintenance ManualASU: Ancillary System UnitCBP: Circuit-Breaker PanelCHK: Condition Check - Airworthiness limitationCM: MaterialCMM: Component Maintenance ManualCSS: Chapter - Section - SubjectD: DayDC: Direct CurrentE: Maintenance Due TimeEASA: European Aviation Safety AgencyELT: Emergency Locator TransmitterEMB: Electrical Master BoxEMM: Engine Maintenance ManualESD: Electrostatic Discharge Sensitive DeviceFC: Functional Check (quantitative)FLM: Flight ManualFM: Log cardH: HourHP: High PressureHT: Hard TimeHz: HertzICS: Intercommunication SystemIGE: In Ground EffectIPL: First Limitation IndicationLACU: Lighting and Ancillaries Control Unit LED: Light-Emitting DiodeLH: LeftLP: Low pressureM: MonthMOD 07 xxxx: ModificationMOD AL xxxx: Minor (simplified) modification MOD OP xxxx: Modification of optional equipment MGB: Main GearboxMP/N: Manufacturer's Part NumberMRH: Main Rotor HubND: Not DescribedNF: Free Turbine rpmNR: Rotor rpmOAT: Outside Air TemperatureOC: On Condition (check, maintenance)OGE: Out of Ground EffectOPT: OptionalOTL: Operating Time LimitPCB: Printed Circuit BoardPTT: Push To TalkRH: RightSDS: System Description SectionSLL: Service Life LimitS/N: Serial NumberSP: Static PressureTBD: To Be DefinedTBO: Time Between OverhaulsTGB: Tail GearboxTP: Total PressureTRH: Tail Rotor HubTSI: Time Since InstallationTSM: Time Since ManufactureU: Operating CycleVEMD: Vehicle & Engine Multifunction DisplayW: WeekWDM: Wiring Diagram ManualY: Year18.GlossaryATTACHMENTThe visual check is carried out on the attachment points of a component (condition of the safetying, marks on self-locking nuts). It may be necessary to complete this examination with a tactile check (manual application of a load on the component to detect any fault in the assembly).CHECKA check consists in comparing the measurement of a magnitude (force, time,pressure, temperature, length, etc.) with a theoretical value. The resulting actionconsists in bringing back this magnitude to a value that ranges within its tolerances, through adjustment or a maintenance action (e.g.: check of tightening torques, check of play, etc.).CLEANLINESSThe cleanliness check consists in making sure that there is no foreign matter, no fluid seepage or splashes and no "fouled" areas likely to conceal a fault.CONDITIONThe visual examination concerns the general external condition of a component and the points that could modify its initial condition (deformation, breaks, cracks, scores, corrosion, signs of overheating or wear).。

AMM手册的使用

AMM手册基本上都是严格按照ATA100格
2. AMM的结构
维护手册AMM依据ATAl00的章节划分形式“**--**--**”划分。
除此之外维护手册根据自身的性质，按照工作的不同内容，将页码分成不同的区段。
页码的第一位是功能位，代表该页码段的工作内容和性质。
页码的后两位是顺序的页码，表明的是每
最新版本（波音737-600/700/800/900飞机）的维护手册在工作的分类上，将通用性、原理性的信息另成一册称为系统描述部分SDS（Systems Description Section）继承了原来（波音737-300/400/500飞机）在01-99页部分的概述内容，由于这部分内容的错误不涉及工作内容，波音公司可以免责。
2. AMM的结构
201-299 维护措施 Maintenance Practices “维护施工”是勤务、拆卸/安装、调整/测试、检查/检验、清洁/喷
漆、经批准的修理和适当处的特定步骤的组合。当要求的维护程序不长并相对简单时，以上的组合组成到“维护施
工”标题下。
2. AMMபைடு நூலகம்结构
301-399 勤务 Servicing
TECHNICAL TRAINING
FOR INFORMATION ONLY
05 AMM手册
1.概述
飞机维护手册（AMM）是外场维护用到频率很高的一本手册，是飞机工作人员的工作指南，这本手册的内容丰富、充实、多样。而且，在维修文件历史的传承中，出现了很多维护手册内容的分支，因此不同时代出现了不同内容的维护手册，新旧不同版本的维护手册的内容也不尽相同。
最小容许要求和设计规范。这些测试可能要地面支援设备，比操测试要更具体，更详细，为了使系统或组件的可靠性保持在一个可接受水平，这些测试应包括完成熟练测试的所有必需的内容。此测试不用参考额外的文件。功能测试一般发生在较短的维修周期。

波音空客AMM手册一般介绍

AMM 手册介绍介绍主要以空客手册为主，MD82 和 MD90 飞机的手册与空客手册基本内容一致。

1. 概述飞机维护手册（AMM）是按照 ATA 100 规范编制的。

飞机维护手册含有正常在停机坪或者在维护机库中完成的，对飞机设备和系统的保养，修理，调节，检验和检查所需信息。

飞机以外设备所需的信息包含在厂家或者制造厂的部件维护手册中。

飞机维护手册也含有关于飞机结构的检查和维护的信息。

当然，结构的修理包含在结构修理手册或短舱结构修理手册内。

用于排除故障所必需的信息被包含在排故手册中。

飞机维护手册含有完成维护评审委员会（MRB）文件和相应维护计划资料（MPD）规定的定期维护程序所必要的数据。

手册中使用公制和非-公制测量系统。

在原来的参考文件里使用的度量衡单位数值先列出，然后在括号中换算成另一单位的量值。

客户代码和修订日期出现在每页的底部，修订日期可以是原版日期，修订日期或者最新版日期。

2. 手册划分飞机维护手册分成各章节飞机概述章时限/维护检查...... 5 尺寸和区域...... 6 顶起与支撑...... 7 校水平和称重...... 8 牵引和滑行...... 9 停放和系留 (10)铭牌和标志...... 11 勤务...... 12 飞机机体系统标准实施-机身...... 20 空调 (21)自动飞行...... 22 通讯...... 23 电源...... 24 设备/装饰...... 25 防火...... 26 飞行操纵...... 27 燃油...... 28 液压源...... 29 防冰和防雨...... 30 指示/记录系统...... 31 起落架...... 32 灯...... 33 导航系统...... 34 氧气...... 35 气动系统...... 36 水/废水 (38)机载辅助电源...... 49 结构结构 (51)舱门...... 52 机身...... 53 短舱/吊架...... 54 安定面...... 55 窗...... 56 机翼 (57)动力装置标准实施-发动机…… 70 动力装置…… 71 发动机…… 72 发动机燃油和控制…… 73 点火…… 74 空气…… 75 发动机操纵…… 76 发动机指示………… 77 排气…… 78 滑油…… 79 起动…… 80 2.1 章节划分规则每个章/系统细分成节/子系统（结合功能/自然组）。

AMM手册查询

AMM手册查询
AMM手册查询
AMM手册由飞机制造厂商发布，手册严格按照ATA100格式编写，页码格式“##__##__##”，页码第一位是功能位，代表该页码段的工作内容性质；后两位是顺序的页码，代表每页的排序，各页码段的具体如下：
01 - 99 说明及工作
101-199 故障及分析
201-299 维护措施
301-399 勤务
401-499 拆卸/安装
501-599 调试/实验
601-699 检验/检查
701-799 清洁/涂漆
801-899 授权维修
901-999 放行偏离指南
在AMM手册中，工作单一般分为两个部分，第一部分是概述（General）用来介绍工作的性质和内容，第二部分是工作单的主体，主体又被分为多项，依次是介绍，专用工具设备，通用工具设备，耗材，参考的其他手册或章节，接近盖板，工作程序。

其中工作程序中又细分工作准备，工作步骤，工作检验，工作恢复等。

这就构成了一张完整的工作单。

耗材的第一个字母标明该材料的性质：
“A”表示粘合剂，填充剂，封严剂
“B”表示清洁剂，光洁剂
“C”表示整修材料
“D”表示滑油，润滑介质
“E”表示除漆，除胶的清除剂
“F”表示焊接材料
“G”表示复合材料
工作单的编号，如“TASK 75-31-01-40 4-008-c 00”
“TASK”是这串编码的标识符，“75-31-01”表明该工作隶属的“章号-节号-目号”“40”表示。

空客AMM维护手册使用介绍

D & O
MP
Description and Operation 系统描述&工作 Maintenance Procedures 维护程序
Technical Data Support & Training - ACSM
3/1/20204
AMM – Breakdown 内容划分
AMM Breakdown is easily displayed in AirN@v TOC
Any Removal or Installation or Deactivation or Reactivation 拆卸/安装, 或失效/ 恢复使用 Any Adjustment or Test: 调节/测试:
Any Inspection or Check 检查/检验:
Any Cleaning or Painting: 清洁/喷漆:
车间附件修理的技术信息不在AMM 而在 CMM 中.
The AMM is structured into ATA chapters and further into sub-systems and units as required. AMM维护手册按需要划分成ATA章节, 分系统和主题(部件)
Reference breakdown example: 例如:
Any Approved Repair: 批准的修理:
Technical Data Support & Training - ACSM
D&O
PB 001 PB 201
S
PB 301
R/I
PB 401
D/R
A/T
PB 501
I/C
PB 601
C/P

AMM手册培训课件

拆卸/安装(R/I)在部/附件层面(XX-XX-XX),本标题提供了拆卸,安装或更换部件所需的所有数据。这些程序由两个独立任务组成,一个是拆卸任务,一个是安装任务。
对于拆卸任务:
因为安装任务通常在拆卸任务之后,所以认为结束程序是不适用的。在拆卸任务和安装任务之间有时间间隔,操作员可靠常识来估计决定采纳合适的结束程序。对于安装任务: 工作准备仅为将要执行主要操作如:开启跳开关,安装警告牌和工作平台等的提示.飞机维护构型提醒操作者必须保证在开始安装程序前,确认拆卸工作后的飞机构型得到核实。
2.2.1.e调节/测试(A/T)(501 到599 页)
1 操作测试: 此测试只用于确定系统或组件是否可用。除了安装在飞机上的设备,该试验正常情况下不需要特殊设备或厂房,其操作与飞行机组的试验相类似。 2 功能测试: 此测试用于根据最低配置系统或组件设计规格确定系统或组件各方面的功能。此测试可能需要附加地面支持设备,比操作测试更明确和详细。 3 系统测试: 此测试包含所有要将系统和/或组件的性能保持在最大效率和设计规格所需的所有调节规格和容差。
2 有三种类型的检查: a 详细检查(DI): 对特定部件、装配或组件的仔细检查以探测损坏、失效或者异常。亮度适当的良好直接光源通常补充有效照明。检查辅助工具,诸如:镜子, 放大镜等等..可能是必要的。需要表面清洗工作和详细的接近程序。 b 一般目视检查(GVI): 目视检查内部或外部区域,安装或组装来探查明显的损伤,故障或异常。该等级的检查在接触距离内进行,除非另有规定。如有必要,使用镜子以确保看到检查区域的全部表面。此等级的检查在正常有效的照明状况进行如: 白天,机库照明,手电筒或者下降灯并可能需要拆卸或者打开接近板或者门。可能需要台架,梯子或者平台以接近检查区域。 c 特别详细检查(SDI) 对特定部件、装配或组件的仔细检查以探测损坏、失效或者异常。此检查可能使用专门检查技术和/或设备。可能需要复杂的清洗工作和实质的接近或者分解程序。

最新2：飞机维修文件及手册查询(AMM)

AMM手册飞机维修手册的编排结构 ⑨维修服务通告清单(Service Bulletin List) ：
服务通告清单在包括服务通告号、服务通告涉及的ATA 章、通告状态、出版日期及其对手册有效性的影响等。在“Started/Completed”项目中,如果标有S ，则说明这份服务通告尚未完成，如果据有C，则说明这份服务通告巳经完成。
AMM手册飞机维修手册的编排结构 3．AMM的章节(Chapter)编排：由于AMM的章节较多，为了便于使用查找， AMM按章划分为四个分组。第一分组飞机维修通用部分ATA 5～12章： 5章：时间限制/维修检查（Time Limits/Maintenance Checks） 6章：尺寸和区域（Dimensions and Areas） 7章：顶升和支撑（Lifting and Shoring）
AMM手册飞机维修手册的编排结构 2．AMM的前言编排：
标题页飞机有效性对照表手册发送说明修订重点说明有效页清单章节有效性修订记录临时修订记录维修服务通告清单简介
AMM手册飞机维修手册的编排结构 ①标题页(Title) ：
AMM手册飞机维修手册的编排结构 ②飞机有效性对照表(Effective Aircraft) ：
（2）临时修订服务手册临时修订服务将根据需要发行。临时修订服务也可作为应用户要求结合服务通告而发行。每次临时修改将编入下次手册的修改中。每次临时修改会提供一组更新的页，这些页面在并入下次定期修改前或用其它的临时修改替代前仍然有效。
AMM手册飞机维修手册的编排结构 1．AMM的整体编排： AMM整体编排的结构也是按ATA规范100 的规则编排的，手册分为:临时修改(Temporary Revisions)、前言(Front Matter)、章节(Chapter) 组成。

飞机相关课件：05 AMM手册

容，以方便查询。
2. AMM的结构
• 201-299 维护施工 Ma intenance Practices • 对于某一组件来说，它的维护内容相对简单时，所有内容就全部列到
“维护施工 ”标题下。或者，对某组件的维护内容不能列到其他页码段时，也列到“维护施工 ”页码段内。
2. AMM的结构
• 除了以上的这些信息外，其他的可以分别到各系统章节，结构章节和发
动机章节中去查询。
4.AMM的使用和查阅
• 一种推荐的维护手册查找程序
• 维修手册依据ATA100规范划分，每一个章的内容依次编辑成有效性每
页清单、目录和内容。
• 由三组数字组成的章-节- 目号码对应某一LRU ，同时在IPC和WDM手册
4.AMM的使用和查阅
• 2、工作内容的查找：
• 工作内容的查找是维护手册最常见的查找问题，一般也最容易解决。 • 查找这部分内容的时候首先要区分工作的性质，是一般性的勤务工作，
还是属于标准施工的内容，还是属于非定期性的检修？ — 勤务工作是12章 — 标准施工按照系统、结构、发动机分别是20 、51 、70章 — 非定期性的检修是第5章的内容
故障隔离
维护施工勤务
拆卸/安装调试/测试
检验/检查
内容 Maintenance Manual
Description and Operation (D&O) Trouble Shooting (TS)
Maintenance Practices (MP) Servicing (SRV)
Removal/Installation (R/I)
关系等所需的详细程序。
2. AMM的结构

飞机维护手册 AMM 简介

为营运人购置或租赁飞机所应获得的技术文件提供了指导。
值得注意的是，第一、二类文件，制造厂有责任持续提供改版服务 (有偿)，而第三类手册是不受控的，仅作为培训资料，此类资料不允许用于生产。
手册另一种分类的情况见下图。
手册的分类：维修类、备件类、运行类
§ 1·2 手册的形式
1.活页手册直观、便于插入修改页
பைடு நூலகம்
飞机维修通用部分
5 Time Limits/Maintenance Checks
5章时间限制/维修检查
6 Dimensions and Areas
6章尺寸和区域
7 Lifting and Shoring
7章顶升和支撑
8 Leveling and Weighing
8章平衡与载重（校准与称重）
31章仪表
32 Landing Gear
32章起落架
33 Lights
33章灯光
34 Navigation
34章导航
35 Oxygen
35章氧气
36 Pneumatic
36章气源
38 Water/waste
38章供水/排污
49 Airborne Auxiliary Power
74章点火装置
75 Air
75章发动机进气
76 Engine Controls 76章发动机操纵
77 Engine Indicating 77章发动机指示
78 Exhaust 78章发动机排气系统
79 Oil
79章发动机滑油系统
80 Starting
80章发动机起动
82 Water Injecting
二、手册的作用本手册为在航线、机库及维修中心维护和修