AMM手册的使用
空客飞机AMM,IPC,TSM手册使用
The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS CHINA LTD. will be pleased to explain the basis thereof.
D&O
PB 001 PB 201
S
PB 301
Any Removal or Installation or Deactivation or Reactivation
R/I
PB 401
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: Any Approved Repair: 批准的修理:
CLM
Component Location Manual
TEM
Tool & Equipment Manual
MMEL CDL
Configuration Deviation List (m) ATA MMEL/CDL Ref. Ref.
MPD
Maintenance Planning Document
AWM
- the component location - the system/component description - the power supply (if applicable) - the interfaces with other systems (if applicable) - the operation/control & indicating - the BITE test. - 部件位置 - 系统及部件描述. - 供电 (如适用) - 与其他系统的交连 (如适用) - 系统工作/控制& 指示 - BITE 测试. This part contains the necessary data to understand the functioning of a system. 本部分内容有助于了解系统的功能.
飞机维护手册(AMM)简介
11
制定“ATA SPECIFICATION 100 ”的 工作于1956年完成。
“ATA SPECIFICATION 100 ” 为世界 绝大多数国家所接受。它使世界各国的航 空器设计、制造、使用、维护等部门，在 各种技术资料、文件、函电、报告和商品 目录索引等方面统一了编号，从而方便了 查阅资料和技术交流，同时还改进了各种 资料和文件的归档和管理，为走向国际标 准化的资料管理创造了条件。
3
机务人员培训手册;
第三类手册 飞行机组培训手册;
机群可靠性报告等。
这类手册是制造厂提供的参考性文件。
以上手册，构成一个完整的手册体系，它为 飞机正常维护、修理提供了全面的技术支持，对 机务管理工作程序化、标准化、科学化的目标提 供了便利。
民航总局为维护航空公司利益，于1991年颁 发了AC-121AA-04"运输类飞机持续适航文件"， 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。
维修方案解决的是什么时间去干什么。法定 技术文件中的各类手册是解决如何干的问题。
上述两项内容构成维修企业维修工作规范。民 航总局所颁发的民用航空器维修行业标准，对维 修行为又作了规范，使全行业维修工作达到安全、 有效的目的。
9
§ 1·4 手册的管理
作为法定技术文件的手册，成为维修方案的 构成部分，直接纳入适航部门检查、监督范围。 手册的完整性与可靠性，则成为工程部门首先要 考虑的问题。根据机队规模、机型多少，航空公 司分别设立资料室 (组)、资料科、资料处对手册 实施全方位地管理和控制。这些管理，事实上己 从飞机引进先期准备即已开始，谈判确定资料项 目、数量、分配方案，接收工作 (飞机交付前接 收项目、随机接收项目)资料上报工作以及资料 更新责任划分。
飞机维修的各种手册介绍-manual
手册内容
1
MPD的内容包括飞机维修计划、维修程序、工作 单卡、航材信息等，涵盖了飞机的各个系统和部 件的维修要求和操作流程。
2
手册中还包括了维修人员的资质要求、工具设备 清单、安全注意事项等内容，以确保维修工作的 顺利进行。
3
MPD的内容会根据飞机型号、维修要求以及适用 的法规进行定期更新和修订，以适应新的维护需 求和技术发展。
手册使用方法
查阅方式
维修人员在进行飞机维护时，应首先查阅AMM以确认所需 的维护程序。
更新与修订
随着技术的进步和法规的变更，AMM需要进行定期的更新和 修订。因此，维修人员应关注手册的版本信息，并使用最新版
本。
培训与授权
由于AMM包含高度专业化的信息，维修人员在使用前应接受 相关培训并获得授权，以确保他们具备执行手册中所述工作的
更新与修订
ACARS手册会定期进行更新和修订，以反映最新的飞机维护技术和行 业标准。维修人员需要定期获取最新的手册版本，以确保遵循最新要按照手册中的步骤和指南进行操作，以确保飞机维修工作的正确性和安全性 。在执行维修任务时，应始终参考手册中的最新版本。
飞机维修的各种手册 介绍
目录
CONTENTS
• 飞机维修手册（AMM） • 航空器持续适航和安全改进措施手册
（ACARS） • 飞机维修计划文件（MPD） • 飞机维修工单系统（AWOS）手册
01 飞机维修手册（AMM）
手册概述
定义
飞机维修手册（AMM）是航空公司或 维修组织用于指导飞机维护和修理工 作的官方文件。
能力。
02 航空器持续适航和安全改 进措施手册（ACARS）
手册概述
定义
ACARS是航空器持续适航和安全改进措施手册的简称，它是一份重 要的飞机维修手册，旨在确保航空器的持续适航性和安全性。
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。
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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
空客飞机AMM,IPC,TSM手册使用
TEI
Tool & Equipment
Index
TED
Tool/Equipment Drawing
CMM
Component Maintenance
Manual
部件翻修手册
SES
Support Equipment Summary
Tool Drawing Status工具图纸状态
Y --> TEI
Technical Data Support & Services
Presented by
Name
JobTitle
AMM 及相关手册 AMM & Associated Products
AMM – General 飞机维护手册 – 概述
WHEN YOU WORK ON AIRCRAFT USE THE AMM 当在飞机上工作时使用 AMM
Table of Contents (TOC)
DThee spucrporsiepotfithoenD &&O isOto pexpelarina: tion (PB 001) 系 统系统描描述述&工&作部工分是作为了(解P释B: 001)
- the component location - the system/component description - the power supply (if applicable) - the interfaces with other systems (if applicable) - the operation/control & indicating - the BITE test.
D&O
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]
![AMM手册的使用[1]](https://img.taocdn.com/s3/m/35a670c39ec3d5bbfd0a74ac.png)
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
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常用操作
I B M B l a d e C e n t e r A M M常用基本操作一．登录AMM (3)二．开启I/O模块外部端口 (3)三．登录I/O模块配置界面（Telnet或Web界面） (4)四．打开Remote Control界面 (6)五．查看I/O模块等的VPD信息 (8)六．查看如刀片服务器等部件的Firmware信息 (9)导读：本文仅对几个常用入门操作进行简单说明。
如果您初次接触A M M，并且上述目录中列出的几个操作您又需要使用，请参考。
如果您经常接触A M M或是资深的系统管理员，本文对您没有技术上的提高以及深入的帮助。
如有深入的需求，请参考A M M用户手册。
A M M常用基本操作（注：本文适用于A M M，但由于微码版本区别界面可能会稍有不同）一．登录AMM在浏览器地址栏中输入A M M的I P地址，（默认为192.168.70.125）会打开如下图登录界面，输入用户名（U s e r I D）和密码（P a s s w o r d）。
（默认用户名为U S E R I D，密码P A S S W0R D，其中0是数字0。
）二．开启I/O模块外部端口默认情况下，I/O模块外部端口为D i s a b l e状态，即外部端口不可用。
在左侧导航栏中选择I/O M o d u l e T a s k s下的A d m i n/P o w e r/R e s t a r t选项，打开如下图所示界面。
在右侧主界面的I/O M o d u l e A d v a n c e d S e t u p下选择需要操作的I/O模块（S e l e c t a m o d u l e）然后选择E x t e r n a l P o r t s为E n a b l e d，点击右下的S a v e按钮保存。
三．登录I/O模块配置界面（Telnet或Web界面）如果要对I/O模块如以太网交换模块进行配置，可以选择I/O M o d u l e T a s k s选项下的C o n f i g u r a t i o n菜单，会打开如下图界面。
空客A320-AMM维护手册使用介绍
28 - 21 - 51
Component (unit) level, breakdown allocated by Manufacturer
部件,
由飞机制造商划分
Sub-sub-system level, breakdown allocated by
Manufacturer
次Su级b-分sy系st统em, 由飞机l制ev造el商, b划re分akdown allocated by ATA 100 Spec.
Keyword – Page Block (PB) 关键字 – 页段 (PB)之间的关系
Description & Operation 系统描述&工作
Any Standard Maintenance Practices:
e.g. pressurizing, jacking, energizing... 任何标准施工: 如: 增压, 顶飞机, 通电
The purpose of the D & O is to explain: 系统描述&工作部分是为了解释:
- the component location - the system/component description - the power supply (if applicable) - the interfaces with other systems (if applicable) - the operation/control & indicating - the BITE test.
Any Adjustment or Test: 调节/测试:
Any Inspection or Check 检查/检验:
Any Cleaning or Painting: 清洁/喷漆:
空客飞机AMM IPC TSM手册使用
分系统
按 ATA 100 规范划分
Chapter 章
level, breakdown allocated by ATA 100 Spec. 按 ATA 100 规范划分
AMM – Breakdown 内容划分
Manual Front Matter page (手册首页) Highlights (only AirN@v) 更改重点 (只在AirN@v 中) Chapter 00 – Introduction (章节00 - 手册介绍) Fleet No. / MSN cross ref table (FSN / MSN 交叉索引表) SB list (SB 清单) COC list (COC 清单)
D&O
Description and Operation 系统描述&工作
MP
Maintenance Procedures 维护程序
AMM – SB List 服务通告清单
AMM – SB List 服务通告清单
AMM – SB List 服务通告清单
Keyword – Page Block (PB) 关键字 – 页段 (PB)之间的关系
例行维护程序
NON-SCHEDULED MAINTENANCE PROCEDURES
非例行维护程序
MRB
MPD
FM CDL
MEL
TSM
AMM – General 维护手册 –概述
The AMM provides detailed information required to maintain the aircraft at line or in the hangar. AMM 维护手册提供航线和定检维护时所需的详细技术信息 This does not include workshop information which is contained in the CMM.
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
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• 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
不再写在AMM中，现在第五章的内容只包含非定时性的维修检查。而原来 停场封存数据专门成册的出版物，现在写在AMM手册11章中。
1.概述
• 从某种意义上讲，AMM手册就是所有针对航线可更换件
LRU进行的维护步骤和程序的集合。
• AMM手册是由飞机制造厂商发布的，依据各种组件、系统、
• 最后是型别号（Configuration Number），如果前缀是空白那么也是空白，如
果前缀使用型别号00表示不适用的情况。
4.飞机维护工卡辅助系统AMTOSS
代码 00 10 说明 拆卸 清洁
20
30 40 50 60 70 80 90
检查，检验
修正，修理 安装 飞机和设备的装卸运输 勤务，存放，润滑 测试，检验 杂项 更换＝拆卸＋安装
3. AMM手册的有效性
• 三、 AMM 的每一页都存在有效性的问题
• 1、在手册每一页的左下方的有效性栏（Effectivity Block）记载了该页
的有效性，有效性为“All”，说明该页适用于手册所对应机队的所有飞机， 注意，维护手册的有效性是针对特定页的。
• 2、某些页由于记载了不同厂商生产的飞机部件是不惟一的。这时，你
上安装的设备或装置外，不需要专用工具设备，并且，测试项目和机组 执行的测试相差无几。组件操作测试不必满足特定的规范和容限。
• 功能测试 Functional Test • 这项程序需要判定某系统或组件所有功能正常并符合系统或组件的最小
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。
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。
耗材的编号表示
4.飞机维护工卡辅助系统AMTOSS
工作单的编号
4.飞机维护工卡辅助系统AMTOSS
ADI的相关信息 •（1）查找并记录ADI在飞机的位置 •（2）查找并记录ADI的拆装步骤及 其注意事项
5. 习题
•6、查找737-300型飞机上第二部甚
高频通讯系统天线的位置和天线的 拆装步骤，同时记录相应章节目录 页码。
5. 习题
油、水和轮胎气压。
• 勤务工作在手册其它章内也能
找到，这些内容作为维护工作 完成后的勤务工作，包括项目 有对减震支柱的充气或充油， 控制钢索的润滑，及饮用水系 统的消毒工作。
2. AMM的结构
2. AMM的结构
• 401-499 拆卸/安装 Removal/Installation
2. AMM的结构
• 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，表中把
该章所被更改的内容及更改的时间一一列出。
• AMM是针对机队编写的文件。
• 例如，现在我们要查找放电刷的检查的内容，我们知道这部分内容要在
AMM 上进行查找。
• 在查找内容之前，我们应先确定被查找的飞机的机队，然后再找到为该
机队编写的AMM。
• 这个步骤很重要，同一型别的飞机如不属于同一机队，则AMM 的内容
是不相同的。
3. AMM手册的有效性
• 系统测试 System Test • 这项程序包含所有的调节规定和容限，以使系统和组件的特性保持在最
大效能和设计规范。这项测试应是独立的并与其它多次测试完全一样。 一般情况下，本测试用于重要维护周期。
2. AMM的结构
• 601-699 检验/检查 Inspection/Check • 确定某个零件、组件、系统的适用性和执行某一功能操作的零件的特殊
Maintenance Practices (MP) Servicing (SRV) Removal/Installation (R/I) Adjustment/Test (A/T) Inspection/Check (I/C) Cleaning/Painting (C/P) Approved Repairs (AR) Dispatch Deviation Guide (DDG)
— 故障报告手册是故障发生时，如何使用故障代码等形式进行报告。 — 这部分内容原载于AMM手册201-299页, 而新手册201-299页则是描述 组件在飞机中的位置。
• 此外，新手册还增加了放行偏离指南（DDG），以对应最低设备清单
（MEL）的内容。
• 因此在不同机型的AMM手册中，未熟练使用前，先应熟悉各页码段的内
容，以方便查询。
2. AMM的结构
• 001-009 说明及工作 Description and Operation • 101-199 部件位置 Component Location
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、
5.飞机维护工卡辅助系统AMTOSS
• 分工作单的编号
• 分工作单是工作单的一
部分，它的编号标在每 个分工作单前一行。
• 编号的内容除功能代码
（Function Code）较 详细外基本与工作单编 号相同。
5. 习题
•1、737-200型飞机（B-2516）气象雷达
系统（Airplanes With Sperry Primus 90 Weather Radar）的相关查询 •（1）查找并记录气象雷达系统部件及 位置 •（2）查找气象雷达天线的拆装步骤， 同时记录相应章节目录页码 •（3）查找气象雷达收/发组的拆装步骤， 同时记录相应章节目录页码
• • • • • • •
工作单的编号写在工作单的工作程序上面一行。 “TASK”是标明这个编码。 之后三组数字是该工作内容隶属的“章号-节号-目号”。 功能代码（Function Code）则标明该工作的性质，如：00，拆除；10清洁等。 页码的第一位，如：4表示拆装；和功能代码一起说明工作的内容。 序列号（Sequence Number）标示如果以上号码都相同的不同工作单的排序。 前缀（Prefix）表示了工作的几种状态： — 空白标示该工作是5-49章中飞机没有型别差异的内容； — “0”标示5-49章中飞机有不同型别的内容； — 49章中空白“A”“B”标示不同型号的APU； — “B”标示结构51-57章内容； — “C”标示发动机70-80章内容。
• 工作程序中还有很多分内容和分步骤，这构成了一张完整的工作单。 • 专用工具设备是指为了这项工作专门制作的工具； • 通用工具设备是指飞机制造厂家设计制造的多个工作都可以使用的工具，
而不是指那些在工具箱中使用的螺丝刀等一般工具；
4.飞机维护工卡辅助系统AMTOSS
• 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
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。
“（新）”表示使用在新近机型的手册中如737-800等
2. AMM的结构
• 新的手册（波音737-600/700/800/900飞机）中，将飞机系统和组件的
故障查找和故障隔离，另外编写了两本手册分别为故障隔离手册FIM （空客公司称为故障定位手册TSM）、故障报告手册FRM。