AMM 及相关手册及相关手册AMM & Associated ProductsTechnical Data Support & ServicesPresented byNameJobTitle1AMM 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当在飞机上工作时使用 AMM FMCDLNON-SCHEDULED MAINTENANCE PROCEDURES非例行维护程序非例行维护程序MELTSMSCHEDULED MAINTENANCE PROCEDURES例行维护程序例行维护程序MPD MRB AMM2AMM General 维护手册 概述This does not include workshop information which is contained in the CMM.车间附件修理的技术信息不在车间附件修理的技术信息不在AMM 而在而在 CMM 中中.The AMM provides detailed information required to maintain theaircraft 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维护手册提供航线和定检维护时所需的详细技术信息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维护手册按需要划分成ATA章节章节, 分系统和主题分系统和主题(部件部件)Reference breakdown example: 例如例如:28 - 21 - 51 Component (unit) level, breakdown allocated by Manufacturer 部件部件, 由飞机制造商划分由飞机制造商划分Sub-sub-system level, breakdown allocated by Manufacturer次级分系统次级分系统, 由飞机制造商划分由飞机制造商划分Sub-system level, breakdown allocated by ATA 100 Spec.分系统分系统 按按 ATA 100 规范划分规范划分Chapter level, breakdown allocated by ATA 100 Spec.章章 按按 ATA 100 规范划分规范划分 3AMM Breakdown 内容划分Deactivation/Reactivation index - MMEL/CDL(失效失效/恢复使用程序恢复使用程序 TEI 参见参见TEIP - Contact Vendor 与厂家联系与厂家联系C - Refer to CMM 参考参考 CMM S - Standard tool 标准工具标准工具etcMAINTENANCE飞机维护飞机维护TEMTEISES15TLMC TimeLimitsMPD Section 9TEMTool & Equipment ManualATA Ref. Tool PNCMLConsumable Material ListMaterial NumberATA Ref.MPDMaintenance PlanningDocument Task numberATA Ref.PPIPCPower PlantIPCIllustrated Parts CatalogCSN / ATA Reference FINNSRMNacelleSRMStructural Repair ManualATA Ref.NTMNon-Destructive Testing ManualATA Ref.CLMComponentLocationManualATA Ref.CMMComponent Maintenance ManualATA Ref.SJCStandard JobCardsCCCGICJICExtractMMELCDLConfiguration DeviationListMMEL/CDL Ref.ATA Ref. (m)ATA Ref. FINAWM Task numberATA Ref.TSM AMM and associated manuals AMM 及相关手册16 AIRBUS CHINA LTD. All rights reserved. Confidential and proprietary document.This document and all information contained herein is the sole property of AIRBUS CHINA LTD. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS CHINA LTD. This document and its content shall not be used for any purpose other than that for which it is supplied.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.AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.17零备件资料介绍零备件资料介绍SPARE DATA FAMILIARIZATIONTechnical Data Support & ServicesPresented byNameJobTitle18Generalities 概述 LINE MAINTENANCE 航线维护航线维护= AIPC /PIPCAIPC = AIRFRAME ILLUSTRATED PARTS CATALOG 飞机图解零件清册PIPC = POWER PLANT ILLUSTRATED PARTS CATALOG发动机图解零件清册 SHOP MAINTENANCE 车间维护车间维护= CMM / ACMM / EIPCCMM = COMPONENT MAINTENANCE MANUAL 部件维护手册ACMM = ABBREVIATED CMM 简化部件维护手册EIPC = ENGINE IPC (发动机IPC)19Generalities 概述THE ILLUSTRATED PARTS CATALOG (IPC) IDENTIFIES:ALL LINE REPLACEABLE PARTS (REPAIRABLE & EXPENDABLE) such as : IPC 用于确认所有航线可更换件用于确认所有航线可更换件(可修理可修理&可消耗可消耗)的件号以用于航线维护及的件号以用于航线维护及 制定备件计划制定备件计划.例如例如: AIRBUS STRUCTURAL PARTS (空客结构件空客结构件) VENDOR COMPONENTS (厂家部件厂家部件) COMPONENT BREAKDOWN PARTS (部件分解件部件分解件) ATTACHING / INSTALLATION PARTS (连接连接/安装件安装件)USED FOR LINE MAINTENANCE & SPARES PLANNING PURPOSES 20IPC21ILLUSTRATION Installation figure 安装图图解GENERALZONING大致的区域大致的区域FRAME INFO隔框区间隔框区间DOTTED LINE CROSS REFDIFFERENT 6 digits 点划线索引到点划线索引到另一不同章节另一不同章节FIN NUMBER功能识别号功能识别号DETAILZONING详细区域详细区域ITEM NUMBER项次号项次号22ILLUSTRATION detailed figure 详图图解CROSS REF AMM链接到链接到AMMLine Maintenance Parts航线维护件航线维护件23DETAILED PART LIST 详细零件清单MATERIEL DOMAIN IPC FAMILIARIZATION24INSTALLATION BREAKOUT 安装图的划分To aid in rapid location of an illustration, the subject part of the CSN (digit 5 and 6) has been assigned as follows:为尽快确认安装图的位置, 章节号CSN的“主题”部分, 即第五,六位按如下划分:CHAPTER-SYSTEMCIRCUIT-SUBJECTSUBJECTXXXX01 to 09XXXX10 to 9025DETAILED PART LISTMATERIEL DOMAIN IPC FAMILIARIZATION26GENERAL SYSTEM OF ASSEMBLY ORDER The indenture system used in DPL shows the relationship of parts and assemblies to next higher assemblies in assembly order as follows:详细零件清单中的缩格关系表示上下级组件之间的关系详细零件清单中的缩格关系表示上下级组件之间的关系:1 2 3 4 5 6 7INSTALLATION. DETAILED PARTS FOR INSTALLATION. ASSEMBLY. ATTACHING PARTS FOR ASSEMBLY. . DETAILED PARTS FOR ASSEMBLY.SUB-ASSEMBLY. . ATTACHING PARTS FOR SUB-ASSEMBLY. DETAILED PARTS FOR SUB-ASSEMBLY.SUB-SUB-ASSEMBLY.ATTACHING PARTS FOR SUB-SUB-ASSEMBLY27AirNv DETAILED PARTS LIST (DPL) 详细件号清单FIGURENUMBER图号图号NOTILLUSTRATEDITEM无图解项无图解项PARTNUMBER件号件号ITEMNUMBER项次号项次号EFFECTIVITY有效性有效性REFERENCEITEM参考项参考项X-REFTODET链接到详图链接到详图QUANTITYPER CSN每个组件数量每个组件数量DATA REVISED YELLOW COLOR黄色为更改处黄色为更改处28AirNv DETAILED PARTS LIST (DPL) 详细件号清单CMM REFCMM 章节号章节号VENDORCODE厂家代码厂家代码NOTPROCURABLEITEM不可购买件不可购买件FIN REF功能识别号功能识别号29AirNv DETAILED PARTS LIST (DPL) 详细件号清单OPTIONALPN/VENDOR互换件号及厂家代码互换件号及厂家代码LOCAL MANUFACTURE可当地加工件可当地加工件BUY PN首选件首选件30Buyer Furnished Equipment (BFE) Identifies a part, which is furnished by the customer to AIRBUS to be installed in the A/C BFE项是由客户提供给空客安装到飞机上的31买方提供设备买方提供设备 - BFEBFE 是用户自己提供并安装到飞机上设备。是用户自己提供并安装到飞机上设备。 (例如例如: 厨房厨房, 麦麦克风克风, 救生衣救生衣, 娱乐设备等娱乐设备等).只有当从用户接收到有关只有当从用户接收到有关BFE的技术信息后的技术信息后(如相关的如相关的CMM, 图纸等图纸等)，BFE 设备才会被收录到手册中。设备才会被收录到手册中。(SFE: 即即Supplier Furnished Equipment)SFE: 卖方提供的设备卖方提供的设备32 NON PROCURABLE ITEM (NP)不可购买件不可购买件Appearing in the nomenclature column “NP” indicates that this item is not procurable (SPC =0). 在名称栏里在名称栏里NP表示此件号不能用于订购表示此件号不能用于订购 OPTIONAL PARTNUMBER (OPT TO)代用件号代用件号“OPT TO” xxxxxxxxx identifies a part fully interchangeable with the basic one shown in the part number column.表明此件与件号栏里的基本件号可完全互换表明此件与件号栏里的基本件号可完全互换IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单33 STORAGE PARTS 储存件储存件Parts needed to store the next higher assembly are comprised between the words “Storage parts” and dots “*”. Quantity given is for one stored part. 若储存上一级组件若储存上一级组件, 则同时需要则同时需要“Storage parts”和和 “*”之间所列之间所列的零件的零件, 所标数量用于储存一个上一级组件所标数量用于储存一个上一级组件. ALTERNATE PART NUMBER (ALT FROM)替换件号替换件号“ALT FROM” xxxxxxxx identifies a part, which is functionally interchangeable with the basic one shown in the part number columnonly after rework.表明此件在表明此件在经过重新加工经过重新加工后后, 与件号栏中的基本件号在功能上可以互换与件号栏中的基本件号在功能上可以互换.IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单34 PREFERRED SPARE PART (BUY PN)首选件号首选件号“BUY PN” xxxxxxx identifies an item which is recommended as the current preferred part for spares purposes. “BUY PN” 表明此件号被推荐为目前备件的首选件号表明此件号被推荐为目前备件的首选件号 LEFT HAND/RIGHT HAND INDICATORS左侧左侧/右侧指示右侧指示A/ Parts used on left hand or right hand of symmetrical installations are designed by “LH” or “RH”. 在对称的安装中在对称的安装中, 左侧和右侧件分别用左侧和右侧件分别用“LH” 和和 “RH”表示表示. B/ Parts , assemblies or installations used only on one side of the aircraft are designated by “(LH SIDE)” or “(RH SIDE)”. 零件零件, 装配件或组装件如只在飞机的一侧使用装配件或组装件如只在飞机的一侧使用, 则用则用“(LH SIDE)”或或 “(RH SIDE)”表示表示.IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单35 LOCAL MANUFACTURE (LM)当地加工件当地加工件“*LM*” identifies a part which can be locally manufactured.“*LM*” 表示此件可当地加工表示此件可当地加工.LM parts are listed in the IPC Additional Cross Reference Table as follows : LM 件在件在ACRT 手册中列有如下信息手册中列有如下信息:- Raw material to finished PN 原材料原材料 - 成品件号索引成品件号索引- Finished PN to raw material 成品件号成品件号 - 原材料索引原材料索引IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单 RESTRICTED USAGE (RU) 限制用于限制用于Exp. RU 010, means only used on item 010.例如例如 RU 010, 表示只用于表示只用于010项件号上项件号上Refer to effectivity of item 010. 参考参考010项的有效性项的有效性36DETAILED PART LIST 详细零件清单MATERIEL DOMAIN IPC FAMILIARIZATION37ONLY AIRCRAFT IDENTIFIED IN THE EFFECTIVITY TABLE ARE COVERED IN THE IPC 有效性表格列出有效性表格列出IPC涵盖的所有飞机号涵盖的所有飞机号38The absence of a restrictive effectivity at all items in one IPC figure indicates that the part is effective for all aircraft of a customers fleet.IPC图中如无有效性限制,则表明适用于机队的所有飞机39The effectivity shown is called “SPARES Effectivity”. The Spares effectivity is given in accordance with the interchangeability code between the parts and the A/C configuration.有效性也称备件有效性, 它是依据飞机的构型以及件号之间的互换性代码共同确定的.40RU 001B (RU= Restricted usage, 001B= Item 001B) means “only used on the assembly defined with item 001B”“限制使用限制使用”表示只用于表示只用于001B项件号上项件号上41DETAILED PART LIST 详细零件清单MATERIEL DOMAIN IPC FAMILIARIZATION42SERVICE BULLETIN HANDLING 服务通告的处理The integration of the PRE/POST Airbus SB in the IPC is in accordance with the policy between AIRBUS and AIRLINES.空客服务通告编入IPC依据空客与航空公司之间协议的政策.The reference of the PRE or POST Airbus SB is in the IPC to help users about the redundant effectivity.IPC中PRE和POST SB的表述, 为用户提供了两种可能的有效性.After airlines reporting the interim PRE/POST Airbus SB configuration is changed in POST SB only, to be consistent with the new A/C configuration.一旦航空公司报告了SB已在机队完成, 则IPC中将只有POST SB表述, 与飞机新构型一致.43SERVICE BULLETIN LIST SB清单INCORPORATION CODEThis is the SB configuration in the manual and can be S or C. S is used to indicate Split (Dual) Configuration and C is used to indicate Complete (Final) Configuration.手册中手册中SB构型构型, “S”表示双构型表示双构型PRE/POST, “C”表示最终构型表示最终构型“POST”44SERVICE BULLETIN INCORPORATION 服务通告编入手册DUAL EFFECTIVITY45DUAL EFFECTIVITY46SERVICE BULLETIN INCORPORATION 服务通告编入手册INCORPORATION CODECOMPLETE EFFECTIVITYC is used to indicate Complete (Final) Configuration.47COMPLETE EFFECTIVITY48IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单MATERIEL DOMAIN IPC FAMILIARIZATION49CURRENT STATUS:Integration of ALL Power Plant data for V2500 A1/A5on A320 A/C family as well as for RR Trent 500 on A340-500/600.For other LR A/C (CFM/GE/PW/RR) Integration into AIPC of PIPC Parts subject to an AMM removal procedure. Including all Engine build-up LRU目前状态目前状态:对于对于A320上的上的V2500 A1/A5 和和A340-500/600上的上的RR Trent 500, 所有发动机相关资料信息已所有发动机相关资料信息已编入飞机编入飞机IPC.对于其它对于其它A330/340系列飞机系列飞机(CFM/GE/PW/RR), 在在AMM拆装程序中涉及到的部件拆装程序中涉及到的部件, 其在发动机其在发动机IPC中的信息编入到飞机中的信息编入到飞机IPC中中. 包括所有组成发动机的航线可更换件包括所有组成发动机的航线可更换件(LRU).REMARKSProvisioning files are not affected.AIRBUS S/V file do not recommend any Power Plant Item.Power Plant Manufacturers keep providing operators with complete recommendation files.注注:定购文件不受影响定购文件不受影响. 空客的空客的S/V文件不推荐任何发动机项目文件不推荐任何发动机项目. 发动机厂商应提供完整的推荐文件发动机厂商应提供完整的推荐文件.PIPC INTEGRATION INTO AIPC PIPC 内容并入AIPCMATERIEL DOMAIN IPC FAMILIARIZATION50POWER PLANT DATA in IPC 发动机内容的有效性Power Plant IPC data are given in specific figures integrated in the Airbus IPCparts replacement is detailed in the Vendor Service Bulletin only.件号的互换性参见件号的互换性参见VSBStandard info Effectivity Engine Serial Number (ESN) 有效性按发动机序号有效性按发动机序号At aEngine model applicability适用的发动机型号适用的发动机型号Aircraft (FSN) applicability at the figure level整个图的有效性按飞机整个图的有效性按飞机FSN号号51IPC52IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单 AIRBUS PART NUMBERING SYSTEM空中客车件号系统 D 533 1 0230 000 00D : A319/A320/A321F : A330/A340 CHAP.SEC.章.节号 D.O. 设计单位SEQUENCE NBR.顺序号 ASSY NBR. 组件号Technical Suffix技术后缀0151. DRAWING REF. 图纸参考号图纸参考号A : A300/A31053IPC DETAILED PARTS LIST (DPL) 详详细件号清单细件号清单TECHNICAL SUFFIXES 技术后缀技术后缀 AIRBUS PART NUMBERING SYSTEM 空中客车件号系统空中客车件号系统 D 533 1 0230 000 0000 and 40 to 50 Spare Part identical to drawing. 备件与设计图纸相同备件与设计图纸相同01 to 39 Production Part not identical to Drawing. 生产用件与设计图纸不同生产用件与设计图纸不同51 to 59 Spare Part not identical to drawing, nor to production part. 备件与设计图纸不同备件与设计图纸不同,也与生产用件不同也与生产用件不同60 to 89 & 99 Non Procurable part. 不可购买件不可购买件.90 to 94 Specific Part for Repair kits. 专用于修理器材包的零件专用于修理器材包的零件.95 to 98 Specific Part for Service Bulletin Kits. 专用于服务通告器材包的零件专用于服务通告器材包的零件. 54AIRBUS PROPRIETARY PN SUFFIX* HANDLING IPC Three possible casesPart installed on AIRCRAFT Suffix “00”& ”40 to 50”1. PN: D521523200100 Suffix 00 by default for all non potential spares* or for other parts which can be delivered compliance with the drawing (no STS) OR Suffix “01 to 39”2. PN: D521523200101 Suffix 01 for Potential Spares Part different PN: D521 5232 001 from the drawing (WHITH OR WITHOUT Suffix) Detailed explanation will be provided by ANA/SSC with the Spare Part Technical Specification (STS delivered with the Part). OR Suffix “51 to 59”3. PN: D521523200151 Suffix 51 for Potential Spares Parts assembly different from the drawing. Content of the assembly detailed parts list will be provided by ANA/SSC with the related STS delivered with the PartNOTE: AIRBUS PROPRIETARY PART NUMBER SUFFIXES ARE PROVIDED BY AIRBUS MANUFACTURING Dept. * Non potential Spares part = Line replaceable part (e.g. part with high MTBUR) not recommended in AIRBUS provisioning document/file.However, should a “Non potential Spares part” be ordered by an operator, the delivered status of this particular part will be checked by AIRBUS manufacturing dept.Should the manufacturing dept. assign a PN suffix different from “00”, the IPC will be accordingly updated with the next possible revision. 55空客产权件后缀的处理 IPC 三种情况三种情况 飞机上安装的件号飞机上安装的件号 后缀后缀 “00”& ”40 至至 50”1. PN: D521523200100 对于对于“非可能性备件非可能性备件non potential spares* 或其或其 它可以按图纸提供的零件它可以按图纸提供的零件(不需要备用件技术规范不需要备用件技术规范 STS), 后缀默认为后缀默认为“00” 或者或者 后缀后缀“01 至至 39” 2. PN: D521523200101 后缀后缀 01 用于不同于图纸的可能备用件用于不同于图纸的可能备用件, 在备用件在备用件 技术规范技术规范(STS)中给出详细的解释中给出详细的解释, STS 与备件与备件 PN: D521 5232 001 一起发给用户一起发给用户 (WHITH OR WITHOUT Suffix) 或者或者 后缀后缀 “51 至至 59”3. PN: D521523200151 后缀后缀 51 用于不同于设计图纸的可能备用组件用于不同于设计图纸的可能备用组件, 组件中包括的详细件号目录标明在相关的在备用组件中包括的详细件号目录标明在相关的在备用 件技术规范件技术规范(STS)中与备件一起提供给用户中与备件一起提供给用户. 注注: AIRBUS 产权件号后缀由产权件号后缀由AIRBUS的零件生产部门提供的零件生产部门提供Non potential Spares part = “非可能性备件非可能性备件”指在空客推荐单中未包含的航线可更换件指在空客推荐单中未包含的航线可更换件(如如:某些高某些高MTBUR零件零件)然而然而, 如某用户订购了这种如某用户订购了这种“非可能性备件非可能性备件”, 此件的供货技术状态此件的供货技术状态(后缀后缀)将由将由AIRBUS的零件生产部门核准的零件生产部门核准. 如零件生产部门确定将如零件生产部门确定将提供的件号后缀不为提供的件号后缀不为“00”, 则则IPC在下一次更改版中将加入此件号在下一次更改版中将加入此件号 (带有或不带有后缀)56 Prefix Root PN Suffix Add Airbus domestic codes XXD21315432100 ZZZZZTo be disregardedTo be disregarded Can be replaced by: PN: D2131543210000 提供备用件技术规范提供备用件技术规范STSor PN: D2131543210001 with STS dataor PN: D2131543210051 with STS data or PN: D2131582210100 with PN change information(when INC 1 or 2) Important remarks : Applicable for not colored parts注意：适用于非彩色零件注意：适用于非彩色零件源件号源件号可被下列件号替换可被下列件号替换前缀前缀后缀后缀可忽略可忽略可忽略可忽略提供件号互换性信息提供件号互换性信息, 互换代码互换代码01或或02增加空客内部代码增加空客内部代码AIRBUS PART NUMBERING 空客公司件号系统57IPC58PN CHANGE 件号互换性WHY ?为什么为什么 TO INDICATE THE INTERCHANGEABILITY BETWEEN PARTS LOCATED IN DIFFERENT FIGURES OR APPLICABLE ON DIFFERENT A/C TYPES. TO PROPOSE ALTERNATIVE PARTS. TO EASE SPARES PLANNING & MAINTENANCE ACTIVITY.给出给出IPC 不同图示之间不同图示之间, 或不同机型之间零件的互换性或不同机型之间零件的互换性.建议可替换的零件建议可替换的零件.方便备件计划及维护工作方便备件计划及维护工作.59PN CHANGE 件号互换性HOW ?如何替换如何替换 BY ADDING IN THE IPC DETAILED PARTS LIST THE FOLLOWING INFORMATION : 在在IPC 详细件号清单中加入下述信息详细件号清单中加入下述信息:Two way I/W (Interchangeable With PN)双向互换双向互换One way RPLD BY (RePlaceD BY PN)单向互换单向互换 60IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单61IPC : Part Number Info IPC 中的件号信息Qualified Spares informationRPLD BY or I/W可用备件信息可用备件信息单向或双向互换单向或双向互换62Y I/W X (Interchangeable With) / The part Y can be replaced by the new PN X as spares or vice versa. This replacement is used without any change in the A/C configuration. When PN X is installed as spares, it can be replaced and PN Y re installed on the same A/C (MSN).件号Y可以被新件号X作为备件替换, 反之亦可.此替换不对飞机的构型产生任何改变. 新件号X安装后,它也可以被替换而将Y重新安装到同一架飞机上. Yx63 PN Y(8450B2) RPLD BY X (8450B3) (replaced by) The part number Y can be replaced by the new PN X as spares. This replacement is used without any change in the A/C configuration. When PN X is installed as spares, it can be replaced and PN Y re installed on the same A/C (MSN).件号Y可以被新件号X作为备件替换.此替换不对飞机的构型产生任何改变. 新件号X安装后,它也可以被替换而将Y重新安装到同一架飞机上. xY64 Y can be replaced by X with qualified condition given with the text . No other PN CHANGE (I/W;REPLD BY or other condition).件号Y可以在一定条件下被件号X替换.但不允许进一步替换.xY65No QUALIFIED SPARES with the MAINTENANCE FIGURE详图上不显示有效备件.66AIRNV-IPC ACCESS & CONTENTS 进入IPC及内容Direct access to the DATA 直接进入到手册内容By description/Table Of Content (TOC) 由内容目录进入By Functional Item Number (FIN) 由功能识别号进入By Part Number (PN) 由件号进入By Zone 按区域进入Service Bulletin 按服务通告进入Effectivity 按有效性Installation figure(CSN) 安装图Part Number CHANGE 可查找互换性Detail figure & IPC/AMM 详图及IPC/AMM链接切换67 AIRBUS CHINA LTD. All rights reserved. Confidential and proprietary document.This document and all information contained herein is the sole property of AIRBUS CHINA LTD. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS CHINA LTD. This document and its content shall not be used for any purpose other than that for which it is supplied.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.AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.68 A320 排故手册排故手册A320 Trouble Shooting ManualTechnical Data Support & Services69A319/A320/A321 TSM 排故手册?PFRLog Book70A319/A320/A321 TSM 排故手册71A319/A320/A321 - Post Flight Report - (PFR) 航后报告ECAM WarningECAM 警告信息警告信息CFDS failure messageCFDS 故障信息故障信息72A319/A320/A321 - Post Flight Report - (PFR) 航后报告参考时间GMT和ATA章节将ECAM 信息和CFDS故障信息联系起来故障信息ECAM警告信息(81)73Source Identifiers 故障信息源 故障识别者ADIRU1EISAFSECAMFADECCFDIUADMsensor19FP1INTEXTEXTEXTEXTPFR:SOURCEIDENTIFIERSADIRU1 : NO ADM 19FP1 DATA ADIRU1 EIS, AFS, ECAM FADECNOTE: Users of ADIRU data send fault messages to CFDIU coded as external: e.g. EIS1: NO ADIRU1 DATA注注: ADIRU 数据信息的用户会向数据信息的用户会向CFDIU 发出故障信息发出故障信息, 为外部信息为外部信息.AIR DATA INERTIAL REF. UNITELECTRONIC INST. STEMAUTOMATIC FLIGHT SYSTEMElect. Centralized Aircraft MonitoringFull Authority Digital Engine Control74故障等级 (A319/A320/A321)123Failure / Fault Classes故障故障/故障等级故障等级对本航段的飞行操作是否有影对本航段的飞行操作是否有影响响是是否否否否是是是是否否对机组是否有指示信息对机组是否有指示信息自动显示自动显示- 在在ECAM显示警告显示警告/警戒警戒 信息信息 - 在驾驶舱中显示警告旗在驾驶舱中显示警告旗 和其它警告和其它警告在在 ECAM STATUS PAGE状态页上状态页上, 但但只在航段只在航段10 & 01对放行影响对放行影响 参考参考 MMEL 可能是可能是 “GO” 无条件放行无条件放行“GO IF” 有条件放行有条件放行“NO GO” 不能放行不能放行勿需参考勿需参考 MMEL无条件放行无条件放行10天天 MMEL 不适用不适用(不影响放行不影响放行)对维护人员是否有对维护人员是否有指示指示是是每个航段之后打印每个航段之后打印 CFDS PFR是是通过通过CFDS SystemReport/Test查寻查寻PFR75CFDS排故原则 维护等级AI/SE-D4- APR 96航站维护航站维护 飞行记录本中无报告则无需做维护工作 记录本中如报告 (一级故障)查阅 PFR + System report/test LRU level only + 参考 MMEL放行本站维护本站维护/航后航后 维护状态信息 PFR 中二级故障信息 LRU level + System report/test定检定检 三级故障一般三级故障报告 LRU level + System report/test LRU level车间部件维护车间部件维护 排故数据TSD + BITE 存储数据 LRU 拆下Trouble shooting data LRU level+ BITE shop memory76TSM Procedure - Fault Isolation TSM 故障隔离程序 PB 201-List of Possible Causes 列出可能的故障原因列出可能的故障原因- Job set-up 工作准备信息工作准备信息-Fault confirmation 故障确认故障确认-Fault isolation 故障隔离程序故障隔离程序 任务号任务号/标题标题-Task N/Title77TSM Task Supporting Data TSM 排故辅助数据- PB301- Block Diagram- Schematics- Logic- Supporting data-方块图方块图-简图简图-逻辑图逻辑图-辅助数据辅助数据78TSM & Associated Documentation TSM 及相关手册PFRPostFlightReportTEMTool & Equipment ManualMMELCDLConfiguration DeviationList (m)TSM Trouble ShootingManualCLMComponentLocationManualMMELPart 3SimplifiedDeactivationProceduresTask NumberATA Ref. LOGBOOKAMM AircraftMaintenanceManualWARNING/MALFUNCTIONMAINTENANCE/CREW OBSERVATIONDeactivationSystemTESTTOOL PNASMAircraftSchematicsManualAWMAircraftWiringManual20-42/0220-42-06MMEL/CDLReferenceMCDU79A319/A320/A321- Post Flight Report PFR 航后报告 A/C ID DATE GMT FLTN CITY PAIRH8-10A 01SEP 0728/1211 SR625 LIML LSZHECAM WARNING MESSAGESGMT PH ATAO74406 34-00 NAV ILS 2 FAULTFAILURE MESSAGESGMT PH ATA SOURCE IDENTIFIERS0744 06 34-36-31 FWC1 NO MMR2 DATA ECAM 1 EIS1 1128 06 28-46-17 FUEL LEVEL SENSING FUEL R INN TEMP SENSOR 29QJ2MAINTENANCEPOST FLIGHT REPORT80This document and all information contained herein is the sole property of AIRBUS S.A.S. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.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 S.A.S. will be pleased to explain the basis thereof.AN EADS JOINT COMPANYWITH BAE SYSTEMS81