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空客飞机AMM,IPC,TSM手册使用.ppt

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1、AMM 及相关手册 AMM & Associated Products,Technical Data Support & Services,Presented byName JobTitle,AMM General 飞机维护手册 概述,AMM 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AMM 而在 CMM 中.,The AMM provides detailed information required to maintain th

2、e 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,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:,28 - 21 - 51,Component (unit) level, breakdown allocated by Manufacturer部件, 由飞机

3、制造商划分,Sub-sub-system level, breakdown allocated by Manufacturer 次级分系统, 由飞机制造商划分,Sub-system level, breakdown allocated by ATA 100 Spec. 分系统 按 ATA 100 规范划分,Chapter level, breakdown allocated by ATA 100 Spec. 章 按 ATA 100 规范划分,AMM Breakdown 内容划分,Deactivation/Reactivation index - MMEL/CDL (失效/恢复使用程序 - MM

4、EL/CDL),SB list (SB 清单),Description and Operation 系统描述&工作,Maintenance Procedures 维护程序,At each chapter level you will find 在各章节包括,TOC ( + Highlights on PDF) 手册内容目录 ( +更改内容重点PDF 手册),D&O,MP,Highlights (only AirNv) 更改重点 (只在AirNv 中),Manual Front Matter page (手册首页),Chapter 00 Introduction (章节00 - 手册介绍),Fl

5、eet No. / MSN cross ref table (FSN / MSN 交叉索引表),COC list (COC 清单),AMM,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,Keyword Page Block (PB) 关键字 页段 (PB)之间的关系,Table of Contents (TOC),Description & Operation (PB 001) 系统描述&工作 (PB 001),The purpose of th

6、e 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 & indicatingthe 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 - BI

7、TE 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.,R/I,Cross ref. to Removal/installation,D&O - Component location 部件位置,Click to see The figure,EFFECTIVITY 有效性,On A/C 007-099, PRE SB 53-4098; 对于007-099飞机, 未执行服务通告SB 53-4098,On A/C 007-099, POST SB

8、 53-4098; 对于007-099飞机, 已执行服务通告SB 53-4098,Removal / Installation 拆卸/安装,程序的结构组成,Task 29-16-51-000-001任务标题包含功能识别号FIN (如适用) 警告/警戒 (如适用) 1 执行本工作的原因- 给出本工作的原因- 或参见 MMEL 任务- 或参见 CDL任务.- 或参见MPD任务 2 工作准备信息部分可提供:- 工具信息:处理 - 专用工具- 通用工具- 消耗材料- IPC/PIPC中消耗零件的章节号- 参考其它AMM 任务, CMM, TSM 等.- 参考图解 3 -工作准备部分可提供:- 安全需知

9、- 特定的飞机状态.- 接近方式 4 程序- 包括简单测试 5 完成- 飞机恢复到原来状态.,Tools/Equipment & Associated Documentation工具/设备及相关文件,AMMAircraft Maintenance Manual,TSMTrouble Shooting Manual,CMM Component Maintenance Manual部件翻修手册,OVERHAUL部件翻修,TEITool & Equipment Index,TEM Tool & Equipment Manual,TED Tool/Equipment Drawing,TEBToolEq

10、uipmentBulletin,TOOL PN 工具件号,SES Support Equipment Summary,Tool Drawing Status工具图纸状态 Y TEI 参见TEI P Contact Vendor 与厂家联系 C Refer to CMM 参考 CMM S Standard tool 标准工具 etc,MAINTENANCE 飞机维护,TEM TEI SES,AMM and associated manuals AMM 及相关手册, AIRBUS CHINA LTD. All rights reserved. Confidential and proprietar

11、y 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 expr

12、ess 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

13、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.,零备件资料介绍 SPARE DATA FAMILIARIZATION,Technical Data Support & Services,Presented by

14、Name JobTitle,Generalities 概述,LINE MAINTENANCE 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= 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 (

15、发动机IPC),Generalities 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(可修理&可消耗)的件号以用于航线维护及 制定备件计划.例如:AIRBUS STRUCTURAL PARTS (空客结构件)VENDOR COMPONENTS (厂家部件)COMPONENT BREAKDOWN PARTS (部件分解件)ATTACHING / INSTALLATION PARTS

16、(连接/安装件),USED FOR LINE MAINTENANCE&SPARES PLANNING PURPOSES,IPC,DETAILED PART LIST,(DPL),详细件号清单,ILLUSTRATION Installation figure 安装图图解,ILLUSTRATION detailed figure 详图图解,DETAILED PART LIST 详细零件清单,INSTALLATION FIG,MATERIEL DOMAIN IPC FAMILIARIZATION,INSTALLATION BREAKOUT 安装图的划分,To aid in rapid locatio

17、n 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:,DETAILED PART LIST,GENERAL SYSTEM,MATERIEL DOMAIN IPC FAMILIARIZATION,ASSEMBLY ORDER,GENERAL SYSTEM OF ASSEMBLY ORDER,The indenture system used in DPL shows the r

18、elationship 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:,AirNv DETAILED PARTS LIST (DPL) 详细件号清单,AirNv DETAILED PARTS LIST (DPL) 详细件号清单,AirNv DETAILED PARTS LIST (DPL) 详细件号清单,Buyer Furnished Equipment (BFE) Identifies a part, which is furni

19、shed by the customer to AIRBUS to be installed in the A/CBFE项是由客户提供给空客安装到飞机上的,买方提供设备 - BFE,BFE 是用户自己提供并安装到飞机上设备。 (例如: 厨房, 麦克风, 救生衣, 娱乐设备等).只有当从用户接收到有关BFE的技术信息后(如相关的CMM, 图纸等),BFE 设备才会被收录到手册中。(SFE: 即Supplier Furnished Equipment) SFE: 卖方提供的设备,NON PROCURABLE ITEM (NP)不可购买件,Appearing in the nomenclature

20、column “NP” indicates that this item is not procurable (SPC =0). 在名称栏里NP表示此件号不能用于订购,OPTIONAL PARTNUMBER (OPT TO) 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,IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单,STORAGE PA

21、RTS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, 则同时需要“Storage parts”和 “*”之间所列的零件, 所标数量用于储存一个上一级组件.,ALTERNATE PART NUMBER (ALT FROM) 替换件号,“ALT FROM” xxxxxxxx identifies a part, which i

22、s functionallyinterchangeable with the basic one shown in the part number column only after rework. 表明此件在经过重新加工后, 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,PREFERRED SPARE PART (BUY PN) 首选件号,“BUY PN” xxxxxxx identifies an item which is recommended as the current preferred part for

23、 spares purposes. “BUY PN” 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/右侧指示,A/ Parts used on left hand or right hand of symmetrical installations aredesigned by “LH” or “RH”. 在对称的安装中, 左侧和右侧件分别用“LH” 和 “RH”表示. B/ Parts , assemblies or installations used only on one side of the aircraft are d

24、esignated by “(LH SIDE)” or “(RH SIDE)”.零件, 装配件或组装件如只在飞机的一侧使用, 则用“(LH SIDE)”或“(RH SIDE)”表示.,IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单,LOCAL MANUFACTURE (LM) 当地加工件,“*LM*” identifies a part which can be locally manufactured. “*LM*” 表示此件可当地加工. LM parts are listed in the IPC Additional Cross Reference Ta

25、ble as follows : LM 件在ACRT 手册中列有如下信息:- Raw material to finished PN 原材料 - 成品件号索引- Finished PN to raw material 成品件号 - 原材料索引,IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单,RESTRICTED USAGE (RU)限制用于,Exp. RU 010, means only used on item 010. 例如 RU 010, 表示只用于010项件号上 Refer to effectivity of item 010. 参考010项的有效性,

26、DETAILED PART LIST 详细零件清单,EFFECTIVITY,MATERIEL DOMAIN IPC FAMILIARIZATION,ONLY AIRCRAFT IDENTIFIED IN THE EFFECTIVITY TABLE ARE COVERED IN THE IPC 有效性表格列出IPC涵盖的所有飞机号,The absence of a restrictive effectivity at all itemsin one IPC figure indicates that the part is effective for all aircraft of a cust

27、omers fleet. IPC图中如无有效性限制,则表明适用于机队的所有飞机,The effectivity shown is called “SPARES Effectivity”. The Spares effectivity is given in accordance with the interchangeability code between the partsand 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.,RU 001B (RU= Restricted usage, 001B= Item 0

28、01B) means “only used on the assembly defined with item 001B” “限制使用”表示只用于001B项件号上,DETAILED PART LIST 详细零件清单,SERVICE BULLETIN,MATERIEL DOMAIN IPC FAMILIARIZATION,SERVICE 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

29、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 t

30、he 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.,SERVICE BULLETIN LIST SB清单,INCORPORATION CODE,This 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

31、SB构型, “S”表示双构型PRE/POST, “C”表示最终构型“POST”,SERVICE BULLETIN INCORPORATION 服务通告编入手册,DUAL EFFECTIVITY,DUAL EFFECTIVITY,SERVICE BULLETIN INCORPORATION 服务通告编入手册,INCORPORATION CODE,COMPLETE EFFECTIVITY,“C“ is used to indicate Complete (Final) Configuration.,COMPLETE EFFECTIVITY,IPC DETAILED PARTS LIST (DPL)

32、 IPC 详细件号清单,Power Plant Data,MATERIEL DOMAIN IPC FAMILIARIZATION,CURRENT 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.

33、Including all Engine build-up LRU目前状态:对于A320上的V2500 A1/A5 和A340-500/600上的RR Trent 500, 所有发动机相关资料信息已编入飞机IPC. 对于其它A330/340系列飞机(CFM/GE/PW/RR), 在AMM拆装程序中涉及到的部件, 其在发动机IPC中的信息编入到飞机IPC中. 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.

34、 Power Plant Manufacturers keep providing operators with complete recommendation files.注:定购文件不受影响. 空客的S/V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.,PIPC INTEGRATION INTO AIPC PIPC 内容并入AIPC,MATERIEL DOMAIN IPC FAMILIARIZATION,POWER PLANT DATA in IPC 发动机内容的有效性,Power Plant IPC data are given in specific figures in

35、tegrated in the Airbus IPC,IPC,AIRBUS PART NUMBERING,空中客车件号系统,IPC 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 00,D : A319/A320/A321 F : 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 01 51,DRAWING REF.图纸参考号,A : A3

36、00/A310,IPC DETAILED PARTS LIST (DPL) 详细件号清单,TECHNICAL SUFFIXES 技术后缀,AIRBUS PART NUMBERING SYSTEM空中客车件号系统D 533 1 0230 000 00,00 and 40 to 50 Spare Part identical to drawing. 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 51 to 59 Spare Part not identical to drawing, nor to

37、production part.备件与设计图纸不同,也与生产用件不同60 to 89 & 99 Non Procurable part. 不可购买件. 90 to 94 Specific Part for Repair kits. 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.,AIRBUS PROPRIETARY PN SUFFIX* HANDLING,IPCThree possible casesPart installed on AIRCRAFT Suffix “00”& ”40

38、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) ORSuffix “01 to 39” 2. PN: D521523200101 Suffix 01 for Potential Spares Part differentPN: D521 5232 001 from the drawing (WHITH OR WITHOUT Suf

39、fix) Detailed explanation will be provided by ANA/SSC with the Spare Part Technical Specification (STS delivered with the Part).ORSuffix “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 provide

40、d 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 “N

41、on 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.,空客产权件后缀的处理,IPC三种

42、情况飞机上安装的件号 后缀 “00”& ”40 至 50” 1. PN: D521523200100 对于“非可能性备件non potential spares* 或其 它可以按图纸提供的零件(不需要备用件技术规范 STS), 后缀默认为“00”或者后缀“01 至 39” 2. PN: D521523200101 后缀 01 用于不同于图纸的可能备用件, 在备用件 技术规范(STS)中给出详细的解释, STS 与备件PN: D521 5232 001 一起发给用户(WHITH OR WITHOUT Suffix) 或者后缀 “51 至 59”3. PN: D521523200151 后缀 51

43、 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 件技术规范(STS)中与备件一起提供给用户. 注: AIRBUS 产权件号后缀由AIRBUS的零件生产部门提供 Non potential Spares part = “非可能性备件”指在空客推荐单中未包含的航线可更换件(如:某些高MTBUR零件) 然而, 如某用户订购了这种“非可能性备件”, 此件的供货技术状态(后缀)将由AIRBUS的零件生产部门核准. 如零件生产部门确定将提供的件号后缀不为“00”, 则IPC在下一次更改版中将加入此件号,(带有或不带有后缀),Prefix Root PN Suffix Add

44、 Airbus domestic codesXX D21315432100 ZZZZZ,To be disregarded,To be disregarded,Can be replaced by:PN: D2131543210000 提供备用件技术规范STSor PN: D2131543210001 with STS dataor PN: D2131543210051 with STS dataor PN: D2131582210100 with PN change information(when INC 1 or 2),Important remarks : Applicable for

45、 not colored parts 注意:适用于非彩色零件,源件号,可被下列件号替换,前缀,后缀,可忽略,可忽略,提供件号互换性信息, 互换代码01或02,增加空客内部代码,AIRBUS PART NUMBERING 空客公司件号系统,IPC,PART NUMBER CHANGE DATA 件号互换性信息,PN CHANGE 件号互换性,WHY ? 为什么,TO INDICATE THE INTERCHANGEABILITY BETWEEN PARTSLOCATED IN DIFFERENT FIGURES OR APPLICABLE ON DIFFERENT A/C TYPES.TO PR

46、OPOSE ALTERNATIVE PARTS.TO EASE SPARES PLANNING & MAINTENANCE ACTIVITY.给出IPC 不同图示之间, 或不同机型之间零件的互换性. 建议可替换的零件. 方便备件计划及维护工作.,PN CHANGE 件号互换性,HOW ? 如何替换,BY ADDING IN THE IPC DETAILED PARTS LISTTHE FOLLOWING INFORMATION :在IPC 详细件号清单中加入下述信息:,Two way I/W (Interchangeable With PN) 双向互换One way RPLD BY (RePl

47、aceD BY PN) 单向互换,IPC DETAILED PARTS LIST (DPL) IPC 详细件号清单,IPC : Part Number Info IPC 中的件号信息,Qualified Spares information RPLD BY or I/W 可用备件信息 单向或双向互换,“Y 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

48、 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.,Y,x,x,Y,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.,x,Y,No QUALIFIED SPARES with the MAINTENANCE FIGURE 详图上不显示有效备件.,

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