1、會(huì)計(jì)學(xué)1空客飛機(jī)空客飛機(jī)AMMIPCTSM手冊使用手冊使用AMM General 飛機(jī)維護(hù)手冊 概述WHEN YOU WORK ON AIRCRAFT USE THE AMM 當(dāng)在飛機(jī)上工作時(shí)使用當(dāng)在飛機(jī)上工作時(shí)使用 AMM FMCDLNON-SCHEDULED MAINTENANCE PROCEDURES非例行維護(hù)程序非例行維護(hù)程序MELTSMSCHEDULED MAINTENANCE PROCEDURES例行維護(hù)程序例行維護(hù)程序MPD MRB AMMThis does not include workshop information which is contained in the CM

2、M.車間附件修理的技術(shù)信息不在車間附件修理的技術(shù)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 維護(hù)手冊提供航線和定檢維護(hù)時(shí)所需的詳細(xì)技術(shù)信息維護(hù)手冊提供航線和定檢維護(hù)時(shí)所需的詳細(xì)技術(shù)信息The AMM is structured into ATA chapters and further into sub-systems and units as required. AMM維護(hù)手冊按需要?jiǎng)澐殖删S護(hù)手冊按

3、需要?jiǎng)澐殖葾TA章節(jié)章節(jié), 分系統(tǒng)和主題分系統(tǒng)和主題(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, 由飛機(jī)制造商劃分由飛機(jī)制造商劃分Sub-sub-system level, breakdown allocated by Manufacturer次級(jí)分系統(tǒng)次級(jí)分系統(tǒng), 由飛機(jī)制造商劃分由飛機(jī)制造商劃分Sub-system level, breakdown allocated by ATA 100 Spec.

4、分系統(tǒng)分系統(tǒng) 按按 ATA 100 規(guī)范劃分規(guī)范劃分Chapter level, breakdown allocated by ATA 100 Spec.章章 按按 ATA 100 規(guī)范劃分規(guī)范劃分 Deactivation/Reactivation index - MMEL/CDL(失效失效/恢復(fù)使用程序恢復(fù)使用程序 TEI 參見參見TEIP - Contact Vendor 與廠家聯(lián)系與廠家聯(lián)系C - Refer to CMM 參考參考 CMM S - Standard tool 標(biāo)準(zhǔn)工具標(biāo)準(zhǔn)工具etcMAINTENANCE飛機(jī)維護(hù)飛機(jī)維護(hù)TEMTEISESTLMC TimeLimitsM

5、PD 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 Manua

6、lATA Ref.CLMComponentLocationManualATA Ref.CMMComponent Maintenance ManualATA Ref.SJCStandard JobCardsCCCGICJICExtractMMELCDLConfiguration DeviationListMMEL/CDL Ref.ATA Ref. (m)ATA Ref. FINAWM Task numberATA Ref.TSM AIRBUS CHINA LTD. All rights reserved. Confidential and proprietary document.This do

7、cument 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

8、 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 st

9、atements 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.Technical Data Support & ServicesPresented byNameJobTitleGeneralities 概述 LINE MAINTENANCE 航線維護(hù)航線維護(hù)= AIP

10、C /PIPCAIPC = AIRFRAME ILLUSTRATED PARTS CATALOG 飛機(jī)圖解零件清冊PIPC = POWER PLANT ILLUSTRATED PARTS CATALOG發(fā)動(dòng)機(jī)圖解零件清冊 SHOP MAINTENANCE 車間維護(hù)車間維護(hù)= CMM / ACMM / EIPCCMM = COMPONENT MAINTENANCE MANUAL 部件維護(hù)手冊ACMM = ABBREVIATED CMM 簡化部件維護(hù)手冊EIPC = ENGINE IPC (發(fā)動(dòng)機(jī)IPC)Generalities 概述THE ILLUSTRATED PARTS CATALOG (I

11、PC) IDENTIFIES:ALL LINE REPLACEABLE PARTS (REPAIRABLE & EXPENDABLE) such as : IPC 用于確認(rèn)所有航線可更換件用于確認(rèn)所有航線可更換件(可修理可修理&可消耗可消耗)的件號(hào)以用于航線維護(hù)及的件號(hào)以用于航線維護(hù)及 制定備件計(jì)劃制定備件計(jì)劃.例如例如: AIRBUS STRUCTURAL PARTS (空客結(jié)構(gòu)件空客結(jié)構(gòu)件) VENDOR COMPONENTS (廠家部件廠家部件) COMPONENT BREAKDOWN PARTS (部件分解件部件分解件) ATTACHING / INSTALLATION PARTS (

12、連接連接/安裝件安裝件)USED FOR LINE MAINTENANCE & SPARES PLANNING PURPOSES IPCGENERALZONING大致的區(qū)域大致的區(qū)域FRAME INFO隔框區(qū)間隔框區(qū)間DOTTED LINE CROSS REFDIFFERENT 6 digits 點(diǎn)劃線索引到點(diǎn)劃線索引到另一不同章節(jié)另一不同章節(jié)FIN NUMBER功能識(shí)別號(hào)功能識(shí)別號(hào)DETAILZONING詳細(xì)區(qū)域詳細(xì)區(qū)域ITEM NUMBER項(xiàng)次號(hào)項(xiàng)次號(hào)CROSS REF AMM鏈接到鏈接到AMMLine Maintenance Parts航線維護(hù)件航線維護(hù)件MATERIEL DOMAIN

13、IPC FAMILIARIZATIONTo aid in rapid location of an illustration, the subject part of the CSN (digit 5 and 6) has been assigned as follows:為盡快確認(rèn)安裝圖的位置, 章節(jié)號(hào)CSN的“主題”部分, 即第五,六位按如下劃分:CHAPTER-SYSTEMCIRCUIT-SUBJECTSUBJECTXXXX01 to 09XXXX10 to 90MATERIEL DOMAIN IPC FAMILIARIZATIONThe indenture system used in

14、 DPL shows the relationship of parts and assemblies to next higher assemblies in assembly order as follows:詳細(xì)零件清單中的縮格關(guān)系表示上下級(jí)組件之間的關(guān)系詳細(xì)零件清單中的縮格關(guān)系表示上下級(jí)組件之間的關(guān)系:1 2 3 4 5 6 7INSTALLATION. DETAILED PARTS FOR INSTALLATION. ASSEMBLY. ATTACHING PARTS FOR ASSEMBLY. . DETAILED PARTS FOR ASSEMBLY. . SUB-ASSEMBL

15、Y. . ATTACHING PARTS FOR SUB-ASSEMBLY. . . DETAILED PARTS FOR SUB-ASSEMBLY. . . SUB-SUB-ASSEMBLY. . . ATTACHING PARTS FOR SUB-SUB-ASSEMBLYFIGURENUMBER圖號(hào)圖號(hào)NOTILLUSTRATEDITEM無圖解項(xiàng)無圖解項(xiàng)PARTNUMBER件號(hào)件號(hào)ITEMNUMBER項(xiàng)次號(hào)項(xiàng)次號(hào)EFFECTIVITY有效性有效性REFERENCEITEM參考項(xiàng)參考項(xiàng)X-REFTODET鏈接到詳圖鏈接到詳圖QUANTITYPER CSN每個(gè)組件數(shù)量每個(gè)組件數(shù)量DATA RE

16、VISED YELLOW COLOR黃色為更改處黃色為更改處CMM REFCMM 章節(jié)號(hào)章節(jié)號(hào)VENDORCODE廠家代碼廠家代碼NOTPROCURABLEITEM不可購買件不可購買件FIN REF功能識(shí)別號(hào)功能識(shí)別號(hào)OPTIONALPN/VENDOR互換件號(hào)及廠家代碼互換件號(hào)及廠家代碼LOCAL MANUFACTURE可當(dāng)?shù)丶庸ぜ僧?dāng)?shù)丶庸ぜ﨎UY PN首選件首選件Buyer Furnished Equipment (BFE) Identifies a part, which is furnished by the customer to AIRBUS to be installed in

17、the A/C BFE項(xiàng)是由客戶提供給空客安裝到飛機(jī)上的BFE 是用戶自己提供并安裝到飛機(jī)上設(shè)備。是用戶自己提供并安裝到飛機(jī)上設(shè)備。 (例如例如: 廚房廚房, 麥麥克風(fēng)克風(fēng), 救生衣救生衣, 娛樂設(shè)備等娛樂設(shè)備等).只有當(dāng)從用戶接收到有關(guān)只有當(dāng)從用戶接收到有關(guān)BFE的技術(shù)信息后的技術(shù)信息后(如相關(guān)的如相關(guān)的CMM, 圖紙等圖紙等)，BFE 設(shè)備才會(huì)被收錄到手冊中。設(shè)備才會(huì)被收錄到手冊中。(SFE: 即即Supplier Furnished Equipment)SFE: 賣方提供的設(shè)備賣方提供的設(shè)備 NON PROCURABLE ITEM (NP)不可購買件不可購買件Appearing in t

18、he nomenclature column “NP” indicates that this item is not procurable (SPC =0). 在名稱欄里在名稱欄里NP表示此件號(hào)不能用于訂購表示此件號(hào)不能用于訂購 OPTIONAL PARTNUMBER (OPT TO)代用件號(hào)代用件號(hào)“OPT TO” xxxxxxxxx identifies a part fully interchangeable with the basic one shown in the part number column.表明此件與件號(hào)欄里的基本件號(hào)可完全互換表明此件與件號(hào)欄里的基本件號(hào)可完全互換

19、IPC DETAILED PARTS LIST (DPL) IPC 詳細(xì)件號(hào)清單 STORAGE PARTS 儲(chǔ)存件儲(chǔ)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. 若儲(chǔ)存上一級(jí)組件若儲(chǔ)存上一級(jí)組件, 則同時(shí)需要?jiǎng)t同時(shí)需要“Storage parts”和和 “*”之間所之間所列的零件列的零件, 所標(biāo)數(shù)量用于儲(chǔ)存一個(gè)上一級(jí)組件所標(biāo)數(shù)量用于儲(chǔ)存一個(gè)上

20、一級(jí)組件. ALTERNATE PART NUMBER (ALT FROM)替換件號(hào)替換件號(hào)“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經(jīng)過重新加工經(jīng)過重新加工后后, 與件號(hào)欄中的基本件號(hào)在功能上可以互換與件號(hào)欄中的基本件號(hào)在功能上可以互換.IPC DETAILED PARTS LIST (DPL) IPC 詳細(xì)件號(hào)清單 PREFE

21、RRED SPARE PART (BUY PN)首選件號(hào)首選件號(hào)“BUY PN” xxxxxxx identifies an item which is recommended as the current preferred part for spares purposes. “BUY PN” 表明此件號(hào)被推薦為目前備件的首選件號(hào)表明此件號(hào)被推薦為目前備件的首選件號(hào) LEFT HAND/RIGHT HAND INDICATORS左側(cè)左側(cè)/右側(cè)指示右側(cè)指示A/ Parts used on left hand or right hand of symmetrical installations

22、are designed by “LH” or “RH”. 在對(duì)稱的安裝中在對(duì)稱的安裝中, 左側(cè)和右側(cè)件分別用左側(cè)和右側(cè)件分別用“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, 裝配件或組裝件如只在飛機(jī)的一側(cè)使用裝配件或組裝件如只在飛機(jī)的一側(cè)使用, 則用則用“(LH SIDE)”或或 “(RH SIDE)”表示表示.IPC DETAILED PARTS

23、LIST (DPL) IPC 詳細(xì)件號(hào)清單 LOCAL MANUFACTURE (LM)當(dāng)?shù)丶庸ぜ?dāng)?shù)丶庸ぜ?LM*” identifies a part which can be locally manufactured.“*LM*” 表示此件可當(dāng)?shù)丶庸け硎敬思僧?dāng)?shù)丶庸?LM parts are listed in the IPC Additional Cross Reference Table as follows : LM 件在件在ACRT 手冊中列有如下信息手冊中列有如下信息:- Raw material to finished PN 原材料原材料 - 成品件號(hào)索引成品件號(hào)索引-

24、Finished PN to raw material 成品件號(hào)成品件號(hào) - 原材料索引原材料索引IPC DETAILED PARTS LIST (DPL) IPC 詳細(xì)件號(hào)清單 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項(xiàng)件號(hào)上項(xiàng)件號(hào)上Refer to effectivity of item 010. 參考參考010項(xiàng)的有效性項(xiàng)的有效性MATERIEL DOMAIN IPC FAMILIARIZATIONONLY AIRCRAFT IDENT

25、IFIED IN THE EFFECTIVITY TABLE ARE COVERED IN THE IPC 有效性表格列出有效性表格列出IPC涵蓋的所有飛機(jī)號(hào)涵蓋的所有飛機(jī)號(hào)The 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圖中如無有效性限制,則表明適用于機(jī)隊(duì)的所有飛機(jī)The effectivity shown is called “SPARES

26、Effectivity”. The Spares effectivity is given in accordance with the interchangeability code between the parts and the A/C configuration.有效性也稱備件有效性, 它是依據(jù)飛機(jī)的構(gòu)型以及件號(hào)之間的互換性代碼共同確定的.RU 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

27、001B項(xiàng)件號(hào)上項(xiàng)件號(hào)上MATERIEL DOMAIN IPC FAMILIARIZATIONThe integration of the PRE/POST Airbus SB in the IPC is in accordance with the policy between AIRBUS and AIRLINES.空客服務(wù)通告編入IPC依據(jù)空客與航空公司之間協(xié)議的政策.The reference of the PRE or POST Airbus SB is in the IPC to help users about the redundant effectivity.IPC中PRE和

28、POST SB的表述, 為用戶提供了兩種可能的有效性.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.一旦航空公司報(bào)告了SB已在機(jī)隊(duì)完成, 則IPC中將只有POST SB表述, 與飛機(jī)新構(gòu)型一致.INCORPORATION CODEThis is the SB configuration in the manual and can be S or C.

29、S is used to indicate Split (Dual) Configuration and C is used to indicate Complete (Final) Configuration.手冊中手冊中SB構(gòu)型構(gòu)型, “S”表示雙構(gòu)型表示雙構(gòu)型PRE/POST, “C”表示最終構(gòu)型表示最終構(gòu)型“POST”DUAL EFFECTIVITYDUAL EFFECTIVITYINCORPORATION CODECOMPLETE EFFECTIVITYC is used to indicate Complete (Final) Configuration.COMPLETE EFFE

30、CTIVITYMATERIEL DOMAIN IPC FAMILIARIZATIONCURRENT 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 bui

31、ld-up LRU目前狀態(tài)目前狀態(tài):對(duì)于對(duì)于A320上的上的V2500 A1/A5 和和A340-500/600上的上的RR Trent 500, 所有發(fā)動(dòng)機(jī)相關(guān)資料信息已所有發(fā)動(dòng)機(jī)相關(guān)資料信息已編入飛機(jī)編入飛機(jī)IPC.對(duì)于其它對(duì)于其它A330/340系列飛機(jī)系列飛機(jī)(CFM/GE/PW/RR), 在在AMM拆裝程序中涉及到的部件拆裝程序中涉及到的部件, 其在發(fā)動(dòng)機(jī)其在發(fā)動(dòng)機(jī)IPC中的信息編入到飛機(jī)中的信息編入到飛機(jī)IPC中中. 包括所有組成發(fā)動(dòng)機(jī)的航線可更換件包括所有組成發(fā)動(dòng)機(jī)的航線可更換件(LRU).REMARKSProvisioning files are not affected.AI

32、RBUS S/V file do not recommend any Power Plant Item.Power Plant Manufacturers keep providing operators with complete recommendation files.注注:定購文件不受影響定購文件不受影響. 空客的空客的S/V文件不推薦任何發(fā)動(dòng)機(jī)項(xiàng)目文件不推薦任何發(fā)動(dòng)機(jī)項(xiàng)目. 發(fā)動(dòng)機(jī)廠商應(yīng)提供完整的推薦文件發(fā)動(dòng)機(jī)廠商應(yīng)提供完整的推薦文件.PIPC INTEGRATION INTO AIPC PIPC 內(nèi)容并入AIPCMATERIEL DOMAIN IPC FAMILIARIZATION

33、parts replacement is detailed in the Vendor Service Bulletin only.件號(hào)的互換性參見件號(hào)的互換性參見VSBStandard info Effectivity Engine Serial Number (ESN) 有效性按發(fā)動(dòng)機(jī)序號(hào)有效性按發(fā)動(dòng)機(jī)序號(hào)At aEngine model applicability適用的發(fā)動(dòng)機(jī)型號(hào)適用的發(fā)動(dòng)機(jī)型號(hào)Aircraft (FSN) applicability at the figure level整個(gè)圖的有效性按飛機(jī)整個(gè)圖的有效性按飛機(jī)FSN號(hào)號(hào) AIRBUS PART NUMBERING SY

34、STEM空中客車件號(hào)系統(tǒng) D 533 1 0230 000 00D : A319/A320/A321F : A330/A340 CHAP.SEC.章.節(jié)號(hào) D.O. 設(shè)計(jì)單位SEQUENCE NBR.順序號(hào) ASSY NBR. 組件號(hào)Technical Suffix技術(shù)后綴0151. DRAWING REF. 圖紙參考號(hào)圖紙參考號(hào)A : A300/A310TECHNICAL SUFFIXES 技術(shù)后綴技術(shù)后綴 AIRBUS PART NUMBERING SYSTEM 空中客車件號(hào)系統(tǒng)空中客車件號(hào)系統(tǒng) D 533 1 0230 000 0000 and 40 to 50 Spare Part i

35、dentical to drawing. 備件與設(shè)計(jì)圖紙相同備件與設(shè)計(jì)圖紙相同01 to 39 Production Part not identical to Drawing. 生產(chǎn)用件與設(shè)計(jì)圖紙不同生產(chǎn)用件與設(shè)計(jì)圖紙不同51 to 59 Spare Part not identical to drawing, nor to production part. 備件與設(shè)計(jì)圖紙不同備件與設(shè)計(jì)圖紙不同,也與生產(chǎn)用件不同也與生產(chǎn)用件不同60 to 89 & 99 Non Procurable part. 不可購買件不可購買件.90 to 94 Specific Part for Repair kit

36、s. 專用于修理器材包的零件專用于修理器材包的零件.95 to 98 Specific Part for Service Bulletin Kits. 專用于服務(wù)通告器材包的零件專用于服務(wù)通告器材包的零件. 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 complian

37、ce 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).

38、 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

39、 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 ma

40、nufacturing dept.Should the manufacturing dept. assign a PN suffix different from “00”, the IPC will be accordingly updated with the next possible revision. IPC 三種情況三種情況 飛機(jī)上安裝的件號(hào)飛機(jī)上安裝的件號(hào) 后綴后綴 “00”& ”40 至至 50”1. PN: D521523200100 對(duì)于對(duì)于“非可能性備件非可能性備件non potential spares* 或其或其 它可以按圖紙?zhí)峁┑牧慵梢园磮D紙?zhí)峁┑牧慵?不需要備

41、用件技術(shù)規(guī)范不需要備用件技術(shù)規(guī)范 STS), 后綴默認(rèn)為后綴默認(rèn)為“00” 或者或者 后綴后綴“01 至至 39” 2. PN: D521523200101 后綴后綴 01 用于不同于圖紙的可能備用件用于不同于圖紙的可能備用件, 在備用件在備用件 技術(shù)規(guī)范技術(shù)規(guī)范(STS)中給出詳細(xì)的解釋中給出詳細(xì)的解釋, STS 與備件與備件 PN: D521 5232 001 一起發(fā)給用戶一起發(fā)給用戶 (WHITH OR WITHOUT Suffix) 或者或者 后綴后綴 “51 至至 59”3. PN: D521523200151 后綴后綴 51 用于不同于設(shè)計(jì)圖紙的可能備用組件用于不同于設(shè)計(jì)圖紙的可能

42、備用組件, 組件中包括的詳細(xì)件號(hào)目錄標(biāo)明在相關(guān)的在備用組件中包括的詳細(xì)件號(hào)目錄標(biāo)明在相關(guān)的在備用 件技術(shù)規(guī)范件技術(shù)規(guī)范(STS)中與備件一起提供給用戶中與備件一起提供給用戶. 注注: AIRBUS 產(chǎn)權(quán)件號(hào)后綴由產(chǎn)權(quán)件號(hào)后綴由AIRBUS的零件生產(chǎn)部門提供的零件生產(chǎn)部門提供Non potential Spares part = “非可能性備件非可能性備件”指在空客推薦單中未包含的航線可更換件指在空客推薦單中未包含的航線可更換件(如如:某些高某些高M(jìn)TBUR零件零件)然而然而, 如某用戶訂購了這種如某用戶訂購了這種“非可能性備件非可能性備件”, 此件的供貨技術(shù)狀態(tài)此件的供貨技術(shù)狀態(tài)(后綴后綴)將

43、由將由AIRBUS的零件生產(chǎn)部門核準(zhǔn)的零件生產(chǎn)部門核準(zhǔn). 如零件生產(chǎn)部門確定如零件生產(chǎn)部門確定將提供的件號(hào)后綴不為將提供的件號(hào)后綴不為“00”, 則則IPC在下一次更改版中將加入此件號(hào)在下一次更改版中將加入此件號(hào) (帶有或不帶有后綴) Prefix Root PN Suffix Add Airbus domestic codes XXD21315432100 ZZZZZTo be disregardedTo be disregarded Can be replaced by: PN: D2131543210000 提供備用件技術(shù)規(guī)范提供備用件技術(shù)規(guī)范STSor PN: D21315432100

44、01 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：適用于非彩色零件注意：適用于非彩色零件源件號(hào)源件號(hào)可被下列件號(hào)替換可被下列件號(hào)替換前綴前綴后綴后綴可忽略可忽略可忽略可忽略提供件號(hào)互換性信息提供件號(hào)互換性信息, 互換代碼互換代碼01或或02增加空客內(nèi)部代碼增加空客內(nèi)部代碼WHY ?為什么為什么 TO I

45、NDICATE 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.給出給出IPC 不同圖示之間不同圖示之間, 或不同機(jī)型之間零件的互換性或不同機(jī)型之間零件的互換性.建議可替換的零件建議可替換的零件.方便備件計(jì)劃及維護(hù)工作方便備件計(jì)劃及維護(hù)工作.HOW ?如何替如何替換換 BY ADDIN

46、G IN THE IPC DETAILED PARTS LIST THE FOLLOWING INFORMATION : 在在IPC 詳細(xì)件號(hào)清單中加入下述信息詳細(xì)件號(hào)清單中加入下述信息:Two way I/W (Interchangeable With PN)雙向互換雙向互換One way RPLD BY (RePlaceD BY PN)單向互換單向互換 Qualified Spares informationRPLD BY or I/W可用備件信息可用備件信息單向或雙向互換單向或雙向互換Y I/W X (Interchangeable With) / The part Y can be r

47、eplaced 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).件號(hào)Y可以被新件號(hào)X作為備件替換, 反之亦可.此替換不對(duì)飛機(jī)的構(gòu)型產(chǎn)生任何改變. 新件號(hào)X安裝后,它也可以被替換而將Y重新安裝到同一架飛機(jī)上. Yx PN Y(8450

48、B2) 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).件號(hào)Y可以被新件號(hào)X作為備件替換.此替換不對(duì)飛機(jī)的構(gòu)型產(chǎn)生任何改變.

49、新件號(hào)X安裝后,它也可以被替換而將Y重新安裝到同一架飛機(jī)上. xY Y can be replaced by X with qualified condition given with the text . No other PN CHANGE (I/W;REPLD BY or other condition).件號(hào)Y可以在一定條件下被件號(hào)X替換.但不允許進(jìn)一步替換.xYNo QUALIFIED SPARES with the MAINTENANCE FIGURE詳圖上不顯示有效備件. Direct access to the DATA 直接進(jìn)入到手冊內(nèi)容 By description/Tab

50、le Of Content (TOC) 由內(nèi)容目錄進(jìn)入 By Functional Item Number (FIN) 由功能識(shí)別號(hào)進(jìn)入 By Part Number (PN) 由件號(hào)進(jìn)入 By Zone 按區(qū)域進(jìn)入 Service Bulletin 按服務(wù)通告進(jìn)入 Effectivity 按有效性 Installation figure(CSN) 安裝圖 Part Number CHANGE 可查找互換性 Detail figure & IPC/AMM 詳圖及IPC/AMM鏈接切換 AIRBUS CHINA LTD. All rights reserved. Confidential and

51、 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 withou

52、t 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 su

53、pporting 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.Technical Data Support & Services?PFRLog BookECAM WarningECAM 警告信息警告信息CFDS

54、 failure messageCFDS 故障信息故障信息參考時(shí)間GMT和ATA章節(jié)將ECAM 信息和CFDS故障信息聯(lián)系起來故障信息ECAM警告信息(81)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 ADI

55、RU1 DATA注注: ADIRU 數(shù)據(jù)信息的用戶會(huì)向數(shù)據(jù)信息的用戶會(huì)向CFDIU 發(fā)出故障信息發(fā)出故障信息, 為外部信息為外部信息.AIR DATA INERTIAL REF. UNITELECTRONIC INST. STEMAUTOMATIC FLIGHT SYSTEMElect. Centralized Aircraft MonitoringFull Authority Digital Engine Control123Failure / Fault Classes故障故障/故障等級(jí)故障等級(jí)對(duì)本航段的飛行操作是否有影對(duì)本航段的飛行操作是否有影響響是是否否否否是是是是否否對(duì)機(jī)組是否有指示

56、信息對(duì)機(jī)組是否有指示信息自動(dòng)顯示自動(dòng)顯示- 在在ECAM顯示警告顯示警告/警戒警戒 信息信息 - 在駕駛艙中顯示警告旗在駕駛艙中顯示警告旗 和其它警告和其它警告在在 ECAM STATUS PAGE狀態(tài)頁上狀態(tài)頁上, 但但只在航段只在航段10 & 01對(duì)放行影響對(duì)放行影響 參考參考 MMEL 可能是可能是 “GO” 無條件放行無條件放行“GO IF” 有條件放行有條件放行“NO GO” 不能放行不能放行勿需參考勿需參考 MMEL無條件放行無條件放行10天天 MMEL 不適用不適用(不影響放行不影響放行)對(duì)維護(hù)人員是否有對(duì)維護(hù)人員是否有指示指示是是每個(gè)航段之后打印每個(gè)航段之后打印 CFDS PF

57、R是是通過通過CFDS SystemReport/Test查尋查尋PFRAI/SE-D4- APR 96航站維護(hù)航站維護(hù) 飛行記錄本中無報(bào)告則無需做維護(hù)工作 記錄本中如報(bào)告 (一級(jí)故障)查閱 PFR + System report/test LRU level only + 參考 MMEL放行本站維護(hù)本站維護(hù)/航后航后 維護(hù)狀態(tài)信息 PFR 中二級(jí)故障信息 LRU level + System report/test定檢定檢 三級(jí)故障一般三級(jí)故障報(bào)告 LRU level + System report/test LRU level車間部件維護(hù)車間部件維護(hù) 排故數(shù)據(jù)TSD + BITE 存儲(chǔ)數(shù)據(jù)

58、 LRU 拆下Trouble shooting data LRU level+ BITE shop memory-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 工作準(zhǔn)備信息工作準(zhǔn)備信息-Fault confirmation 故障確認(rèn)故障確認(rèn)-Fault isolation 故障隔離程序故障隔離程序 任務(wù)號(hào)任務(wù)號(hào)/標(biāo)題標(biāo)題-Task N/Title- Block Diagram- Schematics- Logic- Supporting data-方塊圖方塊圖-簡圖簡圖-邏輯圖邏輯圖-輔助數(shù)據(jù)輔助數(shù)據(jù)PFRPostFlightRe

59、portTEMTool & Equipment ManualMMELCDLConfiguration DeviationList (m)TSM Trouble ShootingManualCLMComponentLocationManualMMELPart 3SimplifiedDeactivationProceduresTask NumberATA Ref. LOGBOOKAMM AircraftMaintenanceManualWARNING/MALFUNCTIONMAINTENANCE/CREW OBSERVATIONDeactivationSystemTESTTOOL PNASMAir

60、craftSchematicsManualAWMAircraftWiringManual20-42/0220-42-06MMEL/CDLReferenceMCDUA/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