常用維修手冊(cè)及維修文件介紹.ppt

1、Manual and Drawing Usage Instructor: Zou Liming Zu Biao,General Classification for Manuals,Customized Manual,Non-Customized Manual,AMM AIPC WDM (AWM, AWL) SSM (ASM) FIM (TSM),SRM SWPM (ESPM) SOPM (PMS) MPD NTM ITEM (TEM) CML (Airbus),PART 1 Boeing Manual System,MyBoeingFleet: ,PART 1 Boeing Manual S

2、ystem,Delta Web page: ,PART 1 Boeing Manual System/AMM,PART 1 Boeing Manual System/AMM,Page Block,PART 1 Boeing Manual System/AMM,AMTOSS (Aircraft Maintenance Task-Oriented Support System) / AMTOSS Numbers TASK 29-11-05-400-801-002,PART 1 Boeing Manual System/AMM,ATA 100 Chapter Aircraft General Gro

3、up / 飛機(jī)概述 05 TIME LIMITS/MAINTENANCE CHECKS 時(shí)限/維護(hù)檢查 06 DIMENSIONS AND AREAS 尺寸和區(qū)域 07 LIFTING & SHORING 頂起與支撐 08 LEVELING & WEIGHING 校水平和稱重 09 TOWING & TAXIING 牽引和滑行 10 PARKING, MOORING, STORAGE & RETURN TO SERVICE 停放和系留 11 PLACARDS AND MARKINGS 標(biāo)牌和標(biāo)記 SERVICING 勤務(wù) Airframe Systems Group / 飛機(jī)機(jī)體系統(tǒng) 20 S

4、TANDARD PRACTICES-AIRFRAME 標(biāo)準(zhǔn)實(shí)施-機(jī)身 21 AIR CONDITIONING 空調(diào) 22 AUTO FLIGHT 自動(dòng)飛行 23 COMMUNICATIONS 通訊,PART 1 Boeing Manual System/AMM,24 ELECTRICAL POWER 電源 25 EQUIPMENT/FURNISHINGS 設(shè)備/裝飾 26 FIRE PROTECTION 防火 27 FLIGHT CONTROLS 飛行操縱 28 FUEL 燃油 29 HYDRAULIC POWER 液壓 30 ICE AND RAIN PROTECTION 防冰和防雨 31

5、INDICATING/RECORDING SYSTEMS 指示/記錄系統(tǒng) 32 LANDING GEAR 起落架 33 LIGHTS 燈 34 NAVIGATION 導(dǎo)航 35 OXYGEN 氧氣 36 PNEUMATIC 氣動(dòng)系統(tǒng) 38 WATER/WASTE 水/污水 46 INFORMATION SYSTEMS 信息系統(tǒng) 49 AIRBORNE AUXILIARY POWER 空運(yùn)的輔助電源,PART 1 Boeing Manual System/AMM,Structure Group / 結(jié)構(gòu) 51 STANDARD PRACTICES AND STRUCTURES - GENERAL

6、 標(biāo)準(zhǔn)施工與結(jié)構(gòu)簡(jiǎn)介 52 DOORS 艙門(mén) 53 FUSELAGE 機(jī)身 54 NACELLES/PYLONS 短艙/吊架 55 STABILIZERS 安定面 56 WINDOWS 窗 57 WINGS 機(jī)翼,PART 1 Boeing Manual System/AMM,Power Plant Group / 動(dòng)力裝置 70 STANDARD PRACTICES - ENGINES 標(biāo)準(zhǔn)實(shí)施-發(fā)動(dòng)機(jī) 71 POWER PLANT 動(dòng)力裝置 72 ENGINE 發(fā)動(dòng)機(jī) 73 ENGINE FUEL AND CONTROL 發(fā)動(dòng)機(jī)燃油和控制 74 IGNITION 點(diǎn)火 75 AIR 空氣

7、76 ENGINE CONTROLS 發(fā)動(dòng)機(jī)控制器 77 ENGINE INDICATING 發(fā)動(dòng)機(jī)指示 78 EXHAUST 排氣 79 OIL 滑油 80 STARTING 起動(dòng),PART 1 Boeing Manual System/AMM,Power Plant Group / 動(dòng)力裝置 70 STANDARD PRACTICES - ENGINES 標(biāo)準(zhǔn)實(shí)施-發(fā)動(dòng)機(jī) 71 POWER PLANT 動(dòng)力裝置 72 ENGINE 發(fā)動(dòng)機(jī) 73 ENGINE FUEL AND CONTROL 發(fā)動(dòng)機(jī)燃油和控制 74 IGNITION 點(diǎn)火 75 AIR 空氣 76 ENGINE CONTR

8、OLS 發(fā)動(dòng)機(jī)控制器 77 ENGINE INDICATING 發(fā)動(dòng)機(jī)指示 78 EXHAUST 排氣 79 OIL 滑油 80 STARTING 起動(dòng),PART 1 Boeing Manual System/AMM,Function Code,PART 1 Boeing Manual System/AMM,The sequence number is used to provide a unique number when the first four elements are not unique. (a) The sequence number starts at 801 for tas

9、ks and continues through 999. If there are more than 200 tasks, the number continues with A01 through A99, B01 through B99, etc. (b) The sequence number starts at 001 for subtasks and continues through 799. The configuration number is used to indicate an engine or page block configuration. (a) The f

10、irst position is the engine prefix. (b) The second and third positions are the page block configuration. (c) If the page block is not part of the engine chapters or does not have a CONFIG number (see effectively and configuration numbering), then the tasks and subtasks will not have this element. (d

11、) If the page block is not part of the engine chapters but does have a configuration number, then the first position will have a zero and the last two will indicate the CONFIG number.,PART 1 Boeing Manual System/AMM,PART 1 Boeing Manual System/IPC,PART 1 Boeing Manual System/IPC, 如果已知件號(hào)，則由數(shù)碼索引入手： 在數(shù)

12、碼索引中找到此件號(hào)，并記下對(duì)應(yīng)的章、節(jié)、組件、圖和項(xiàng)目號(hào)。 由圖號(hào)可找到相應(yīng)的圖解。 在圖解中找到部件及項(xiàng)目號(hào)，并在清單中可找到相應(yīng)的部件及相關(guān)的內(nèi)容。, 如果未知件號(hào)，則由目錄內(nèi)容表入手： 在預(yù)想到的章節(jié)中找到內(nèi)容目錄表。 參見(jiàn)零件所在的主組。 圖是按主要名稱的字母順序列出的，找到零件最有可能被顯示的圖解標(biāo)題，記下圖號(hào)。 由圖解和清單可找到相應(yīng)的內(nèi)容。,查找IPC的方法,PART 1 Boeing Manual System/IPC,PART 1 Boeing Manual System/IPC,PART 1 Boeing Manual System/IPC,PART 1 Boeing Ma

13、nual System/IPC,1. FIGURE NUMBER - The figure number identifies the illustration and the part list defining a specific portion of the aircraft coverage. The figure number appears in the illustration title, to the left of the first item number in the FIGURE ITEM column at the top of each parts list p

14、age, and in the footing of each applicable page. 2. ITEM NUMBER - The item number corresponds to the number on the part in the illustrations. A dash (-) preceding the item number indicates that the part is not illustrated. As noted in the Explanation of Customizing description, item numbers missing

15、from parts list section but found on the illustration are not applicable. 3. NEXT HIGHER ASSEMBLY (NHA) CROSS REFERENCE - The reference catalog location indicates where the used on component or assembly is defined. 4. UNITS PER ASSEMBLY (UPA)- The quantity of the part which is used on the NHA assemb

16、ly. The following entries other than a numeric value maybe found in the IPC data: RF (Reference) - Indicates the item is listed at the NHA location which carries the UPA quantity. The NHA location is found through the NHA cross reference (See 3.). AR (As Required) - Indicates the part is used in a q

17、uantity determined at the time when the part is installed.,PART 1 Boeing Manual System/IPC,5. SUPPLIER CODE - The (5) digit code which identifies the manufacturer of the part. The Supplier Code is found in the nomenclature column following the supplier part number entry. The Supplier Code is extract

18、ed from the Cataloging Handbook H4/H8, Commercial and Government Entity (CAGE), the NATO Supply Code for Manufacturers (NSCM), or it is assigned by Boeing if not available from the CAGE or NSCM handbooks. The supplier name and address corresponding to each Supplier Code is available in the Suppliers

19、 Name and Address Index. 6. SPECIFICATION NUMBER and QUALIFIED PARTS - The Specification Number is a Boeing assigned number which defines all of the necessary part performance requirements a supplier must comply with to be qualified to produce the part. The Boeing Specification number is documented

20、in the Part Number column when no supplier part has been qualified. When a supplier part qualifies to a Boeing Specification, the supplier part number is shown in the Part Number column and the specification is placed in the Nomenclature column. Any additional qualified supplier parts are captured a

21、s optional parts in the nomenclature column. 7. USED ON - A note in the Nomenclature column which indicates the appropriate next higher assembly when the part is not common to all of the next higher assemblies listed preceding the part.,PART 1 Boeing Manual System/IPC,8. FOR DETAILS SEE - A referenc

22、e to another location where the installation or assembly is broken down in further detail to its component parts. 9. POSITION DATA - Extra information defining where the part is installed. Typical information presented here includes station or zone location information or physical installed position

23、 information. 10. ALTERED FROM - An existing component that was altered to create another part number. There are only minor modification differences between the original (Altered from) part number and the new part number. 11. EFFECT TO FROM - Where a design change produces a qualified or limited int

24、erchangeability condition, the delivered effectivity is shown and an appropriate note is included in the nomenclature column to define this condition. The relationship between parts shown in interchangeability notes is defined by the following terms: REPLACES OR REPL BY - Indicates the parts (or set

25、s) are physically and functionally interchangeable. MAY USE - Indicates a one-way interchangeability exists, either forward or backward, depending on the parts involved. T/W (together with) - Indicates parts which are necessary to be replaced along with the main part for interchangeability. Intercha

26、ngeability is only accomplished as specified by the note.,PART 1 Boeing Manual System/IPC,12. ILLUSTRATION REFERENCE - A reference note to the functionally related figure which defines the part(s). The part is drawn at this figure in phantom for identification of an Illustration Reference condition.

27、 Tubing and ducts are example uses for This reference. 13. OVERLENGTH PART NUMBER - A Boeing Company Reference(BCREF) number is assigned to all overlength part numbers which exceed 15 digits. The BCREF number is placed in the Part column and the overlength number is in the nomenclature column. PN UN

28、ASSIGNED - BCREF numbers are also assigned when there is no part number for a component. This condition occurs for supplier or customer modification data. 14. MAINTENANCE COMPONENTS OF ASSEMBLIES - Disassembly sequence of intermediate subassemblies may not be included in the IPC if the intermediate

29、subassemblies are not considered line maintenance components. TEMPORARY BREAKDOWN - A note which is included in the IPC when a design change produces an assembly part number for which breakdown information is not available. Breakdown components for the current assembly are extended as a applicable f

30、or the new assembly. The temporary breakdown note is removed when actual breakdown information is available and incorporated in the IPC.,PART 1 Boeing Manual System/IPC,15. ATTACHING PARTS - Attaching parts are listed immediately following the item which they attach. They are preceded by the phrase

31、Attaching Parts and are followed by the symbol -*-. 16. BOEING STANDARD PARTS - Boeing Standard Parts are identified by a BAC prefix. The Boeing Standard Part Number appears in the part number column when no supplier part has yet been qualified. When an equivalent supplier part number is qualified,

32、it will appear in the part number column and the Boeing Standard Part Number and any other equivalent supplier numbers will appear in the nomenclature column as optional parts If no supplier part numbers are included in the Parts List for a Boeing Standard, see the Boeing Standards Volumes (D-590),

33、Boeing to Supplier Part Number Cross-Reference Index or the specific standards page for procurement source information. 17. CHANGE INDICATORS - Change indicators are applied opposite the revised data line entry. An R in the margin indicates the line opposite was added or revised in the current revis

34、ion. When the Parts List page for a figure includes Airline Stock Numbers, the letter S is shown opposite the line entry When a change in the Airline Stock Number data is the only Change to the item entry.,PART 1 Boeing Manual System/IPC,18. FUNCTIONALIZED COVERAGE - Certain items contain components

35、 which are illustrated and listed in various chapters according to their ATA Specification 100 function. The presence of this condition is indicated by showing the figure location(s) for the functionalized coverage in the NOMENCLATURE column of the major installation or assembly line entry. In the e

36、xample, the portion of the Door Instal- lation covering LIGHTS is displayed in the figure identified in Chapter 33. The portion covering NACELLES/ PYLONS is shown in the figure identified in Chapter 54. 19. BOEING PROPRIETARY COLOR CODED PARTS - Boeing Proprietary Color Coded Parts, excluding Boeing

37、 specification part numbers 10-XXXXX, SXXXNXXX, SXXXTXXX, SXXXUXXX, SXXXWXXX or 60BXXXXX, are identified with an alpha SP suffix. This entry represents consolidation of all color codes applicable for the given usage. Color coded parts may be ordered with either the specific airline (alpha) color cod

38、e suffix or the consolidated SP suffix. Orders received for SP parts will be converted and processed under the airlines (alpha) color coded part number. A reference to the appropriate aircraft registry number or the color name on orders for SP parts will facilitate the color conversion. Note: Color

39、code does not affect physical or functional interchangeability aspects. 20. LOCAL FABRICATION PARTS - Material requirements for parts which can be locally fabricated are included in the Nomen- clature column within a (MFD FROM-) note.,PART 1 Boeing Manual System/IPC,21. FIGURE TITLE - Where more tha

40、n one lead entry or subject is included in a figure, a figure title is used to facilitate the preparation and maintenance of the Chapter Table of Contents entries. The Effectivity column for the figure title identifies the aircraft covered in the figure. 22. COMPONENT MAINTENANCE MANUAL REFERENCE -

41、The applicable Component Maintenance Manual providing detail coverage of an assembly is identified in a (REF CMM-) note in the Nomenclature column. For Supplier Assemblies the applicable supplier code is shown following the nomenclature of the part identified in the Part Number Column. 23. SERVICE B

42、ULLETIN ENTRIES - Boeing Service Bulletins are incorporated in the IPC only upon notification from the airline that the intent of the SB has been accomplished. Service Bulletin coverage is incorporated using one of the following methods as specified by the airline: Dual configuration reflects both t

43、he before and after Service Bulletin incorporation components in accordance with Spares Letter No. 309, Option 1. Single configuration reflects only the after Service Bulletin incorporation components in accordance with Spares Letter No. 309, Option 2. A record of the Service Bulletins submitted for

44、 incorporation in the IPC is shown in the Service Bulletin/Modification List.,PART 1 Boeing Manual System/IPC,24. FILTER MAINTENANCE KITS - Boeing defines a kit part number which contains all of the parts necessary to support the removal and maintenance of a filter on the airplane. The kit is a conv

45、enience to the operator and contains the filter/module element(s), packing(s)/O-ring(s), gaskets and all standard parts necessary for maintaining the element. The filter Maintenance Kit part number is referenced in the nomenclature column of the element entry. The definition of the Filter Maintenanc

46、e Kit contents are detailed in the Filter Maintenance Kit section of the IPC. 25. ELECTRICAL EQUIPMENT NUMBER - The Wiring Diagram equipment numbers are referenced in the IPC nomenclature as applicable to a documented part. Electrical Equipment Numbers also appear in the IPC on placards for identify

47、ing equipment. 26. ETOPS ENTRIES - The IPC defines parts which are required to support Extended Twin Operation (ETOPS) for two (2) engine aircraft. ETOPS notes appear in the nomenclature field of the IPC under the following conditions: Not Approved for ETOPS Means that part can not be installed to m

48、eet ETOPS flying requirements. Not Approved For ETOPS After Service Bulletin or Service Letter Incorporation Means that the part is not certified for ETOPS if the referenced Service Bulletin or Service Letter is incorporated on the airplane.,PART 1 Boeing Manual System/IPC,27. MAINTENANCE MANUAL REF

49、ERENCE - A cross reference to the applicable Boeing Maintenance Manual location which contains the procedure for removal and repair of that part. EXPLANATION OF ILLUSTRATION TECHNIQUE The illustration portion of a figure in the Illustrated Parts Catalog pictorially displays the relationship of the p

50、arts identified in the Parts List. The following is an explanation of certain techniques used in the illustration to present the relationship of these parts. The numbers correspond to those shown in the following sample. 1. Detail coverage of any portion of the illustration is provided by isolating

51、sections in specific exploded views with alphabetic designations. 2. Components of assemblies are shown either within a specific exploded view of the assembly or the item numbers of the components are included within a bracket which is identified by the item number of the assembly. 3. When a compone

52、nt is physically illustrated such that a lead line from the item number within a bracket to the illus- tration of the part would be confusing or indeterminate, an arrow is used to point in the direction of the illustrated component. 4. Alternate configuration are indicated by a dual-headed arrow rel

53、ating the illustration of the configuration involved.,PART 1 Boeing Manual System/IPC,GENERAL SYSTEM OF ASSEMBLY ORDER-DETAILED PARTS LIST (DPL) The indenture system used in the Parts Lists of the figures included within this catalog shows the relationship of one part to another. For a given item, t

54、he number of indentures defines the relationship of the item to the associated installation, next higher assembly, or components of the item as follows:,PART 1 Boeing Manual System/WDM,查找WDM的方法： 已知Equipment Number, Wire Number, 根據(jù)Equipment List 或 Wire List 索引到相應(yīng)的電路圖。 未知Equipment Number, Wire Number,

55、 則需要設(shè)備所屬章節(jié)，功能在WDM上找到相應(yīng)的電路圖。 以Wire Number W0018-0001-22 和Equipment Number C1434為例。,PART 1 Boeing Manual System/WDM,PART 1 Boeing Manual System/WDM,PART 1 Boeing Manual System/WDM,PART 1 Boeing Manual System/WDM,作用：進(jìn)行系統(tǒng)排故時(shí)使用的輔助手冊(cè)。,PART 1 Boeing Manual System/SSM,SWPM Standard Wire Practice Manual手冊(cè)的用途

56、： Standard Practice Procedure Wire Material Terminal/Splice Part Number Connector Configuration/Repair Contact Part Number Example: Locate the Wire Material for W0018-0001-22 and configuration for D40576P.,PART 1 Boeing Manual System/SWPM,PART 1 Boeing Manual System/SWPM,PART 1 Boeing Manual System/

57、SWPM,20 - Cross Reference Index,PART 1 Boeing Manual System/SWPM,PART 1 Boeing Manual System/SWPM,PART 1 Boeing Manual System/FIM, 如果有故障碼：,由第一個(gè)兩位數(shù)找出對(duì)應(yīng)的章，然后找到故障碼索引； 由索引可得到相應(yīng)的條件或措施； 如果有說(shuō)明可能原因，即按要求排故； 如果給出參考流程圖，即按圖索驥； 如果故障碼是X-字母，即有說(shuō)明要求參考WDM或SSM。,PART 1 Boeing Manual System/FIM, 如果無(wú)故障碼：,有EICAS信息： 如果不知道屬于哪一章，由EICAS信息入手； 如果知道了哪一章，即由該章的信息表入手。,系統(tǒng)測(cè)試： 找到相應(yīng)系統(tǒng)的測(cè)試索引； 由索引可得到相應(yīng)的章節(jié)； 在相應(yīng)的小節(jié)內(nèi)可找到測(cè)試步驟。, 無(wú)EICAS信息，也無(wú)系統(tǒng)測(cè)試：由故障代碼流程圖入手。,PART