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1、Manual and Drawing UsageInstructor:Zou Liming Zu Biao,General Classification for Manuals,Customized Manual,Non-Customized Manual,AMMAIPCWDM(AWM,AWL)SSM(ASM)FIM(TSM),SRMSWPM(ESPM)SOPM(PMS)MPDNTMITEM(TEM)CML(Airbus),PART 1 Boeing Manual System,MyBoeingFleet:,PART 1 Boeing Manual System,Delta Web page:
2、https,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 NumbersTASK 29-11-05-400-801-002,PART 1 Boeing Manual System/AMM,ATA 100 ChapterAircraft General Group/飞机概述05 TIME LIMITS/
3、MAINTENANCE CHECKS 时限/维护检查06 DIMENSIONS AND AREAS 尺寸和区域07 LIFTING&SHORING 顶起与支撑08 LEVELING&WEIGHING 校水平和称重09 TOWING&TAXIING 牵引和滑行10 PARKING,MOORING,STORAGE&RETURN TO SERVICE 停放和系留11 PLACARDS AND MARKINGS 标牌和标记SERVICING 勤务Airframe Systems Group/飞机机体系统20 STANDARD PRACTICES-AIRFRAME 标准实施-机身21 AIR CONDI
4、TIONING 空调22 AUTO FLIGHT 自动飞行23 COMMUNICATIONS 通讯,PART 1 Boeing Manual System/AMM,24 ELECTRICAL POWER 电源25 EQUIPMENT/FURNISHINGS 设备/装饰26 FIRE PROTECTION 防火27 FLIGHT CONTROLS 飞行操纵28 FUEL 燃油29 HYDRAULIC POWER 液压30 ICE AND RAIN PROTECTION 防冰和防雨31 INDICATING/RECORDING SYSTEMS 指示/记录系统32 LANDING GEAR 起落架3
5、3 LIGHTS 灯34 NAVIGATION 导航35 OXYGEN 氧气36 PNEUMATIC 气动系统38 WATER/WASTE 水/污水46 INFORMATION SYSTEMS 信息系统49 AIRBORNE AUXILIARY POWER 空运的辅助电源,PART 1 Boeing Manual System/AMM,Structure Group/结构51 STANDARD PRACTICES AND STRUCTURES-GENERAL 标准施工与结构简介52 DOORS 舱门53 FUSELAGE 机身54 NACELLES/PYLONS 短舱/吊架55 STABILI
6、ZERS 安定面56 WINDOWS 窗57 WINGS 机翼,PART 1 Boeing Manual System/AMM,Power Plant Group/动力装置70 STANDARD PRACTICES-ENGINES 标准实施-发动机71 POWER PLANT 动力装置72 ENGINE 发动机73 ENGINE FUEL AND CONTROL 发动机燃油和控制74 IGNITION 点火75 AIR 空气76 ENGINE CONTROLS 发动机控制器77 ENGINE INDICATING 发动机指示78 EXHAUST 排气79 OIL 滑油80 STARTING 起
7、动,PART 1 Boeing Manual System/AMM,Power Plant Group/动力装置70 STANDARD PRACTICES-ENGINES 标准实施-发动机71 POWER PLANT 动力装置72 ENGINE 发动机73 ENGINE FUEL AND CONTROL 发动机燃油和控制74 IGNITION 点火75 AIR 空气76 ENGINE CONTROLS 发动机控制器77 ENGINE INDICATING 发动机指示78 EXHAUST 排气79 OIL 滑油80 STARTING 起动,PART 1 Boeing Manual System/
8、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 tasks and continues through 999.If there are more than 200 tasks,the number continues with A01 through A99,B01
9、 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 first position is the engine prefix.(b)The second and third positions are the page block configuration.(c)If the page
10、 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)If the page block is not part of the engine chapters but does have a configuration number,then the first position will hav
11、e 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,如果已知件号，则由数码索引入手：在数码索引中找到此件号，并记下对应的章、节、组件、图和项目号。由图号可找到相应的图解。在图解中找到部件及项目号，并在清单中可找到相应的部件及相关的内容。,如果未知件号，则由目录内容表入手：在预想到的章节中找到内容目录表。参见零件所在的主组。图是按主要名称的字
12、母顺序列出的，找到零件最有可能被显示的图解标题，记下图号。由图解和清单可找到相应的内容。,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 Manual System/IPC,1.FIGURE NUMBER-The figure number identifies the illustration and the part list defining a specific portion of the air
13、craft 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 page,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 d
14、ash(-)preceding the item number indicates that the part is not illustrated.As noted in the Explanation of Customizing description,item numbers missing from parts list section but found on the illustration are not applicable.3.NEXT HIGHER ASSEMBLY(NHA)CROSS REFERENCE-The reference catalog location in
15、dicates where theused on component or assembly is defined.4.UNITS PER ASSEMBLY(UPA)-The quantity of the part which is used on the NHA assembly.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
16、 UPA quantity.The NHA location is found through the NHA cross reference(See 3.).AR(As Required)-Indicates the part is used in a quantity 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.T
17、he Supplier Code is found in the nomenclature column following the supplier part number entry.The Supplier Code is extracted 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 CA
18、GE or NSCM handbooks.The supplier name and address corresponding to each Supplier Code is available in the Suppliers 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
19、 a supplier must comply with to be qualified to produce the part.The Boeing Specification number is documented 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 t
20、he specification is placed in the Nomenclature column.Any additional qualified supplier parts are captured as 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 high
21、er assemblies listed preceding the part.,PART 1 Boeing Manual System/IPC,8.FOR DETAILS SEE-A reference 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 informa
22、tion presented here includes station or zone location information or physical installed position 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 pa
23、rt number.11.EFFECT TO FROM-Where a design change produces a qualified or limited interchangeability 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 i
24、s defined by the following terms:REPLACES OR REPL BY-Indicates the parts(or sets)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
25、be replaced along with the main part for interchangeability.Interchangeability 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 ph
26、antom for identification of an Illustration Reference condition.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 t
27、he overlength number is in the nomenclature column.PN UNASSIGNED-BCREF numbers are also assigned when there is no part number for a component.Thiscondition occurs for supplier or customer modification data.14.MAINTENANCE COMPONENTS OF ASSEMBLIES-Disassembly sequence of intermediate subassemblies may
28、 not be included in the IPC if the intermediate 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 cur
29、rent assembly are extended as a applicable for 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
30、attach.They are preceded by the phrase 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 sup
31、plier part number is qualified,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 Boei
32、ng Standards Volumes(D-590),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 revis
33、ed in the current revision.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
34、contain components 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
35、 entry.In the example,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
36、Boeing 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 code s
37、uffix 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 code does
38、 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 than one lead entry or
39、 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-The applicable Component
40、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 BULLETIN ENTRIES-Boeing Service
41、 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 the before and after Service Bullet
42、in 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 incorporation in the IPC is shown in th
43、e 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 convenience to the operator and contains the fil
44、ter/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 Maintenance Kit contents are detailed in the Filter Mainte
45、nance 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 identifying equipment.26.ETOPS ENTRIES-The IPC defines parts
46、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 meet ETOPS flying requirements.Not Approved For ETOPS After Serv
47、ice 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 REFERENCE-A cross reference to the applicable Boeing Maintenance Man
48、uallocation which contains the procedure for removal and repair of that part.EXPLANATION OF ILLUSTRATION TECHNIQUEThe illustration portion of a figure in the Illustrated Parts Catalog pictorially displays the relationship of the parts identified in the Parts List.The following is an explanation of c
49、ertain 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 sections in specific exploded views with alphabetic designations.2.Compone
50、nts 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 component is physically illustrated such that a lead line from the item number within
